Launch times are in UTC and are either from the launching agency or estimated by 'walking back' along the ground track to the launch site. Most orbit data and decay information comes from SpaceTrack. The Space-Track data occasionally contains inconsistencies (eg - incorrect re-entry dates or early sets of elements allocated to the wrong object) that need to be corrected from other sources.

To fill the gaps where elements are not formally published, usually because they have a classification of "Secret", some orbits are based on amateur observations. Such data is published near-daily by Mike McCants. Occasionally, orbits are estimated by myself from public data.

Space-Track sometimes has insufficient information to allocate names to objects in its catalogue. In these cases, names are derived from public information.

Apogee and perigee are measured against a spherical Earth with a radius of 6378.145 km, assumed to be situated at the focus of the orbital ellipse. The value for the orbital period is the Anomalistic Period, or time to complete one circuit of the ellipse. It is not the same as the time taken to complete one circuit of the Earth. Care should be exercised when comparing Orbital Focus data with other published orbits because they may have been derived using a different model.

Users can go straight to specific launches by pointing to the page URL followed by the three digit launch number, eg - https://www.OrbitalFocus/Diaries/Launches/Launches.php?year=2023#001

You can keep up to date with changes or mission events by following Orbital Focus at Blue Sky.

2023-001 Falcon 9 Block 5 (Transporter 6) Cape Canaveral Space Force Station						2023 Jan 3, 14:56
STARVIBE (Small Telescope for Advanced Reconnaissance Vision Inspection Boom Experiment) 2023-001A 55009						in space
6U Cubesat from Scanway Space - demonstration mission to verify the performance of two optical payloads - an Earth observation telescope and a system for auto-inspection of satellites. Released from launch vehicle at L +01:00:35.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 13, 17:22	6909	0.0010	524	538	95.25	97.50	191	09:30
Menut 2023-001B 55010						in space
6U Cubesat from Spanish company Open Cosmos and carrying an Earth imaging system. Released from launch vehicle at L +01:00:12.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 13, 17:22	6908	0.0010	523	538	95.24	97.50	193	09:30
BRO 8 (Breizh Reconnaissance Orbiter 8) 2023-001C 55011						in space
6U Cubesat (3x2) from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Released from launch vehicle at L +01:00:01.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 13, 17:21	6908	0.0011	523	538	95.24	97.51	194	09:30
Connecta T1.2 2023-001D 55012						in space
3U Cubesat from Turkish company Plan-S as a demonstrator for a constellation of broadband communications satellites. Released from launch vehicle at L +00:59:51.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 13, 17:20	6908	0.0012	522	538	95.23	97.51	193	09:31
Milspace 2 - Birkeland 2023-001G 55015						in space
6U Cubesat in joint military project between The Netherlands Norway to detect and pinpoint the source of radar transmissions from the Earth's surface. One of a pair of similar satellites launched on the Transporter 6 mission. Released from launch vehicle at L +01:02:02.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 13, 17:19	6908	0.0012	521	537	95.22	97.51	189	09:31
Lynk Tower 4 2023-001AB 55034						in space
Small satellite from Lynk Global providing two-way connectivity for broadband, voice, and text messaging globally. Released from launch vehicle at L +01:20:02.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 13, 07:44	6907	0.0013	520	537	95.21	97.50	177	09:31
Umbra 05 2023-001AD 55036						in space
Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Released from launch vehicle at L +01:23:50.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 13, 12:25	6905	0.0014	517	537	95.17	97.50	183	09:31
Lemur-2 (Emmaculate) 2023-001AE 55037						Re-entered - 2024 May 23 Life 506 days
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. Lemur-2 satellites are named after development and support team members. Released from launch vehicle at L +00:58:44. One of six Lemur-2 satellites carried on the Transporter 6 launch. All are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 13, 09:10	6903	0.0016	514	536	95.14	97.51	177	09:31
Flock 4Y-1 2023-001AG 55039						Re-entered - 2024 Dec 24 Life 721 days
3U Cubesat - part of Planet's Flock 4Y cluster of second generation imaging satellites. Released from launch vehicle at L +01:05:03. One of thirty six similar satellites carried on the Transporter 3 launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 14:45	6906	0.0013	519	537	95.19	97.50	158	09:30
Skykraft 1 2023-001AJ 55041						in space
Small satellite from Australia as a demonstrator for a 200 satellite system to provide air traffic control services in areas away from convential ground station coverage. Released from launch vehicle at L +01:27:34. Also acted as a carrier of four further Skykraft satellites that were released from it around Jan 12.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 14:42	6906	0.0014	518	537	95.19	97.50	162	09:30
Sternula 1 2023-001AM 55044						Re-entered - 2025 Jan 9 Life 737 days
6U Cubesat - Danish satellite carrying a VDES (AIS 2) transmitter/receiver to relay messages between ships at sea and between ships and shore staions. Released from launch vehicle at L +1:06:30.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 14:44	6906	0.0013	519	537	95.20	97.51	167	09:31
ÑuSat 34 (Amelia Earhart) 2023-001AN 55045						in space
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Released from launch vehicle at L +01:21:48.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 14:44	6906	0.0014	518	538	95.19	97.50	158	09:30
Lynk Tower 3 2023-001AP 55046						in space
Small satellite from Lynk Global providing two-way connectivity for broadband, voice, and text messaging globally. Released from launch vehicle at L +01:19:46.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 21:05	6906	0.0013	519	537	95.20	97.50	160	09:30
ÑuSat 33 (Albania 2) 2023-001AQ 55047						in space
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. To provide data under contract to the Albanian government. Released from launch vehicle at L +01:22:03.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 16:19	6906	0.0014	518	538	95.19	97.50	158	09:30
ÑuSat 35 (Williamina Fleming) 2023-001AR 55048						in space
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Released from launch vehicle at L +01:24:47.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 16:18	6906	0.0014	518	537	95.19	97.50	160	09:30
ICEYE X21 2023-001AS 55049						in space
Small satellite fitted with a sythetic aperture radar for Earth surface imaging. Released from launch vehicle at L +01:23:04.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 14:42	6906	0.0014	518	537	95.18	97.50	160	09:30
Umbra 04 2023-001AT 55050						Re-entered - 2024 Sep 3 Life 609 days
Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Released from launch vehicle at L +01:23:46.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 16:16	6905	0.0013	517	536	95.16	97.50	163	09:30
ION SCV-008 (Fierce Franciscus) 2023-001AU 55051						in space
Satellite Carrier Vehicle built by D-Orbit. Released from launch vehicle at L +01:26:05. Hosted payloads: Genergo 2 - a low thrust manoeuvring system, to be confirmed - may be aboard SCV-007. Satellites: TAUSat 2, released Jan 16, Sharjah Sat 1, released Jan 17, Futura SM1, released Jan 18, Futura SM3, released Jan 20, Astrocast 17, released 2023 early December, Astrocast 18, released 2023 early December Astrocast 19, Catalogued by Space-Track 2024 January - release date unknown, Astrocast 20, Catalogued by Space-Track 2024 January - release date unknown.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 17:53	6906	0.0016	517	539	95.19	97.50	169	09:30
2023 Jan 24, 11:59	6906	0.0015	517	538	95.19	97.50	142	09:30
2023 Jan 24, 16:45	6906	0.0016	517	539	95.20	97.50	137	09:30
2023 Jan 31, 09:06	6905	0.0016	516	538	95.18	97.54	121	09:30
2023 Feb 2, 16:41	6907	0.0019	516	542	95.22	97.54	115	09:30
2023 Feb 4, 08:23	6908	0.0020	517	544	95.24	97.57	113	09:30
2023 Feb 10, 13:42	6909	0.0020	517	545	95.25	97.65	96	09:31
2023 Feb 27, 09:27	6914	0.0026	518	553	95.35	98.23	63	09:35
2023 Nov 28, 15:30	6913	0.0008	530	540	95.34	97.63	181	10:38
2023 Dec 4, 01:36	6901	0.0017	512	534	95.09	97.63	101	10:38
2024 Jan 17, 05:27	6912	0.0011	527	541	95.32	97.63	195	10:41
EOS Sat 1 2023-001AW 55053						in space
Small satellite from EOS Sat equipped with Earth imaging and remote sensing systems to support agriculture in particular. Released from launch vehicle at L +01:31:10
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 21:03	6906	0.0015	517	538	95.19	97.50	161	09:30
Skykraft 1A 2023-001AX 55054						in space
Small satellite from Australia as a demonstrator for a 200 satellite system to provide air traffic control services in areas away from convential ground station coverage. One of four similar satellites released from Skykraft 1 around Jan 12. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 16:17	6906	0.0014	518	537	95.18	97.50	162	09:30
Vigoride 5 2023-001AZ 55056						in space
Satellite carrier from US company Momentus Systems, carrying a single satellite to be released in the weeks after launch. Released from launch vehicle at L +01:28:10. Payload: Zeus 1 - released May 11 at around 00:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 16:15	6905	0.0014	517	537	95.17	97.50	164	09:30
Orbiter SN1 2023-001BC 55059						Re-entered - 2024 Jan 6 Life 368 days
Satellite carrier from a company called Launcher with six small satellites and four hosted payloads. Released from launch vehicle at L +01:26:11. Failed to establish orientation due to a problem with its onboard GPS. As a result it was unable to point its solar cells correctly and the internal batteries ran down so planned release of satellites was not possible. Deployable payloads may include: PROVES-Yearling (Pleiades Rapid Orbital Verification Experimental System) - 1U Cubesat from BroncoSpace al Calpoly, designed to allow users on the ground to experiment with satellite hardware and software - includes and imaging system. Celestial - 1U Cubesat from Skyline as a demonstrator of its small satellite platform, name unknown - 1U Cubesat from InnovaSpace - mission details awaited, Sapling Sempervirens - 1U Cubesat from Stanford Student Space Initiative to demonstrate smart downlinking of images using a Google Coral camera and Google Coral Edge coprocessor, name unknown - 1U Cubesat from Italian company NPC Spacemind, name unknown - 1U Cubesat, unidentified owner. Hosted payloads include: CesiumAstro’s Nightingale - to demonstrate advanced phased array communication, Undisclosed customer – payload not known, Beyond Burials – carrying cremated human remains, TRL11 – details awaited.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 16:16	6905	0.0014	517	537	95.18	97.50	162	09:30
ION SCV-007 (Glorious Gratia) 2023-001BD 55060						in space
Satellite Carrier Vehicle built by D-Orbit. Released from launch vehicle at L +01:24:59. Hosted payloads: Drago 2 (Demonstrator of Remote Analysis of Ground Observations) - equipped with infrared Earth imaging system, Cryptosat 2 - prototype of a satellite to operate blockchain and other encrypted systems in orbit, to be confirmed. Satellites: Kelpie 1 (55107/2023-001DC) - released around February 28.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 03:39	6909	0.0018	518	543	95.25	97.50	178	09:30
2023 Jan 25, 08:33	6955	0.0079	522	632	96.21	97.49	161	09:30
2023 Jan 28, 14:40	6957	0.0082	522	636	96.24	97.57	150	09:30
2023 Feb 1, 08:33	6957	0.0083	521	636	96.25	97.61	138	09:29
2023 Feb 8, 23:33	6957	0.0084	520	638	96.26	97.80	113	09:30
2023 Feb 23, 18:09	7024	0.0012	638	655	97.65	98.06	260	09:31
ICEYE X27 2023-001BF 55062						in space
Small satellite fitted with a sythetic aperture radar for Earth surface imaging. Released from launch vehicle at L +01:27:31.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 17:49	6905	0.0015	516	537	95.17	97.50	164	09:30
ÑuSat 32 (Albania 1) 2023-001BH 55064						in space
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. To provide data under contract to the Albanian government. Released from launch vehicle at L +01:20:00.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 19:23	6904	0.0015	516	536	95.16	97.50	167	09:31
NSLSat-2 2023-001BL 55067						Re-entered - 2024 Jul 11 Life 555 days
6U Cubesat from Israel equipped with an expandable, reconfigurable antenna that will unfurl once in orbit. It carries an internet communicaions system to allow tracking of mobile items such as individual shipping containers. Released from launch vehicle at L +01:05:50
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 17:42	6903	0.0016	514	536	95.13	97.51	166	09:31
Sony Sphere-1 2023-001BR 55072						Re-entered - 2025 Mar 4 Life 791 days
6U Cubesat from Sony-Starsphere equipped with a high resolution video and still imaging system from Sony, and a water-based thruster system for orbit control. Released from launch vehicle at L +01:05:40
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 17:45	6904	0.0016	515	537	95.15	97.51	164	09:31
TAUSat 2 (Tel Aviv University Satellite) 2023-001BS 55073						Re-entered - 2025 Mar 25 Life 812 days
2U Cubesat from Tel Aviv University designed to detect small objects in orbit. Released from SCV-008 Jan 16.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 17:45	6902	0.0018	511	536	95.10	97.50	145	09:31
YAM 5 (Yet Another Mission 5) 2023-001BV 55076						in space
Small satellite from Loft Orbital Solutions - unspecified payload. Released from launch vehicle at L +01:20:42
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 17:48	6905	0.0015	516	537	95.17	97.50	164	09:30
Gama Alpha 2023-001CD 55084						in space
6U Cubesat from NanoAvioniccs carrying a solar sail from the Gama company to demonstrate its use as a propulsion system. Released from launch vehicle at L +01:00:00.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 19:17	6903	0.0016	514	537	95.14	97.50	156	09:31
Kleos Observer Mission 1 (KSF-3a) 2023-001CF 55086						in space
6U Cubesat - one of four satellites orbiting together, designed to observe maritime activity, particularly of shipping in strategic areas not using AIS. Carries radio receivers to monitor nautical radio bands. Satellite built by GomSpace in Denmark for Luxemburg company Kleos Space. Released from launch vehicle at L +01:01:11. One of four Kleos satellites carried by Sherpa LTE-1, all aimed at similar orbits to fly in formation. All have been confirmed operational.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 19:16	6903	0.0017	513	536	95.13	97.50	159	09:31
Milspace 2 - Huygens 2023-001CN 55093						in space
6U Cubesat in joint military project between The Netherlands Norway to detect and pinpoint the source of radar transmissions from the Earth's surface. One of a pair of satellites launched on the Transporter 6 mission. Released from launch vehicle at L +01:00:18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 19:14	6903	0.0017	513	536	95.12	97.50	156	09:31
SpaceBEE 156 2023-001CU 55099						Re-entered - 2024 Sep 15 Life 621 days
0.25U Cubesat from Swarm Technologies to provide a two-way communications system from LEO as part of a 150 satellite constellation. To aid tracking,the satellite carries a radar retro-reflector. It also carries a GPS receiver to help determine its location.Released from launch vehicle at L +01:02:07. One of twelve SpaceBEE satellites carried on this launch. All were aimed at similar orbits. All are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 19:13	6902	0.0017	512	536	95.11	97.50	157	09:31
KuwaitSat-1 2023-001CY 55103						in space
2U Cubesat from Kuwait University, equipped with an imaging payload to be used to determine the satellite's attitude in space. Released from launch vehicle at L +00:58:24.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 18, 19:13	6903	0.0018	512	537	95.12	97.51	156	09:31
Sharjah Sat 1 2023-001CZ 55104						in space
3U Cubesat from Sharjah Academy for Astronomy, Space Sciences and Technology (SAASST) of the University of Sharjah. Carries instruments to study the Sun and space weather. Released from SCV-008 Jan 17.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 24, 18:28	6909	0.0013	522	539	95.24	97.50	156	09:30
Futura SM1 2023-001DA 55105						Re-entered - 2023 May 4 Life 121 days
3U Cubesat from Italian company NPC Spacemind with a payload consisting of a space sail and an on-board computer developed by partner Apogeo Space. Released from ION SCV-008 Jan 18. The sail caused rapid orbit decay.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 25, 03:41	6896	0.0014	508	528	94.99	97.51	131	09:30
Futura SM3 2023-001DB 55106						Re-entered - 2023 Apr 19 Life 106 days
6U Cubesat from Italian company NPC Spacemind. Payload includes the company's 'Artica' space sail. Released from ION SCV-008 Jan 18.The sail caused rapid orbit decay.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 24, 19:55	6902	0.0015	514	535	95.12	97.51	147	09:30
Kelpie 1 (AAC-AIS-SAT-1) 2023-001DC 55107						in space
3U Cubesat from AAC Clyde Space built in collaboration with ORBCOMM. It carries a multi-channel AIS receiver for relating short messages from ship to shore via ORBCOMM's satellite comms network. Released from ION SCV-007 Mar 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 2, 13:00	7024	0.0013	637	655	97.64	98.07	226
Zeus 1 2023-001DD 55108						Re-entered - 2025 Feb 11 Life 770 days
3U Cubesat from Qosmosys of Singapore to demonstrate its satellite platform. Also carries copies of fifty pieces of artwork. Released from Vigoride 5 on May 11 at around 00:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 May 19, 03:57	6899	0.0012	513	529	95.06	97.48	114	09:30
Astrocast 18 (Astrocast 0402) 2023-001DE 55109						in space
3U Cubesat in a planned eighty satellite constellation to provide communications for internet-connected devices. Released from ION SCV-008 early-December.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 12, 19:35	6917	0.0005	535	542	95.41	97.63	183
Astrocast 17 (Astrocast 0401) 2023-001DF 55110						in space
3U Cubesat in a planned eighty satellite constellation to provide communications for internet-connected devices. Released from ION SCV-008 early-December.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 12, 16:46	6915	0.0013	528	546	95.39	97.63	135
Astrocast 19 (Astrocast 0403) 2023-001DG 55111						in space
3U Cubesat in a planned eighty satellite constellation to provide communications for internet-connected devices. Released from ION SCV-008, possibly as late as 2021 January.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 Jan 17, 17:38	6916	0.0009	532	544	95.40	97.62	154
Astrocast 20 (Astrocast 0404) 2023-001DH 55112						in space
3U Cubesat in a planned eighty satellite constellation to provide communications for internet-connected devices. Released from ION SCV-008, possibly as late as 2021 January.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 Jan 17, 16:58	6915	0.0011	529	544	95.37	97.63	170
BDSat 2 2023-001xx						in space
1U Cubesat from the Czech Republic testing space environment sensors and carrying an amateur radio system. Launched to replace the failed BDSat 1 (52175/2022-33U). Released from launch vehicle at L +00:58:34. Catalogue Number and Designation based on amateur observations and are to be confirmed.
Orbit parameters awaited
Chimera LEO 1 2023-001xx						in space
Satellite carrier from Epic Aerospace - holding a single unidentified satellite. Released from launch vehicle at L +01:28:54 but probably failed to activate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6904	0.0015	516	537	95.15	97.51	167	09:31
Endurosat Platform 2 (SharedSat 2211) 2023-001xx						in space
6U Cubesat - carries several individual payloads. Released from launch vehicle at L +00:58:35.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6904	0.0015	516	537	95.15	97.51	167	09:31
Guardian-alpha 2023-001xx						in space
3U Cubesat from Orbital Astronautics, a UK/New Zealand base company - payload details awaited. Released from launch vehicle at L +01:05:23. May have failed to activate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6904	0.0015	516	537	95.15	97.51	167	09:31
PolyITAN-HP-30 2023-001xx						in space
1U Cubesat from the National Technical University of Ukraine carrying a demonstrator for the use of heat pipes for thermal regulation. Released from launch vehicle at L +01:05:12. May have failed to activate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6904	0.0015	516	537	95.15	97.51	167	09:31
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jan 3 Life <1 day
Launched Transporter 6, multisatellite mission. Caused to re-enter above the Indian Ocean at about 17:15 UTC. The following satellites failed to be released and re-entered together with the rocket stage: ICEYE X-22 - Small satellite fitted with a sythetic aperture radar for Earth surface imaging, RROCI (Rapid Revisit Optical Cloud Imager) - 12U Cubesat, demonstrator of an imaging sensor to identify cloud types and assist in weather forecasting for active military troops on the ground.
Not Catalogued - orbit parameters unavailable

2023-I01 JEM Small Satellite Orbital Deployer International Space Station						2023 Jan 6, 08:02
SuryaSat 1998-067UY 55181						Re-entered - 2023 May 9 Life 123 days
1U Cubesat - student developed satellite from Surya University, Indonesia.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 10, 17:26	6792	0.0004	411	416	92.84	51.64	216

2023-I02 JEM Small Satellite Orbital Deployer International Space Station						2023 Jan 6, 09:00
OPTIMAL 1 1998-067VZ 55183						Re-entered - 2023 Aug 22 Life 228 days
3U Cubesat jointly developed by ArkEdge Space Inc and the University of Fukui, Japan. Carries an imaging system, an onboard processor for preparing data for transmission and a propulsion system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 10, 17:25	6792	0.0005	410	417	92.84	51.64	288

2023-I03 JEM Small Satellite Orbital Deployer International Space Station						2023 Jan 6, 09:32
HSKSat 1 1998-067UZ 55182						Re-entered - 2023 Jul 11 Life 186 days
3U Cubesat for the HSK radio club of Japan, providing high-speed data links for amateur radio users.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 10, 17:25	6792	0.0003	412	416	92.84	51.64	200

2023-002 CZ 7A (Y-5) Wenchang Space Centre						2023 Jan 8, 22:00
Shijian 23 (Practice 23) 2023-002A 55131						in space
Test satellite described as "…scientific testing, technical verification". May be a satellite retrieval & disposal mission similar to Shijian 21 (49330/2021-094A) or may be a servicing/refuelling mission for Tianlian 1-03. Drifted around the GEO belt then settled close to Tianlian 1-03 (38730/2012-040A) at 20°.4 east on February 28. Started to drift away March 18 and stopped near 19°.8 east on March 29. Commenced move back towards Tianlian on Apr 15 but continued past it and started to drift eastwards away from it. Stopped near 174° east 2022 Oct 11.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Jan 9, 08:07	24379	0.7298	209	35793	631.36	16.42	180
2023 Jan 9, 14:27	24719	0.7063	883	35799	644.63	14.31	180
2023 Jan 17, 15:46	42431	0.0001	36050	36057	1449.74	0.50	288
2023 Jan 17, 19:16	42384	0.0012	35956	36055	1447.32	0.50	229
2023 Jan 18, 15:03	42335	0.0032	35823	36092	1444.81	0.50	239
2023 Jan 23, 16:46	42411	0.0015	35968	36096	1448.67	0.52	233
2023 Jan 29, 23:28	42362	0.0004	35967	36000	1446.18	0.53	246
2023 Feb 1, 10:44	42329	0.0004	35934	35967	1444.48	0.54	51
2023 Feb 6, 10:42	42296	0.0010	35876	35960	1442.81	0.55	64
2023 Feb 7, 21:15	42301	0.0009	35885	35960	1443.06	0.55	59
2023 Feb 8, 10:30	42351	0.0005	35952	35993	1445.60	0.56	309
2023 Feb 8, 21:29	42489	0.0029	35987	36235	1452.69	0.56	13
2023 Feb 14, 16:59	42489	0.0030	35986	36237	1452.72	0.57	13
2023 Feb 19, 09:44	42512	0.0024	36031	36237	1453.87	0.58	14
2023 Feb 27, 14:16	42211	0.0013	35777	35889	1438.48	0.61	6	20°.3 E
2023 Feb 28, 12:54	42165	0.0005	35764	35809	1436.10	0.61	340	20°.2 E
2023 Mar 18, 02:32	42191	0.0011	35765	35860	1437.43	0.65	303	20°.2 E
2023 Mar 19, 20:14	42177	0.0012	35749	35849	1436.73	0.66	287	19°.9 E
2023 Mar 22, 20:05	42167	0.0008	35754	35824	1436.22	0.67	296	19°.5 E
2023 Mar 23, 09:29	42162	0.0008	35748	35818	1435.93	0.67	286	19°.6 E
2023 Mar 29, 20:44	42165	0.0007	35756	35818	1436.12	0.68	286	19°.8 E
2023 Apr 14, 15:40	42165	0.0007	35757	35817	1436.12	0.72	290	19°.8 E
2023 Apr 15, 04:20	42157	0.0009	35742	35817	1435.72	0.73	290	19°.8 E
2023 Apr 16, 06:31	42141	0.0001	35758	35768	1434.90	0.73	121	20°.1 E
2023 Apr 16, 22:05	42121	0.0001	35741	35746	1433.88	0.73	276	20°.6 E
2023 Jun 8, 13:47	42073	0.0000	35694	35696	1431.40	0.87	144	53°.8 E
2023 Jun 9, 21:42	41977	0.0023	35503	35695	1426.53	0.87	77
2023 Jul 2, 15:44	42095	0.0002	35706	35726	1432.51	0.93	85	106°.0 E
2023 Jul 10, 21:23	42116	0.0000	35737	35739	1433.60	0.95	301	113°.1 E
2023 Oct 4, 22:52	42114	0.0006	35711	35761	1433.50	1.17	151	168°.2 E
2023 Oct 5, 14:13	42094	0.0009	35680	35752	1432.48	1.17	119	168°.7 E
2023 Oct 11, 18:07	42161	0.0008	35750	35815	1435.90	1.19	300	174°.2 E
2023 Oct 12, 15:22	42197	0.0001	35815	35823	1437.75	1.18	108	174°.0 E
2023 Oct 19, 12:42	42180	0.0003	35789	35815	1436.89	1.20	309	171°.3 E
2023 Oct 19, 19:31	42165	0.0001	35784	35790	1436.11	1.20	90	171°.3 E
2023 Dec 4, 22:41	42210	0.0000	35831	35833	1438.42	1.33	15	171°.1 E
unidentified object 2023-002C 55180						in space
Separated from Shijian 23 on January 16 at around 21:30 UTC. A similar item accompanied Shijian 21 (49330/2021-094A) and was used as a practice rendezvous target. May be the propulsion stage that transferred Shijian 23 to GEO drift orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Jan 19, 06:22	42422	0.0002	36036	36051	1449.24	0.50	291
CZ 7A fourth stage 2023-002B 55132						in space
Launched Shijian 23. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 9, 08:02	23516	0.7225	149	34126	598.13	16.44	179

2023-003 Ceres 1 (Gushenxing 1 Y-5) Jiuquan Space Centre						2023 Jan 9, 05:04
Science & Technology 1 2023-003A 55133						in space
Payload includes an Earth imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 9, 20:47	6881	0.0012	495	511	94.68	97.27	293	11:23
2023 Jan 11, 23:37	6887	0.0008	503	514	94.79	97.27	255	11:23
2023 Jan 13, 05:18	6892	0.0006	510	519	94.91	97.27	249	11:22
2023 Mar 7, 04:51	6884	0.0006	502	511	94.74	97.27	64	11:17
2023 Mar 10, 11:42	6901	0.0004	520	526	95.09	97.26	178	11:17
2023 Mar 17, 07:25	6905	0.0005	524	530	95.17	97.26	40	11:16
Tianmu 1-01 2023-003C 55135						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 9, 13:02	6881	0.0012	494	511	94.67	97.28	296	11:23
2023 Jul 19, 19:38	6881	0.0007	498	507	94.67	97.26	351	11:08
Tianmu 1-02 2023-003E 55137						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jan 9, 20:44	6880	0.0012	494	511	94.66	97.27	298	11:23
2023 Jul 19, 20:25	6881	0.0008	497	509	94.67	97.26	320	11:07
Nantong Zhongxue 2023-003xx						in space
Student satellite from Nantong Middle School, China.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 9, 11:28	6880	0.0014	492	511	94.65	97.27	294
Tianqi 13 2023-003xx						in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 9, 11:28	6880	0.0014	492	511	94.65	97.27	294
Ceres 1 fourth stage uncatalogued						Re-entered - 2023 Jan 9 Life <1 day
Launched cluster of five satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-004 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Jan 9, 22:50
OneWeb 0532 2023-004A 55140						in space
Broadband distribution satellite for the UK company OneWeb. One of 40 similar satellites carried on this launch, all initially in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 10, 05:45	6983	0.0002	603	606	96.78	86.50	128
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jan 9 Life <1 day
Launched forty OneWeb satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-F01 - failed to reach orbit LauncherOne Boeing 747, Atlantic Ocean SW of Ireland						2023 Jan 9, 23:10
Nine small satellites
Carried on first Virgin Orbit launch from Europe. Carrier aircraft took off from Newquay, Cornwall UK. Lost when launcher second stage failed to perform to expectation.

2023-F02 - failed to reach orbit ABL RS1 Kodiak Launch Centre, Alaska						2023 Jan 10, 23:27
Varisat
6U Cubesat - one of a pair of satellites owned by Varisat LLC on first orbital launch attempt by ABL Space Systems. Carries a payload to test inter-satellite radio communications. Aimed at 200 - 350 km, 87° orbit. Destroyed when launch vehicle first stage shut down a few seconds after lift-off and it fell back onto the launch pad.
Varisat
6U Cubesat - one of a pair of satellites owned by Varisat LLC on first orbital launch attempt by ABL Space Systems. Carries a payload to test inter-satellite radio communications. Aimed at 200 - 350 km, 87° orbit. Destroyed when launch vehicle first stage shut down a few seconds after lift-off and it fell back onto the launch pad.

2023-005 CZ 2C Xichang Space Centre						2023 Jan 12, 18:10
APStar 6E (Asia Pacific Satellite 6E) 2023-005A 55239						in space
Commercial comsat owned by APT Mobile SatCom to provide to provide high-bandwidth satellite broadband telecommunications services for airborne, shipborne and other mobile applications. Launched initially to low orbit but main engine of attached propulsion unit failed to fire so early orbit raising to GTO used repeated firings of the module's low-thrust engines until Jan 21. The propulsion unit separated from Apstar Jan 23. Orbit raised continued slowly using Apstar's onboard electric propulsion system. For more than eight from 2023 March to November, Space-Track issued no orbit data because of human error in cataloguing it. A further error by Space-Track 2023 December resulted in data again ceasing to be published with nothing further until 2024 June when it 're-appeared' at its GEO location.. Expected location - 134° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Jan 13, 08:12	6813	0.0303	229	641	93.28	28.51	94
2023 Jan 17, 12:38	7895	0.1015	716	2318	116.36	28.50	104
2023 Jan 19, 03:39	8795	0.1873	770	4064	136.82	28.23	117
2023 Jan 21, 10:42	10289	0.2979	846	6977	173.12	28.51	121
2023 Jan 28, 07:15	10634	0.2677	1409	7103	181.89	28.71	145
2023 Feb 5, 02:31	11063	0.2412	2016	7354	193.01	28.51	161
2023 Feb 12, 05:26	11297	0.2298	2323	7515	199.16	28.53	176
2023 Feb 19, 04:48	11997	0.2093	3107	8130	217.95	28.46	188
2023 Feb 26, 00:23	12429	0.1868	3729	8372	229.82	28.46	198
2023 Mar 5, 04:54	13260	0.1887	4380	9383	253.26	28.66	208
2023 Mar 11, 13:49	13591	0.1616	5017	9409	262.82	28.53	213
2023 Mar 17, 04:27	13983	0.1606	5360	9850	274.26	28.80	226
2023 Nov 21, 15:28	32276	0.0958	22806	28991	961.80	13.78	255
2023 Nov 27, 14:58	32506	0.0923	23127	29128	972.08	13.50	255
2024 Jun 10, 16:06	42166	0.0009	35750	35826	1436.16	0.08	241	135°.5 E
CZ 2C second stage 2023-005B 55240						Re-entered - 2023 Feb 7 Life 26 days
Launched APStar 6E and attached propulsion module.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 13, 02:28	6723	0.0207	206	485	91.44	28.51	112
APStar 6E propulsion module 2023-005C 55447						in space
Intended to propel APStar 6E towards GEO. A fault prevented use of its main engine nozzle but, up to January 23, orbit raising continued by use of its low-thrust nozzles. Reportedly separated from APStar 6E January 23 at 13:31 UTC. Its first measured orbit indicates that perigee was lowered after it departed from Apstar 6E.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 1, 06:39	10923	0.2303	2030	7060	189.35	28.66	154

2023-006 CZ 2D Jiuquan Space Centre						2023 Jan 13, 07:00
Shiyan 22A (Test 22A) 2023-006A 55242						Re-entered - 2024 Jun 28 Life 532 days
Small satellite carrying an unspecified demonstration payload, one of a pair carried on the same launch as Yaogan 37. Catalogue Number, Designation and orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 13, 15:01	6894	0.0011	508	523	94.94	43.20	287
Shiyan 22B (Test 22B) 2023-006B 55243						in space
Small satellite carrying an unspecified demonstration payload, one of a pair carried on the same launch as Yaogan 37. Catalogue Number, Designation and orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 13, 15:01	6894	0.0010	509	523	94.94	43.20	287
Yaogan 37 2023-006C 55244						in space
Chinese photographic or electronic reconnaissance satellite. Catalogue Number, Designation and orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 13, 16:33	6896	0.0007	513	523	94.98	43.20	270
2023 Feb 13, 10:58	6894	0.0004	513	519	94.94	43.20	110
CZ 2D second stage 2023-006D 55245						Re-entered - 2024 Feb 17 Life 400 days
Launched Yaogan 37, Shiyan 22A and Shiyan 22B. Catalogue Number, Designation and orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 13, 16:32	6896	0.0008	512	523	94.98	43.20	277

2023-007 CZ 2D Taiyuan Space Centre						2023 Jan 15, 03:14
BUPT 1 2023-007xx						in space
Communications test/demonstrator satellite from the Beijing University of Posts and Telecommunications.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Golden Bauhinia 3 (Jinzijing 3) 2023-007xx						in space
Satellite from the Hong Kong Aerospace Technology Group for a constellation of 165 LEO remote sensing satellites equipped with optical and radar imagers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Golden Bauhinia 4 (Jinzijing 4) 2023-007xx						in space
Satellite from the Hong Kong Aerospace Technology Group for a constellation of 165 LEO remote sensing satellites equipped with optical and radar imagers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Golden Bauhinia 6 (Jinzijing 6) 2023-007xx						in space
Satellite from the Hong Kong Aerospace Technology Group for a constellation of 165 LEO remote sensing satellites equipped with optical and radar imagers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Jilin-1 High Resolution 03D 34 (Jilin-1 GF3D 34) 2023-007xx						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Jilin-1 MF02 2023-007xx						in space
Imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Jilin-1 MF03 2023-007xx						in space
Imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Jilin-1 MF04 2023-007xx						in space
Imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Luojia-3 01 (Shuangqing 1) 2023-007xx						in space
Small satellite equipped with an imaging system and an intelligent processing system to prepare data before transmission to the ground. Also equipped with a (probably laser) communications system to provide links to other satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Qilu 2 2023-007xx						in space
Small satellite equipped with an Earth imaging system. Also carries a laser communications system for satellite to satellite links with the earlier-launched Qilu 1 (2021-033 launch).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Qilu 3 2023-007xx						in space
Small satellite equipped with an Earth imaging system. Also carries a laser communications system for satellite to satellite links with the earlier-launched Qilu 1 (2021-033 launch).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Tianzhi 2 2023-007xx						in space
Software defined satellite from the Chinese Academy of Sciences, carrying an Earth imaging system. The software is capable of modifying how the imaging system operates and processing data onboard before transmitting it to the ground.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
TJ Hai He 01 2023-007xx						in space
Small satellite with an infrared detector, unclear whether it's for Earth observation or for astronomy.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
Wo Fu Man 01 2023-007xx						in space
Small satellite with an infrared detector, unclear whether it's for Earth observation or for astronomy.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6867	0.0010	482	496	94.39	97.38	283	10:21
CZ 2D second stage uncatalogued						Re-entered - 2023 Jan 15 Life <1 day
Launched fourteen small satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-008 Falcon Heavy Kennedy Space Center						2023 Jan 15, 22:56
USA 342 (Continuous Broadcast Augmenting SATCOM 2, CBAS 2) 2023-008A 55263						in space
Primary payload of the USSF-67 mission. US military comsat to supplement the fixed comsat network and provide specialised comms to US armed forces in the field. Separated from launch vehicle Jan 16, ~05:00 UTC. Aimed at an unannounced geosynchronous location. The first orbit listed is based on information provided by Space-Track and SpaceX.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Jan 16, 05:00	41603	0.0006	35199	35251	1407.50	0.06	0
2023 Jan 18, 21:30	41635	0.0002	35248	35265	1409.11	0.05	262
2023 Jan 31, 12:51	41813	0.0003	35420	35449	1418.15	0.04	6
2023 Feb 3, 13:41	41934	0.0009	35520	35592	1424.35	0.02	60
2023 Feb 6, 12:00	42131	0.0003	35740	35766	1434.38	0.01	164	131°.2 W
2023 Feb 9, 23:58	42164	0.0002	35777	35794	1436.05	0.02	20	130°.5 W
LDPE 3A (Long Duration Propulsive Evolved Expendable Launch Vehicle Secondary Payload Adapter) 2023-008B 55264						in space
Secondary satellite carried on the USSF-67 mission. Platform built by Northrop Grumman carrying five USSF payloads and possible payloads from other US government/military agencies. Payloads include two small satellites - WASSAT and Catcher. Separated from launch vehicle Jan 16, ~05:00 UTC. Orbital data not available for the period prior to March 28 but the initial orbit parameters can be derived from published Space-Track data.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	41628	0.0000	35248	35251	1408.74	0.20	262
2023 Mar 28, 14:55	41972	0.0001	35592	35597	1426.29	0.10	132
2023 Apr 19, 20:34	42351	0.0001	35970	35976	1445.63	0.16	318
2023 May 21, 21:17	42279	0.0001	35899	35903	1441.95	0.24	77
Falcon 9 third stage 2023-008C 55265						in space
Launched USSF-67 mission.
Geosynchronous Drift Orbit - parameters awaited

2023-009 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Jan 18, 12:24
USA 343 (GPS IIIA SV06) 2023-009A 55268						in space
Block 3 GPS Navsat. Released from launch vehicle at 13:53 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 18, 15:07	16655	0.5936	391	20162	356.51	55.01	270
2023 Jan 31, 17:31	26559	0.0008	20160	20202	717.92	55.08	100
Falcon 9 second stage uncatalogued						in space
Launched USA 343. Caused to re-enter after releasing satellite, about seven hours or 1.5 circuits of the Earth.
Not Catalogued - orbit parameters unavailable

2023-010 Falcon 9 Block 5 (Starlink Group 02-04) Vandenberg Space Force Base						2023 Jan 19, 15:43
Starlink 5277 2023-010A 55269						in space
One member of a simultaneously-launched cluster of fifty one LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 16:13 UTC. All satellites were injected initially into similar orbits at 200-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 24, 16:00	6668	0.0039	264	316	90.32	70.00	164
Falcon 9 second stage uncatalogued						in space
Launched fifty one Starlink satellites. Caused to re-enter after releasing satellites
Not Catalogued - orbit parameters unavailable

2023-011 Electron (Virginia Is For Launch Lovers) Mid Atlantic Regional Space Port, Wallops Island						2023 Jan 24, 23:00
Hawk 6B (Cluster 6 #2) 2023-011A 55324						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. Separated from launch vehicle at 23:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 25, 10:32	6929	0.0003	549	553	95.67	40.51	253
Hawk 6C (Cluster 6 #3) 2023-011C 55326						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. Separated from launch vehicle at 23:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 25, 10:29	6928	0.0001	550	551	95.65	40.51	212
Hawk 6A (Cluster 6 #1) 2023-011D 55327						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. Separated from launch vehicle at 23:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 25, 10:29	6928	0.0003	547	552	95.64	40.51	220
Electron third stage (kick stage) 2023-011B 55325						in space
Launched 3x Hawk satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 25, 10:30	6929	0.0002	549	552	95.66	40.51	196
Electron second stage 2023-011E 55328						Re-entered - 2023 May 27 Life 123 days
Launched 3x Hawk satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 25, 10:14	6822	0.0174	325	563	93.46	40.53	125

2023-012 H-IIA 202 (F-46) Tanegashima Space Centre						2023 Jan 26, 01:50
IGS 15 (IGS Radar 7) 2023-012A 55329						in space
Information Gathering Satellite - Japanese government/military radar imaging reconnaissance satellite. Orbit info based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Apr 10, 23:36	6857	0.0002	477	480	94.17	97.27	248	10:40
H-IIA upper stage 2023-012B 55330						Re-entered - 2024 Oct 7 Life 620 days
Launched IGS 15. Orbit info based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 11, 01:20	6907	0.0075	477	581	95.21	97.66	139

2023-013 Falcon 9 Block 5 (Starlink Group 05-02) Cape Canaveral Space Force Station						2023 Jan 26, 09:32
Starlink 5492 2023-013A 55331						in space
One member of a simultaneously-launched cluster of fifty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 09:50 UTC. All satellites were injected initially into similar orbits at 200-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 31, 18:00	6671	0.0044	264	322	90.38	43.00	191
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jan 26 Life <1 day
Launched fifty six Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-014 Falcon 9 Block 5 (Starlink Group 02-06) Vandenberg Space Force Base						2023 Jan 31, 16:15
Starlink 5077 2023-014A 55391						Re-entered - 2025 May 2 Life 822 days
One member of a simultaneously-launched cluster of forty nine LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 17:32 UTC. All satellites were injected initially into similar orbits at 200-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 7, 16:00	6730	0.0003	350	354	91.58	70.01	272
ION SCV-009 (Eclectic Elena) 2023-014BC 55441						Re-entered - 2024 Feb 14 Life 379 days
Satellite Carrier Vehicle built by D-Orbit, carrying four hosted payloads. Released from launch vehicle at 17:12 UTC. Hosted payloads: ADEO-N3 - an autonomous braking sail, with area 5 sq metres, developed by Munich-based space company HPS designed to help deorbit satellites in LEO (up to 900 km), NEA Payload Release Ring (PRR) - from MEA Electronics, a subsidiary of the Ensign-Bickford Aerospace & Defense Company, as a demonstrator of its system for deployment of payloads/spacecraft from a launch vehicle or orbital transfer vehicle: simulated satellite (55446/2023-014BH) released February 8. Bunny - an onboard computer developed in-house by the students of the Spacecraft Team of the Swiss Institute École Polytechnique Fédérale de Lausanne (EPFL), SD-1 - a memorial payload from StardustMe consisting of a batch of aluminum machined capsules, each carrying one gramme of human cremated ashes from an inividual.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 7, 14:53	6708	0.0008	324	335	91.12	70.01	246
2023 Feb 10, 02:07	6705	0.0008	322	332	91.07	70.01	241
2023 Feb 10, 14:16	6717	0.0021	325	353	91.31	70.01	318
2023 Feb 13, 03:22	6729	0.0034	328	373	91.55	70.01	328
2023 Feb 14, 20:56	6739	0.0050	327	395	91.77	70.01	330
2023 Mar 17, 09:52	6772	0.0002	393	396	92.44	70.01	286
NEA simulated payload mass 2023-014BH 55446						Re-entered - 2023 Jun 10 Life 130 days
Separated from the NEA Electronics Payload Release Ring hosted aboard ION SCV-009 on February 8 - as a test of its mechanism. NEA is owned by the Ensign-Bickford Aerospace & Defense Company (EBAD).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 22, 11:35	6701	0.0007	318	327	90.97	70.01	217
Falcon 9 second stage uncatalogued						in space
Launched forty nine Starlink satellites and D-Orbit's transfer vehicle ION SCV009. Caused to re-enter above the Atlantic/Indian Ocean boundary after releasing satellites around 18:15-18:30 UTC.
Not Catalogued - orbit parameters unavailable

2023-015 Falcon 9 Block 5 (Starlink Group 05-03) Kennedy Space Center						2023 Feb 2, 07:58
Starlink 5699 2023-015A 55449						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 09:02 UTC. All satellites expected to be injected initially into similar orbits at about 330 km altitude.
Orbit parameters awaited
Falcon 9 upper stage uncatalogued						Re-entered - 2023 Feb 2 Life <1 day
Launched fifty three Starlink satellites. Expected to be caused to re-enter above the southern Indian Ocean at about 10:05 UTC.
Not Catalogued - orbit parameters unavailable

2023-016 Proton-M + Blok DM3 Baikonur Cosmodrome						2023 Feb 5, 09:12
Elektro-L №4 2023-016A 55506						in space
Second generation Russian geosynchronous metsat providing a multispectral image of the complete visible hemisphere every 30 minutes with the interval increased to 15 minutes to cope with emergencies. The satellite also carries a COSPAS-SARSAT search and rescue system receiver. Separated from launch vehicle at 15:40 UTC. Expected location - 165°.8 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Feb 6, 17:42	41819	0.0015	35379	35502	1418.45	0.56	239
2023 Feb 21, 17:37	42041	0.0037	35507	35820	1429.79	0.52	50	150°.7 E
2023 Mar 3, 02:17	42150	0.0012	35723	35821	1435.34	0.50	51	164°.8 E
2023 Mar 7, 01:59	42162	0.0009	35746	35822	1435.95	0.49	54	165°.7 E
2023 Mar 8, 12:40	42164	0.0008	35752	35820	1436.07	0.49	51	165°.7 E
2023 Apr 6, 00:00	42159	0.0004	35764	35797	1435.79	0.42	56	165°.7 E
2023 Apr 7, 23:52	42165	0.0003	35776	35798	1436.12	0.41	42	165°.9 E
Blok DM-03 rocket stage 2023-016B 55507						in space
Launched Elektro-L №4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 6, 18:04	41357	0.0098	34576	35382	1395.04	0.44	29

2023-017 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Feb 7, 01:32
Amazonas Nexus 2023-017A 55508						in space
High throughput serving North, South and Central America, and the Atlantic Ocean region - supplementing the service through Amazonas 2 (35942/2009-054A). Released from launch vehicle at 02:07 UTC. Expected location - 61° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Feb 7, 21:36	36281	0.8149	338	59467	1146.25	25.05	178
2023 Feb 24, 07:20	39983	0.7745	2638	64572	1326.08	18.90	183
2023 Feb 27, 02:09	40854	0.7649	3226	65726	1369.67	17.60	184
2023 Feb 28, 00:48	41183	0.7613	3452	66157	1386.22	17.14	184
2023 Mar 7, 18:00	43699	0.7370	5113	69529	1515.21	14.30	185
2023 Mar 15, 12:52	44559	0.6870	7569	68793	1560.15	11.34	187
2023 Mar 22, 01:54	45045	0.6403	9823	67510	1585.72	9.03	187
2023 Mar 29, 19:57	45398	0.5819	12603	65437	1604.40	7.01	188
2023 Apr 5, 01:37	45080	0.5326	14693	62710	1587.58	5.84	189
2023 Apr 13, 09:36	42660	0.4972	15073	57491	1461.48	4.41	184
2023 Apr 19, 00:41	45568	0.4061	20686	57694	1613.45	3.41	189
2023 Apr 25, 19:12	45212	0.3504	22990	54676	1594.53	2.71	188
2023 May 1, 06:43	44832	0.2860	25633	51275	1574.51	2.07	189
2023 May 8, 18:16	44112	0.2074	28586	46882	1536.71	1.43	190
2023 May 15, 14:32	43441	0.1319	31332	42794	1501.79	0.91	190
2023 May 30, 18:54	42163	0.0001	35782	35789	1436.03	0.04	26	59°.0 W
2023 Jun 8, 09:32	42165	0.0001	35784	35790	1436.12	0.03	72	58°.9 W
2023 Jul 3, 16:36	42166	0.0000	35788	35789	1436.18	0.03	194	59°.0 W
2023 Jul 4, 11:31	42193	0.0006	35788	35841	1437.54	0.03	215	59°.2 W
2023 Jul 7, 08:24	42170	0.0008	35760	35824	1436.38	0.03	16	61°.0 W
Falcon 9 second stage 2023-017B 55509						Re-entered - 2024 Dec 11 Life 673 days
Launched Amazonas Nexus.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 7, 21:36	36377	0.8154	336	59661	1150.78	25.06	178

2023-018 Soyuz-2.1a Baikonur Cosmodrome						2023 Feb 9, 06:15
Progress MS-22 (Progress 7K-MS №452) 2023-018A 55560						Re-entered - 2023 Aug 21 Life 193 days
Supplies to ISS. Docked with aft port of Zvezda Feb 11 at 08:45 UTC. Initial orbit was similar to rocket stage. Undocked August 20 at 23:49 UTC. Retrofire August 21 at 02:58 UTC above central Asia led to destructive re-entry with any surviving debris hitting the surface of the southern Pacific Ocean around 03:50 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 9, 15:01	6671	0.0033	271	314	90.37	51.64	322
2023 Feb 10, 22:37	6674	0.0031	275	316	90.43	51.65	326
2023 Feb 11, 12:43	6795	0.0009	411	423	92.91	51.64	339
2023 Aug 20, 23:59	6796	0.0004	416	421	92.93	51.64	331
Soyuz third stage 2023-018B 55561						Re-entered - 2023 Feb 11 Life 2 days
Launched Progress MS-22.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 9, 10:49	6580	0.0026	185	219	88.53	51.66	74

2023-019 SSLV + VTM (SSLV D-2) Satish Dhawan Space Centre						2023 Feb 10, 03:48
EOS 07 (Earth Observation Satellite 7) 2023-019A 55562						Re-entered - 2025 Jan 1 Life 691 days
Experimental optical remote sensing satellie from India developed in a short space of time to demonstrate rapid launch on demand ability. Replacement for EOS 2 - lost in a 2022 launch failure. Separated from launch vehicle at 15:01 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 10, 11:31	6823	0.0008	439	450	93.48	37.18	320
AzaadiSat 2 2023-019B 55563						Re-entered - 2023 Dec 5 Life 298 days
8U Cubesat - carrying multiple experiments provided by female students at schools across India under the 'Space Kidz India' initiative. Includes an amateur radio payload. Replaces an earlier satellite lost when its launch vehicle failed 2022. Separated from VTM at 15:03 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 11, 04:29	6819	0.0013	433	450	93.40	37.18	345
Janus 1 2023-019C 55564						Re-entered - 2023 Jun 29 Life 139 days
6U Cubesat from US company Antaris as a demonstrator of its software configured payload - includes a broadband messaging system, a laser communication system and a machine learning module. Separated from VTM at 15:02 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 15, 18:24	6818	0.0012	432	448	93.38	37.18	30
SSLV third stage 2023-019D 55565						Re-entered - 2023 Dec 21 Life 314 days
Launched EOS 07 and two other satellites. Perigee lowered after VTM separation then disintegrated later the same day.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 10, 09:23	6802	0.0041	397	452	93.06	37.19	339
VTM rocket stage (Velocity Trimming Module) 2023-019E 55566						Re-entered - 2024 May 15 Life 460 days
Launched EOS 07 and two other satellites. Conducted test manoeuvres after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6819	0.0009	435	447	93.40	37.20	344
2023 Feb 10, 06:30	6797	0.0047	387	451	92.95	37.19	340
2023 Feb 10, 14:01	6796	0.0049	385	451	92.94	37.20	342
2023 Feb 15, 12:59	6787	0.0046	378	440	92.75	37.20	28
2023 Feb 15, 20:48	6794	0.0050	382	450	92.89	37.90	55

2023-020 Falcon 9 Block 5 (Starlink Group 05-04) Cape Canaveral Space Force Station						2023 Feb 12, 05:10
Starlink 5749 2023-020A 55569						in space
One member of a simultaneously-launched cluster of fifty five LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:13 UTC. All satellites expected to be injected initially into similar orbits at about 250-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 14, 20:00	6699	0.0020	308	334	90.95	43.00	314
Falcon 9 second stage uncatalogued						Re-entered - 2023 Feb 12 Life <1 day
Launched fifty five Starlink satellites. Caused to re-enter above the Indian Ocean at about 07:15 UTC, after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-021 Falcon 9 Block 5 (Starlink Group 02-05) Vandenberg Space Force Base						2023 Feb 17, 19:12
Starlink 5484 2023-021A 55628						in space
One member of a simultaneously-launched cluster of fifty one LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at about 19:31 UTC. All satellites expected to be injected initially into similar orbits at about 250-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 22, 16:00	6668	0.0038	265	315	90.31	70.00	163
Falcon 9 second stage uncatalogued						Re-entered - 2023 Feb 17 Life <1 day
Launched fifty one Starlink satellites. Caused to re-enter after their release.
Not Catalogued - orbit parameters unavailable

2023-022 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Feb 18, 03:59
Inmarsat 6 F2 (GX-6B) 2023-022A 55683						in space
New generation, dual band, high capacity comsat providing services to the Indian Ocean region. Released from launch vehicle at 04:31 UTC. Orbit raising to GEO using near-continuous low thrust ceased 2023 August 15 and was followed by a statement from owner Viasat that there had been an onboard power failure. Expected location 28° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Feb 21, 23:07	27368	0.7528	387	41593	750.98	26.98	167
2023 Mar 4, 01:21	27404	0.7525	403	41649	752.47	26.87	172
2023 Mar 10, 22:15	27907	0.7443	759	42300	773.28	25.38	175
2023 Mar 20, 05:02	28664	0.7315	1318	43254	804.94	23.29	178
2023 Mar 27, 16:12	29250	0.7188	1848	43895	829.73	21.79	181
2023 Apr 3, 18:05	29861	0.7081	2339	44627	855.89	20.23	183
2023 Apr 12, 15:40	30650	0.6936	3014	45529	890.02	18.42	185
2023 Apr 17, 15:52	31110	0.6836	3463	46000	910.13	17.47	187
2023 Apr 23, 18:44	31666	0.6723	3999	46577	934.65	16.54	188
2023 May 1, 15:57	32494	0.6557	4811	47421	971.54	14.91	190
2023 May 9, 19:54	33337	0.6385	5675	48242	1009.59	13.58	192
2023 May 15, 15:56	34442	0.6284	6420	49709	1060.22	12.87	193
2023 Jun 5, 07:12	36648	0.5842	8862	51678	1163.68	10.73	164
2023 Jun 12, 16:46	36791	0.5447	10373	50453	1170.50	8.81	199
2023 Jun 20, 02:32	36463	0.5475	10123	50048	1154.90	8.01	194
2023 Jun 27, 18:58	38150	0.4941	12922	50622	1235.97	7.13	202
2023 Jul 3, 15:11	38667	0.4721	14036	50542	1261.17	6.52	203
2023 Jul 10, 09:12	38019	0.4899	13017	50266	1229.60	5.20	213
2023 Jul 17, 01:44	39746	0.4223	16583	50152	1314.30	5.27	205
2023 Jul 26, 00:00	40566	0.3861	18525	49850	1355.19	4.67	208
2023 Jul 31, 17:53	41021	0.3624	19778	49508	1378.06	4.23	29
2023 Aug 7, 19:58	41563	0.3315	21408	48961	1405.45	3.73	31
2023 Aug 15, 13:53	41971	0.2984	23068	48117	1426.20	3.27	211
Falcon 9 second stage 2021-022B 55684						in space
Launched Inmarsat 6 F2.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 21, 22:11	27319	0.7585	219	41664	748.97	27.01	167

2023-023 CZ 3B Xichang Space Centre						2023 Feb 23, 11:49
Zhongxing 26 (Chinasat 26) 2023-023A 55686						in space
Communications satellite described as carrying high-quality voice, data and radio and TV transmissions and China's first high-throughput satellite with a capacity of more than 100 Gbps. Serves mainland China. Moved to geosynchronous drift orbit probably February 23 or February 24.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Feb 23, 14:18	24386	0.7292	226	35789	631.63	27.87	179
2023 Mar 3, 17:21	42186	0.0006	35780	35835	1437.17	0.02	77	125°.0 E
2023 Mar 5, 12:19	42164	0.0002	35775	35796	1436.05	0.03	11	125°.1 E
CZ 3B fourth stage 2023-023B 55687						in space
Launched Zhongxing 26.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 23, 16:52	23703	0.7227	195	34455	605.30	27.85	179

2023-024 Soyuz-2.1a Baikonur Cosmodrome						2023 Feb 24, 00:24
Soyuz MS-23 (Soyuz 11F732A48 № 754) 2023-024A 55688						Re-entered - 2023 Sep 27 Life 215 days Returned to Earth
Replacement crew vehicle to ISS as substitute for the damaged Soyuz MS-22. Separated from launch vehicle at 00:33 UTC. Docked with the Poisk module February 26 at 00:58 UTC, three minutes ahead of schedule. Undocked carrying original Soyuz MS-22 crew Apr 6 at 08:44:55 UTC and docked with the Prichal module at 09:21:44. The manoeuvre was to simplify access to open space for future EVAs. Undocked Sep 27 at 07:54 UTC carrying Soyuz MS-22 crew - Sergey Prokovyev (commander) and Dmitri Petelin (both Roscosmos) and Frank Rubio (NASA). Retro-fire at 09:24 UTC was followed by landing near Dzhezkazgan, Russia at 10:17 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 24, 04:58	6586	0.0022	193	222	88.65	51.64	71
2023 Feb 24, 10:33	6691	0.0023	298	328	90.79	51.64	344
2023 Feb 25, 08:02	6694	0.0026	298	333	90.84	51.63	348
2023 Feb 26, 13:41	6797	0.0006	415	422	92.94	51.64	31
2023 Sep 26, 07:30	6796	0.0006	414	422	92.92	51.64	63
Soyuz third stage 2023-024B 55689						Re-entered - 2023 Feb 26 Life 2 days
Launched Soyuz MS-23.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 24, 09:06	6584	0.0021	191	220	88.60	51.66	61

2023-025 CZ 2C Jiuquan Space Centre						2023 Feb 24, 04:01
Horus 1 2023-025A 55690						in space
Described as a remote sensing satellite but with no detail of the sensors carried, suggesting it is military/government in nature. Owned by Egypt and developed in co-operation with China using Chinese technology. The name of the god, Horus, can be translated as 'the one who is above'. One of a pair of satellites launched to matching LTDN, Horus 2 followed on March 13.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Feb 24, 11:56	6874	0.0011	488	503	94.53	97.47	248	10:21
2023 Mar 1, 11:47	6875	0.0010	490	504	94.55	97.47	223	10:21
2023 Mar 18, 15:11	6875	0.0015	486	507	94.55	97.47	158	10:22
2023 Mar 19, 21:06	6875	0.0013	488	506	94.56	97.47	141	10:22
2023 Nov 13, 04:06	6873	0.0007	490	500	94.52	97.45	91	10:30
CZ 2C second stage 2023-025B 55691						in space
Launched Horus 1. Orbit raised and inclination adjusted after satellite separation, possibly indicating that it carries instruments or sensors.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 24, 21:26	6892	0.0066	468	559	94.89	97.60	281

2023-026 Falcon 9 Block 5 (Starlink Group 06-01) Cape Canaveral Space Force Station						2023 Feb 27, 23:13
Starlink 30053 2023-026A 55695						Re-entered - 2024 Jul 27 Life 516 days
One member of a simultaneously-launched cluster of twenty one V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 19:41 UTC. All satellites expected to be injected initially into similar orbits at about 360 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 1, 22:00	6748	0.0002	368	371	91.93	43.01	272
Falcon 9 second stage uncatalogued						Re-entered - 2023 Feb 27 Life <1 day
Launched twenty one Starlink V2 satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-027 Falcon 9 Block 5 Kennedy Space Center						2023 Mar 2, 05:34
SpaceX Dragon Crew 6 (Dragon Endeavour flight #4) 2023-027A 55740						Re-entered - 2023 Sep 4 Life 186 days Returned to Earth
Crew flight to ISS provided by SpaceX under contract to NASA. Crew members - Steven Owen (commander) & Warren Hoburg (both NASA), Andrei Fedyaev (Roscosmos) and Sultan Alneyadi of the UAE. Separated from launch vehicle at 05:46 UTC. Docked with the upward facing port of the Harmony module March 3 at 06:40 UTC. Undocked, carrying original crew, September 3 at 23:05 UTC. Retro-fire September 4 at 03:24 UTC led to splashdown in the Atlantic Ocean off Jacksonville, Florida at 04:17 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 2, 05:58	6579	0.0014	192	210	88.51	51.65	1
2023 Mar 2, 12:53	6660	0.0107	211	353	90.16	51.65	222
2023 Mar 2, 17:33	6786	0.0003	406	410	92.73	51.65	183
2023 Mar 3, 01:16	6787	0.0005	405	413	92.74	51.65	189
2023 Mar 3, 14:18	6796	0.0006	414	422	92.93	51.64	51
Falcon 9 second stage uncatalogued						in space
Launched Crew Dragon 6. Caused to re-enter after releasing the spacecraft.
Not Catalogued - orbit parameters unavailable
Crew Dragon trunk module 2023-027B 57799						Re-entered - 2024 Feb 4 Life 339 days
Released from Dragon Crew 6 2023 September 4 at about 11:20 UTC prior to retro-fire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 6, 19:18	6783	0.0005	402	409	92.67	51.78	42

2023-028 Falcon 9 Block 5 (Starlink Group 02-07) Vandenberg Space Force Base						2023 Mar 3, 18:38
Starlink 5592 2023-028A 55741						in space
One member of a simultaneously-launched cluster of fifty one LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at about 18:59 UTC. All satellites expected to be injected initially into similar orbits at about 250-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 8, 20:00	6667	0.0033	267	312	90.30	70.00	165
Falcon 9 second stage uncatalogued						Re-entered - 2023 Mar 3 Life <1 day
Launched fifty one Starlink satellites. Caused to re-enter after their release.
Not Catalogued - orbit parameters unavailable

2023-F03 - failed to reach orbit H-3 22S (TF-1) Tanegashima Space Centre						2023 Mar 7, 01:37
Daichi 3 (ALOS 3, Advanced Land Observation Satellite 3)
Japanese Earth imaging satellite aimed at LTDN 10:30, lost when launch vehicle second stage failed to ignite properly. Earlier launch attempt Jan 17 was called off after main engine ignition but before ignition of solid rocket boosters.

2023-029 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Mar 9, 19:13
OneWeb 0530 2023-029A 55796						in space
Broadband distribution satellite for the UK company OneWeb. One of 40 similar satellites carried on this launch, all initially in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 13, 22:00	6972	0.0009	588	600	96.56	86.51	194
Falcon 9 second stage uncatalogued						Re-entered - 2023 Mar 9 Life <1 day
Launched forty OneWeb satellites. Caused to re-enter above the southern Indian Ocean around 21:00 UTC.
Not Catalogued - orbit parameters unavailable

2023-030 CZ 4C Taiyuan Space Centre						2023 Mar 9, 22:41
Tianhui 6A 2023-030A 55836						in space
One of a pair of satellites carried on the same launch vehicle. Second generation cartographic and imaging satellite using radar orbiting in a tandem formation maintaing spacing of 15-20 km.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 10, 07:15	7262	0.0005	880	887	102.64	98.99	230	05:59
Tianhui 6B 2023-030D 55839						in space
One of a pair of satellites carried on the same launch vehicle. Second generation cartographic and imaging satellite using radar orbiting in a tandem formation maintaing spacing of 15-20 km.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 10, 07:22	7261	0.0005	880	887	102.63	99.00	240	05:59
CZ 4C third stage 2023-030C 55838						in space
Launched Tianhui 6A & 6B. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 10, 07:16	7199	0.0088	757	885	101.32	99.00	43

2023-031 Proton-M + Briz-M Baikonur Cosmodrome						2023 Mar 12, 23:13
Luch 5Х (Olympus 2?) 2023-031A 55841						in space
Mission obscure but may be be a combined communications payload (Luch) for use by satellites in LEO, and an electronic intelligence gathering ELINT payload (Olympus) - possibly for the Security Service of the Russian Federation (FSB). May also carry a payload that provides a reference signal to increase navigational accuracy for GLONASS users.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Mar 14, 08:43	41921	0.0054	35316	35771	1423.68	0.26	197
2023 Mar 19, 07:21	41944	0.0050	35357	35774	1424.81	0.25	194
2023 Mar 21, 13:37	42055	0.0054	35448	35906	1430.49	0.25	195	77°.8 E
2023 Mar 22, 15:18	42137	0.0050	35549	35970	1434.70	0.24	193	78°.5 E
2023 Mar 23, 13:59	42172	0.0046	35599	35988	1436.46	0.23	194	78°.6 E
2023 Mar 23, 16:46	42178	0.0046	35607	35992	1436.75	0.23	193	78°.6 E
2023 Mar 27, 14:17	42310	0.0027	35816	36048	1443.55	0.17	199
2023 Apr 9, 14:07	42165	0.0001	35784	35789	1436.10	0.05	307	58°.0 E
2023 May 3, 21:29	42247	0.0004	35852	35885	1440.30	0.05	114
2023 May 22, 22:57	42164	0.0001	35784	35788	1436.07	0.04	122	8°.9 E
Briz-M rocket stage 2023-031B 55842						in space
Launched Luch 5X. Moved to graveyard orbit after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 16, 05:41	42538	0.0068	35871	36448	1455.19	0.29	151
Briz-M propellant tank 2023-031C 55843						in space
Discarded auxilliary propellant tank from Briz-M that launched Luch 5X.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 13, 15:37	24426	0.7233	381	35716	633.21	48.73	0

2023-032 CZ 2C Jiuquan Space Centre						2023 Mar 13, 04:02
Horus 2 2023-032A 55844						in space
Described as a remote sensing satellite but with no detail of the sensors carried, suggesting it is military/government in nature. Owned by Egypt and developed in co-operation with China using Chinese technology. Launched followed Horus 1 (launched February 24) to make a pair of satellites in orbits with similar LTDN.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 13, 07:02	6874	0.0010	489	502	94.52	97.47	264	10:21
2023 Apr 27, 04:53	6870	0.0013	483	501	94.45	97.47	101	10:23
2023 Apr 27, 11:26	6874	0.0008	490	501	94.52	97.47	105	10:23
2023 Nov 13, 03:18	6873	0.0006	491	499	94.52	97.45	132	10:30
CZ 2C second stage 2023-032B 55845						Re-entered - 2023 Sep 19 Life 190 days
Launched Horus 2. Orbit raised and inclination adjusted after satellite separation, possibly indicating that it carries instruments or sensors.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 13, 16:39	6909	0.0100	461	600	95.25	97.26	222

2023-033 Falcon 9 Block 5 Kennedy Space Center						2023 Mar 15, 00:30
SpaceX Dragon 2 CRS-27 2023-033A 55860						Re-entered - 2023 Apr 15 Life 31 days Returned to Earth
Carrying a cargo to/from the ISS under NASA's Commercial Resupply Services (CRS) contract. Separated from launch vehicle at 00:42 UTC. Docked with the forward-facing port of the Harmony module of ISS Mar 16 at 11:31 UTC, about 20 minutes earlier than anticipated. Undocked 2023 Apr 15 at 15:05 UTC. retrofire at about at 20:08 UTC led to splashdown in the Gulf of Mexico at 20:58 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 15, 00:54	6579	0.0011	194	208	88.51	51.64	10
2023 Mar 15, 03:50	6648	0.0089	210	329	89.91	51.65	230
2023 Mar 16, 05:28	6787	0.0003	407	412	92.75	51.64	106
2023 Mar 16, 08:47	6795	0.0006	413	421	92.90	51.65	106
2023 Mar 16, 10:23	6797	0.0006	415	423	92.95	51.64	97
2023 Apr 14, 19:41	6795	0.0006	413	422	92.92	51.64	193
Falcon 9 second stage uncatalogued						Re-entered - 2023 Mar 15 Life <1 day
Launched SpaceX Dragon 2 CRS-27. Caused to re-enter above the Indian Ocean at about 01:15 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable
Dragon 2 trunk module 2023-033B 56234						Re-entered - 2023 May 19 Life 65 days
Separated from Dragon 2 CRS-27 2023 April 15 prior to retrofire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 16, 16:27	6711	0.0109	260	406	91.19	51.63	165

2023-034 CZ 11 Jiuquan Space Centre						2023 Mar 15, 11:41
Shiyan 19 (Test 19) 2023-034A 55861						in space
Earth imaging satellite equipped with a radar imager. Probably a technology demonstrator.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 15, 14:40	6883	0.0014	495	515	94.72	97.46	284	18:00
CZ 11 fourth stage uncatalogued						Re-entered - 2023 Mar 15 Life <1 day
Launched Shiyan 19. Caused to re-enter after releasing the satellite.
Not Catalogued - orbit parameters unavailable

2023-035 Electron (Stronger Together) Mid Atlantic Regional Space Port, Wallops Island						2023 Mar 16, 22:38
Capella 10 (Whitney 8) 2023-005B 55909						Re-entered - 2025 May 5 Life 781 days
Second generation satellite from Capella Space carrying Synthetic Aperture Radar for Earth imaging. Member of a planned thirty satellite constellation. Released from launch vehicle at 23:36 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 17, 14:40	6976	0.0004	595	600	96.64	44.01	246
Capella 9 (Whitney 7) 2023-005C 55910						Re-entered - 2025 Mar 29 Life 744 days
Second generation satellite from Capella Space carrying Synthetic Aperture Radar for Earth imaging. Member of a planned thirty satellite constellation. Released from launch vehicle at 23:36 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 17, 14:39	6976	0.0004	595	600	96.64	44.01	242
Electron third stage (kick stage) 2023-035A 55908						in space
Launched 2x Capella satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 17, 14:40	6977	0.0003	597	601	96.66	44.18	196
Electron second stage 2023-035D 55911						Re-entered - 2023 Mar 22 Life 6 days
Launched 2x Capella satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 17, 01:13	6618	0.0095	177	303	89.30	44.00	136

2023-036 CZ 3B Xichang Space Centre						2023 Mar 17, 08:33
Gaofen 13-02 2023-036A 55912						in space
Chinese optical remote sensing satellite. Probably moved to Geosynchronous Drift Orbit March 19 then 'lost' by Space-Track until Mar 31.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Mar 17, 12:01	24379	0.7303	197	35805	631.38	28.51	180
2023 Mar 31, 13:03	42165	0.0002	35777	35796	1436.11	3.03	303	146°.7 E
CZ 3B fourth stage 2023-036B 55913						in space
Launched Gaofen 13-02.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 17, 11:47	23646	0.7240	149	34387	603.11	28.49	179

2023-037 Falcon 9 Block 5 (Starlink Group 02-08) Vandenberg Space Force Base						2023 Mar 17, 19:26
Starlink 5856 2023-037A 55914						in space
One member of a simultaneously-launched cluster of fifty two LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at about 18:59 UTC. All satellites expected to be injected initially into similar orbits at about 250-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 22, 18:00	6667	0.0040	262	316	90.29	70.00	162
Falcon 9 second stage uncatalogued						Re-entered - 2023 Mar 17 Life <1 day
Launched fifty two Starlink satellites. Caused to re-enter after their release.
Not Catalogued - orbit parameters unavailable

2023-038 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Mar 17, 23:38
SES 18 2023-038A 55970						in space
One of a pair of simultaneously launched comsats from SES to provide services to the US. Separated from launch vehicle March 18 at 00:09 UTC. Expected location 103° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Mar 18, 20:34	16400	0.5923	309	19736	348.37	26.89	176
2023 Mar 20, 15:45	18061	0.6299	306	23060	402.61	26.80	179
2023 Mar 24, 00:56	24424	0.7241	360	35732	633.12	26.68	181
2023 Mar 24, 16:10	26566	0.5848	4653	35723	718.21	15.13	181
2023 Mar 28, 13:53	37083	0.1346	25715	35695	1184.47	1.92	184
2023 Mar 28, 22:35	40492	0.0395	32515	35712	1351.47	0.54	189
2023 Apr 2, 13:37	42159	0.0003	35768	35794	1435.81	0.08	343	141°.2 W
2023 Apr 3, 15:15	42165	0.0001	35784	35790	1436.11	0.08	29	141°.2 W
2023 Apr 27, 13:07	42123	0.0009	35706	35784	1433.98	0.07	54	141°.0 W
2023 May 1, 12:58	42094	0.0002	35709	35722	1432.46	0.06	38	137°.4 W
2023 Jun 8, 16:45	42162	0.0000	35783	35784	1435.95	0.04	187	103°.1 W
2023 Jun 9, 11:10	42165	0.0000	35785	35788	1436.10	0.02	107	103°.1 W
SES 19 2023-038B 55971						in space
One of a pair of simultaneously launched comsats from SES to provide services to the US. Separated from launch vehicle March 18 at 00:15 UTC. Expected location 135° west, alongside SES 22.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Mar 18, 18:40	16390	0.5921	308	19717	348.05	26.89	176
2023 Mar 20, 12:37	20336	0.6711	310	27605	481.00	26.65	178
2023 Mar 21, 18:42	23029	0.7092	319	32983	579.68	26.62	179
2023 Mar 24, 16:47	26360	0.5984	4207	35756	709.85	15.70	181
2023 Mar 28, 11:40	37382	0.1261	26291	35717	1198.84	1.80	184
2023 Mar 29, 13:03	40591	0.0372	32704	35721	1356.44	0.49	190
2023 Mar 30, 13:31	42107	0.0001	35724	35734	1433.16	0.09	34	144°.8 W
2023 Apr 3, 14:47	42165	0.0000	35784	35788	1436.09	0.08	333	142°.8 W
2023 May 5, 08:53	42163	0.0000	35783	35786	1435.99	0.01	191	142°.5 W
2023 May 7, 12:00	42117	0.0001	35734	35744	1433.65	0.01	205	141°.2 W
2023 May 19, 15:53	42165	0.0002	35780	35794	1436.12	0.05	312	134°.9 W
Falcon 9 second stage 2023-038C 55972						in space
Launched SES 18 and SES 19.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 18, 20:32	16385	0.5922	303	19710	347.88	26.90	176

2023-039 Kuaizhou 1A Jiuquan Space Centre						2023 Mar 22, 08:09
Tianmu 1-03 2023-039A 55973						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 22, 12:06	6889	0.0010	503	517	94.83	97.42	255	15:29
2023 Jul 19, 17:42	6886	0.0014	498	517	94.78	97.43	190	15:28
Tianmu 1-04 2023-039B 55974						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 22, 15:14	6888	0.0011	502	517	94.82	97.41	261	15:29
2023 Jul 19, 18:52	6886	0.0011	500	515	94.78	97.42	188	15:28
Tianmu 1-05 2023-039C 55975						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 22, 15:13	6888	0.0010	502	516	94.81	97.41	260	15:29
2023 Jul 19, 18:29	6886	0.0007	503	512	94.78	97.43	175	15:28
Tianmu 1-06 2023-039D 55976						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 22, 15:13	6887	0.0010	501	516	94.79	97.41	263	15:29
2023 Jul 19, 18:05	6886	0.0006	504	512	94.78	97.43	175	15:28
Kuaizhou 11 third stage 2023-039E 55977						Re-entered - 2023 Mar 23 Life 1 day
Launched Tianmu 1 03 - Tianmu 1 06. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 22, 15:15	6675	0.0267	119	475	90.46	97.39	45

2023-F04 - failed to reach orbit Terran 1 Cape Canaveral Space Force Station						2023 Mar 23, 03:25
Terran 1 second stage
Instrumented rocket body aimed at ~28° inclination. Lost when it failed to ignite properly.

2023-040 Soyuz-2.1a Plesetsk Cosmodrome						2023 Mar 23, 06:40
Cosmos 2567 (Bars-M №4) 2023-040A 55978						in space
Russian government optical imaging satellite for use in cartography.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 23, 11:32	6797	0.0119	338	500	92.95	97.64	72	22:23
2023 Mar 24, 23:18	6799	0.0115	343	499	92.99	97.64	67	22:24
2023 Mar 25, 22:25	6831	0.0067	408	499	93.65	97.64	63	22:24
2023 Mar 31, 08:27	6880	0.0008	496	507	94.65	97.63	290	22:25
2023 Nov 22, 02:47	6870	0.0012	484	500	94.45	97.61	167	22:52
2023 Dec 21, 10:49	6869	0.0013	482	500	94.43	97.61	75	22:55
2024 Feb 6, 03:19	6879	0.0006	497	505	94.64	97.61	257	23:01
2024 Oct 31, 04:57	6867	0.0009	482	495	94.38	97.59	44	23:29
Soyuz upper stage 2023-040B 55979						Re-entered - 2023 Nov 22 Life 244 days
Launched Cosmos 2567.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 23, 10:19	6795	0.0118	337	498	92.92	97.65	72

2023-041 Electron (The Beat Goes On) Rocket Lab Launch Complex, New Zealand						2023 Mar 24, 09:14
BlackSky 19 (Global 19) 2023-041B 55982						in space
Second Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc. Released from kick stage at 10:11 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 25, 10:43	6831	0.0005	450	456	93.65	42.02	258
BlackSky 5 (Global 5) 2023-041C 55983						in space
Second Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc. Released from kick stage at 10:11 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 24, 19:34	6829	0.0009	445	457	93.61	42.02	273
Electron third stage (kick stage) 2023-041D 55984						Re-entered - 2023 Apr 7 Life 14 days
Launched 2x BlackSky satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 24, 22:33	6721	0.0154	240	446	91.40	41.97	19
Electron second stage 2023-041E 55985						Re-entered - 2023 Apr 1 Life 8 days
Launched 2x BlackSky satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 24, 17:22	6690	0.0196	181	443	90.76	42.02	261

2023-042 Falcon 9 Block 5 (Starlink Group 05-05) Cape Canaveral Space Force Station						2023 Mar 24, 15:43
Starlink 5905 2023-042A 55986						in space
One member of a simultaneously-launched cluster of fifty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:54 UTC. All satellites expected to be injected initially into similar orbits at about 250-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 30, 16:00	6708	0.0007	326	335	91.13	43.00	317
Falcon 9 upper stage uncatalogued						Re-entered - 2023 Mar 24 Life <1 day
Launched fifty six Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-043 LVM3 (M3) Satish Dhawan Space Centre						2023 Mar 26, 03:30
OneWeb 0537 2023-043A 56046						in space
Broadband distribution satellite for the UK company OneWeb. Released from launch vehicle in nine batches of four, to avoid collisions, starting at 10:50 UTC. One of 36 similar satellites carried on this launch, all initially in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 28, 16:00	6827	0.0011	441	457	93.57	87.42	266
LVM3 third stage 2023-043AN 56082						Re-entered - 2024 Jun 14 Life 446 days
Launched 36 OneWeb satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 26, 04:45	6827	0.0011	441	457	93.57	87.47	246

2023-044 Shavit 2 Palmachim AFB, Israel						2023 Mar 28, 23:10
Ofeq 13 2023-044A 56083						in space
Israeli electro-optical (probably) reconnaissance satellite to monitor the Middle East from highly retrograde orbit.
Orbit classified as 'Secret' - data withheld
Shavit fourth stage 2023-044B 56084						Re-entered - 2023 Jul 23 Life 117 days
Launched Ofeq 13.
Orbit classified as 'Secret' - data withheld

2023-045 Soyuz-2.1v Plesetsk Cosmodrome						2023 Mar 29, 19:57
Cosmos 2568 2023-045A 56091						Re-entered - 2025 Jan 3 Life 646 days
Possible imaging reconnaissance satellite. Initial near-sun-synchronous LTDN matched Cosmos 2560 (54050/2022-135A), Cosmos 2555 (52330/2022-044A) and Cosmos 2551 (49127/2021-081A). All of them re-entered naturally after a few weeks without any orbital manoeuvres. Cosmos 2568 followed a similar pattern until a minor orbit 'tweak' July 11. Then, for about eight weeks, August 16 - October 6, it operated a thruster to maintain a steady orbit height with a precise 16 day repeating ground track before resuming steady orbit decay. On Oct 11 it started a new phase of orbit maintenance that lasted through 2024 August when the orbit was raised by 11 km. Ceased all manoeuvring 2024 November.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 29, 21:45	6715	0.0011	329	345	91.27	96.46	299	11:30
2023 Jul 11, 11:38	6684	0.0009	300	312	90.64	96.46	240	11:11
2023 Aug 17, 17:06	6671	0.0009	286	299	90.36	96.45	110	11:07
2023 Oct 5, 09:14	6671	0.0005	289	296	90.36	96.44	251	11:01
2023 Oct 12, 18:59	6667	0.0006	284	293	90.29	96.45	228	11:00
2024 Oct 31, 15:36	6673	0.0002	293	296	90.41	96.36	131	10:04
Soyuz upper stage 2023-045B 56092						Re-entered - 2023 Jul 4 Life 97 days
Launched Cosmos 2568.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 29, 21:45	6713	0.0013	326	344	91.23	96.46	289

2023-046 Falcon 9 Block 5 (Starlink Group 05-10) Cape Canaveral Space Force Station						2023 Mar 29, 20:01
Starlink 6102 2023-046A 56093						Re-entered - 2024 Dec 19 Life 631 days
One member of a simultaneously-launched cluster of fifty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 20:06 UTC. All satellites expected to be injected initially into similar orbits at about 250-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 16:00	6717	0.0004	336	342	91.32	43.00	269
Falcon 9 upper stage uncatalogued						Re-entered - 2023 Mar 29 Life <1 day
Launched fifty six Starlink satellites. Caused to re-enter above the Indian Ocean after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-047 CZ 2D Taiyuan Space Centre						2023 Mar 30, 10:50
Hongtu 1-01 (Piesat 1-01) 2023-047A 56153						in space
One of a simultaneously-launched cluster of four commercially-operated radar imaging satellites from the PieSat company. They will fly in formation, with the main satellite transmitting the radar signal and three auxiliary satellites acting as receivers, using interferometry to produce high resolution images.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 30, 13:50	6884	0.0010	500	513	94.75	97.44	270	18:00
2023 Apr 12, 11:30	6884	0.0011	498	513	94.73	97.44	221	18:00
2023 Apr 15, 12:03	6885	0.0013	498	516	94.76	97.43	216	18:00
Hongtu 1-02 (Piesat 1-02) 2023-047B 56154						in space
One of a simultaneously-launched cluster of four commercially-operated radar imaging satellites from the PieSat company. They will fly in formation, with the main satellite transmitting the radar signal and three auxiliary satellites acting as receivers, using interferometry to produce high resolution images.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 30, 13:50	6884	0.0011	498	513	94.73	97.44	281	18:00
2023 Apr 12, 12:56	6883	0.0011	497	512	94.71	97.44	228	18:00
2023 Apr 13, 14:18	6884	0.0011	498	513	94.73	97.44	226	18:00
Hongtu 1-03 (Piesat 1-03) 2023-047C 56155						in space
One of a simultaneously-launched cluster of four commercially-operated radar imaging satellites from the PieSat company. They will fly in formation, with the main satellite transmitting the radar signal and three auxiliary satellites acting as receivers, using interferometry to produce high resolution images.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 30, 13:48	6883	0.0011	497	512	94.71	97.44	281	18:00
2023 Apr 11, 13:18	6882	0.0011	496	512	94.70	97.44	236	18:00
2023 Apr 14, 13:58	6885	0.0014	497	516	94.76	97.44	228	18:00
2023 Apr 21, 16:34	6891	0.0012	505	521	94.88	97.44	198	18:00
Hongtu 1-04 (Piesat 1-04) 2023-047D 56156						in space
One of a simultaneously-launched cluster of four commercially-operated radar imaging satellites from the PieSat company. They will fly in formation, with the main satellite transmitting the radar signal and three auxiliary satellites acting as receivers, using interferometry to produce high resolution images.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Mar 30, 13:48	6882	0.0011	496	511	94.70	97.44	289	18:00
2023 Apr 11, 13:15	6881	0.0011	495	511	94.68	97.44	242	18:00
2023 Apr 14, 20:22	6884	0.0013	497	515	94.73	97.44	231	18:00
CZ 2D second stage uncatalogued						Re-entered - 2023 Mar 30 Life <1 day
Launched Hongtu-1 Group1 (4 satellites). Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-048 CZ 4C Jiuquan Space Centre						2023 Mar 31, 06:27
Yaogan 34-04 2023-048A 56157						in space
Imaging satellite - orbit is similar to the Yaogan 31 electronic surveillance satellites, and the Initial orbit plane has RAAN about three degrees to the east of that of the first Yaogan 31 triplet (launch no 2018-034). Expected to move into formation with the Yaogan 31 group.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 31, 10:05	7472	0.0003	1092	1096	107.14	63.40	257
2023 Apr 1, 09:07	7473	0.0002	1094	1097	107.16	63.40	277
2023 Apr 15, 14:15	7470	0.0007	1087	1097	107.09	63.40	307
CZ 4C third stage 2023-048B 56158						in space
Launched Yaogan 34-04. Perigee lowered after releasing satellite
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 31, 10:01	7384	0.0122	915	1096	105.24	63.41	44

2023-049 Tianlong-2 Jiuquan Space Centre						2023 Apr 2, 08:48
Love Space Science 2023-049A 56159						Re-entered - 2024 Feb 7 Life 311 days
4U Cubesat (4x1) to demonstrate capability of the Tianlong-2 rocket on its first launch. Equipped with an Earth imaging system, reportedly for remote sensing.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Apr 3, 05:06	6865	0.0013	478	496	94.36	97.41	281	15:08
Tianlong-2 third stage uncatalogued						Re-entered - 2023 Apr 2 Life <1 day
Launched Love Space Science. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable

2023-050 Falcon 9 Block 5 Vandenberg Space Force Base						2023 Apr 2, 14:29
Checkmate 8 (SDA Tranche 0 Data Relay 8) 2023-050A 56162						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations. Separated from launch vehicle at about 15:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 09:32	7326	0.0005	944	952	104.00	81.00	227
Checkmate 5 (SDA Tranche 0 Data Relay 5) 2023-050B 56163						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations. Separated from launch vehicle at about 15:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 09:37	7326	0.0006	943	952	104.00	81.00	226
Checkmate 4 (SDA Tranche 0 Data Relay 4) 2023-050C 56164						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations. Separated from launch vehicle at about 15:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 09:31	7325	0.0006	943	952	103.99	81.00	224
Checkmate 6 (SDA Tranche 0 Data Relay 6) 2023-050D 56165						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations. Separated from launch vehicle at about 15:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 21:00	7325	0.0006	943	952	103.99	81.00	221
Checkmate 7 (SDA Tranche 0 Data Relay 7) 2023-050E 56166						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations. Separated from launch vehicle at about 15:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 21:00	7325	0.0006	943	951	103.99	81.00	219
Checkmate 2 (SDA Tranche 0 Data Relay 2) 2023-050F 56167						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations. Separated from launch vehicle at about 15:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 21:00	7325	0.0006	943	951	103.99	81.00	221
Checkmate 1 (SDA Tranche 0 Data Relay 1) 2023-050G 56168						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations. Separated from launch vehicle at about 15:30 UTC. One of eight similar satellites carried on this launch. All are in similar orbits
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 21:00	7325	0.0006	943	951	103.98	81.00	218
Checkmate 3 (SDA Tranche 0 Data Relay 3) 2023-050H 56169						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations. Separated from launch vehicle at about 15:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 21:00	7325	0.0006	942	951	103.98	81.00	215
BB 2 (SDA Tranche 0 Target Tracker 2) 2023-050J 56170						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture", equipped with sensors to provide 'beyond line-of-sight targeting' for ships and mobile missile launchers. Separated from launch vehicle at about 15:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 21:00	7323	0.0008	939	951	103.94	81.00	208
2023 Apr 16, 12:57	7328	0.0010	943	957	104.05	81.00	169
2023 Apr 21, 02:01	7330	0.0006	948	956	104.09	81.00	173
2023 Apr 24, 18:16	7333	0.0010	948	962	104.15	81.00	151
2023 May 21, 22:02	7344	0.0011	958	975	104.40	81.00	58
BB 1 (SDA Tranche 0 Target Tracker 1) 2023-050K 56171						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture", equipped with sensors to provide 'beyond line-of-sight targeting' of ships and mobile missile launchers. Separated from launch vehicle at about 15:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 3, 20:59	7323	0.0009	938	951	103.94	81.00	206
2023 Apr 22, 07:40	7329	0.0011	943	959	104.08	80.99	133
2023 May 22, 17:51	7331	0.0012	945	962	104.12	81.00	74
2023 May 23, 07:45	7333	0.0010	947	962	104.15	81.01	84
2023 May 24, 13:16	7334	0.0013	947	965	104.18	81.00	66
2023 May 26, 03:30	7336	0.0014	948	968	104.22	81.03	67
2023 Jun 2, 14:34	7340	0.0015	951	973	104.31	81.00	35
2023 Jun 7, 18:05	7343	0.0017	953	977	104.36	81.00	22
2023 Jun 16, 09:11	7344	0.0017	954	978	104.39	81.00	0
2023 Jul 1, 08:38	7344	0.0015	955	977	104.40	81.00	319
Falcon 9 upper stage uncatalogued						in space
Launched ten Tranche 0 satellites for the US Space Development Agency. Caused to re-enter at about 16:45 UTC after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-051 Hyperbola 1 (Y6) Jiuquan Space Centre						2023 Apr 7, 04:00
Hyperbola 1 fourth stage 2023-051A 56172						Re-entered - 2023 Oct 29 Life 205 days
Instrumented upper stage carried on verification flight of a launch vehicle operated by Chinese private company i-Space. Three of the previous four launches failed to reach orbit. Initial value for Argument of Perigee suggests perigee was lowered from an initial 500 km circular orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Apr 7, 14:59	6778	0.0154	295	504	92.55	97.34	350	10:20

2023-052 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Apr 7, 04:30
Intelsat 40e 2023-052A 56174						in space
Comsat to provide services to commercial aviation, maritime customers, land mobile customers and commercial networks. Also carries NASA's TEMPO (Tropospheric Emissions: Monitoring of Pollution) instrument as a hosted payload - it will provide hourly measurements of air quality and pollution over North America. Expected location - 91° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Apr 7, 13:03	21828	0.6995	181	30719	534.91	26.98	177
2023 Apr 10, 22:00	23411	0.7177	230	33836	594.14	26.97	179
2023 Apr 13, 17:12	26355	0.5950	4296	35658	709.68	15.40	181
2023 Apr 17, 09:12	40762	0.0308	33129	35638	1365.02	0.30	168
2023 Apr 18, 18:36	42021	0.0002	35632	35653	1428.75	0.03	207	108°.4 W
2023 Apr 19, 11:41	42009	0.0004	35614	35647	1428.14	0.03	249	106°.9 W
2023 Apr 25, 08:50	42059	0.0004	35666	35696	1430.70	0.01	260	97°.1 W
2023 Apr 30, 21:19	42113	0.0005	35713	35756	1433.43	0.00	103	92°.3 W
2023 May 3, 19:52	42122	0.0004	35726	35761	1433.89	0.07	304	90°.5 W
2023 May 4, 21:00	42165	0.0001	35781	35792	1436.09	0.02	245	91°.0 W
Falcon 9 second stage 2023-052B 56175						in space
Launched Intelsat 40E.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 7, 07:10	21795	0.6992	178	30656	533.70	27.00	177

2023-053 Ariane 5ECA (VA-260) Centre Spatiale Guyanaise						2023 Apr 14, 12:14
JUICE (Jupiter Icy Moons Explorer) 2023-053A 56176						Re-entered - 2023 Apr 15 Life 1 day
ESA planetary explorer aimed to study potentially trapped water in Jupiter's the largest moons - Europa, Ganymede and Callisto. Expected to arrive in the vicinity of Jupiter in 2031 after following a convoluted trajectory using Earth fly-by to increase speed.
Heliocentric orbit
Ariane 5 third stage 2023-053B 56177						Re-entered - 2023 Apr 15 Life 1 day
Launched JUICE.
Heliocentric orbit

2023-054 Falcon 9 Block 5 (Transporter 7) Vandenberg Space Force Base						2023 Apr 15, 06:47
IMECE 2023-054A 56178						in space
Earth observation satellite designed and developed by TÜBİTAK Space Technologies Research Institute (TÜBİTAK UZAY) of Turkey. Separated from launch vehicle at 09:23 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Apr 19, 13:18	7052	0.0008	668	679	98.22	98.21	192	22:31
OrbAstro AF 1 (Brokkr 1) 2023-054B 56179						in space
Separated from launch vehicle at 07:50 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 14:44	6881	0.0007	498	508	94.68	97.41	242
DewaSat 2 2023-054C 56180						Re-entered - 2025 Mar 18 Life 703 days
6U Cubesat from the Dubai Electricity and Water Authority of the UAE and built in co-operation with NanoAvionics of Lithuania, equipped with an Earth Imaging System. It will also study greenhouse gases and provide a link to relay data from internet-connected sensors on the ground. Separated from launch vehicle at 07:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 19, 04:56	6881	0.0009	496	508	94.67	97.42	239
KilicSat 2023-054D 56181						Re-entered - 2025 Jan 31 Life 657 days
3U Cubesat from Gumush Aerospace and the The University of Turkish Aerospace Association (UTAA) equipped with an AIS receiver to relay messages from ships at sea to the ground. Separated from launch vehicle at 07:49 UTC. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 14:44	6881	0.0008	497	508	94.67	97.41	238
Lemur 2 (KAUST, OnReflection) 2023-054E 56182						Re-entered - 2024 Oct 7 Life 541 days
6U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. Also carries a hyperspectral Earth imaging camera with an onboard image processing system. Separated from launch vehicle at 07:50 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 14:44	6880	0.0007	497	507	94.66	97.40	231
Sateliot 0 2023-054F 56183						in space
6U Cubesat - demonstrator for an eventual constellation to provide internet messaging connectivity for remote stations. Separated from launch vehicle at 07:55 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 14:44	6880	0.0007	497	507	94.66	97.41	225
SSS 2B 2023-054G 56184						Re-entered - 2024 Dec 26 Life 621 days
3U Cubesat from TÜBİTAK Space Technologies Research Institute (TÜBİTAK UZAY) used to train students in satellite engineering. Payload includes a remote sensing camera. Separated from launch vehicle at 07:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 14:43	6880	0.0009	496	509	94.66	97.42	239
BRO 9 (Breizh Reconnaissance Orbiter 9) 2023-054H 56185						in space
6U Cubesat from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Separated from launch vehicle at 07:50 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 14:43	6880	0.0008	497	507	94.66	97.41	232
GHGSat C8 (Océane) 2023-054J 56186						in space
Small satellite in a constellation being built for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground. Separated from launch vehicle at 07:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 14:43	6880	0.0009	496	508	94.66	97.41	236
Lemur-2 + Adler 2 (SpaceGus) 2023-054K 56187						Re-entered - 2024 Aug 17 Life 490 days
6U Cubesat carrying the Austrian Particle Impact Detector (APID) to detect very small items of debris in LEO and a radar system with a 100m range. Design is based on the 3U Lemur-2 satellite from Spire but with specialised instrumentation alongside the standard Lemur-2 equipment. Separated from launch vehicle at 07:55 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 14:43	6880	0.0007	497	507	94.65	97.41	220
CIRBE (Colorado Inner Radiation Belt Experiment) 2023-054L 56188						Re-entered - 2024 Oct 4 Life 538 days
3U Cubesat from the University of Coloado, Boulder - equipped to study the formation of electrons in the Earth's inner radiation belt. NASA's ELaNa 47 (Educational Launch of NanoSats) mission. Separated from launch vehicle at 07:54 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 14:43	6880	0.0008	496	507	94.65	97.41	230
It's About Time 2023-054M 56189						in space
?U Cubesat - demonstrator payload from US company TrustPoint, details not disclosed. Separated from launch vehicle at 07:54 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:17	6879	0.0009	495	507	94.64	97.41	229
ÑuSat 36 (Annie Cannon) 2023-054N 56190						Re-entered - 2025 Apr 15 Life 731 days
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Separated from launch vehicle at 07:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:17	6879	0.0008	495	507	94.64	97.41	218
Hawk 7A 2023-054P 56191						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. Separated from launch vehicle at 08:01 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:17	6879	0.0009	494	507	94.63	97.41	221
ION SCV-010 (Masterful Matthaeus) 2023-054Q 56192						in space
Satellite Carrier Vehicle built by D-Orbit. Separated from launch vehicle at 08:15 UTC. Satellites: VCub 1 - released Apr 22, ~22:15 UTC, Kepler 20 - released Apr 26, ~06:50 UTC, Kepler 21 - released Apr 26, ~17:00 UTC, ELO 3 - released Apr 25, ~10:30 UTC, EPICHyper 1 - released late-June. Hosted payloads include: Scorpio - sensor from Elt's Space for use in electronic intelligence gathering, MicroCMG - demonstrator from Veoware of a gyroscope-based attitude control system for small satellites,
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:17	6879	0.0009	494	507	94.63	97.41	219
Hawk 7B 2023-054R 56193						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. Separated from launch vehicle at 08:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:17	6879	0.0009	494	507	94.63	97.41	217
NorSat TD 2023-054S 56194						in space
Small satellite carrying an experimental navigation radar detector to augment ship detection capabilities from an on-board Automatic Identification System (AIS) receiver. Also carries an experimental thruster and a space-ground laser communication system. Separated from launch vehicle at 08:03 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:16	6879	0.0009	494	507	94.63	97.41	221
GHOSt 1 (Global Hyperspectral Observation Satellite) 2023-054T 56195						in space
Commercial satellite in a planned constellation of six equipped with a multi-spectral Earth imaging system. Separated from launch vehicle at 08:18 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:16	6879	0.0010	494	507	94.62	97.41	217
Vigoride 6 2023-054U 56196						Re-entered - 2024 Nov 23 Life 588 days
Satellite carrier from US company Momentus Systems, separated from launch vehicle at 08:20 UTC. Satellites: LLITED A - released on May 15 around 23:30 UTC, LLITED B - released on May 15 around 23:30 UTC, VIREO - released on May 15 around 23:00 UTC, DISCO 1 - released on May 15 at about 23:00 UTC, IRIS C (Intelligent Remote Sensing and Internet Satellite) - released May 17 around 19:30 UTC, Revela - released May 31 around 20:00 UTC. Hosted payloads: TASSA (Tape Spring Solar Array) - a developmental solar array.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:16	6878	0.0010	493	507	94.61	97.41	222
GHOSt 2 (Global Hyperspectral Observation Satellite) 2023-054V 56197						in space
Commercial satellite in a planned constellation of six equipped with a multi-spectral Earth imaging system. Separated from launch vehicle at 08:14 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:16	6878	0.0011	492	507	94.61	97.41	219
Umbra 06 2023-054W 56198						Re-entered - 2024 Nov 18 Life 583 days
Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Separated from launch vehicle at 08:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:15	6877	0.0011	492	507	94.60	97.41	216
Tomorrow R1 2023-054X 56199						Re-entered - 2025 Apr 19 Life 735 days
Small satellite from US company Tomorrow.io to demonstrate a weather radar sytem to be used in a future constellation of LEO meteorological satellites. Separated from launch vehicle at 08:02 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:15	6878	0.0011	492	507	94.61	97.41	221
Hawk 7C 2023-054Y 56200						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. Separated from launch vehicle at 08:02 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 17:50	6878	0.0011	492	507	94.61	97.41	218
ÑuSat 39 (Tikvah Alper) 2023-054Z 56201						in space
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Separated from launch vehicle at 08:14 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 17:50	6877	0.0011	491	507	94.60	97.41	220
ÑuSat 38 (Maria Gaetana Agnesi) 2023-054AA 56202						in space
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Separated from launch vehicle at 07:55 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 17:50	6877	0.0011	491	507	94.60	97.41	219
ÑuSat 37 (Joan Clarke) 2023-054AB 56203						in space
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Separated from launch vehicle at 07:55 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 17:50	6877	0.0012	491	507	94.60	97.41	216
GHGSat C6 (Mey-Lin) 2023-054AC 56204						in space
Small satellite in a constellation being built for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground. Separated from launch vehicle at 07:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:14	6877	0.0012	490	507	94.58	97.41	214
FACSat 2 (Chiribiquete) 2023-054AD 56205						in space
6U Cubesat for the Colombian Air Force (FAC) equipped with an Earth imaging system. Separated from launch vehicle at 07:52 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:13	6875	0.0014	487	507	94.56	97.41	212
Lemur 2 (GNSS-4, Romeo'n'Leo) 2023-054AE 56206						Re-entered - 2024 Apr 29 Life 380 days
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. Carries additional equipment to gather data about the Earth's atmosphere, including measurements of temperature, humidity, precipitation, plus ionospheric electron density. Separated from launch vehicle at 07:56 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:14	6876	0.0012	489	506	94.57	97.41	211
Pleiades Squared (Pleiades Yearling replacement) 2023-054AF 56207						Re-entered - 2024 Aug 12 Life 485 days
1U Cubesat from BroncoSpace al Calpoly, designed to allow users on the ground to experiment with satellite hardware and software - includes and imaging system. Lack of reports from its owner or radio reception reports after launch indicates that it probably failed to activate. Intended to replace a similar satellite (Pleiades Yearling) carried on the Transporter 6 flight 2023 Jan that was unable to separate from the Orbiter SN1 carrier when the latter malfunctioned.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:14	6876	0.0013	488	507	94.57	97.42	218
Taifa 1 2023-054AG 56208						Re-entered - 2025 Apr 28 Life 744 days
3U Cubesat from the Kenyan Space Agency, equipped with an Earth observation camera. Separated from launch vehicle at 07:51 UTC. Lack of news reports and radio reception reports after launch indicates that it probably failed to activate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 19, 15:53	6876	0.0012	489	506	94.57	97.40	203
GHGSat C7 (Gaspard) 2023-054AH 56209						in space
Small satellite in a constellation being built for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground. Separated from launch vehicle at 07:50 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:14	6876	0.0013	489	506	94.57	97.41	208
Connecta T2.1 2023-054AJ 56210						in space
3U Cubesat from Turkish company Plan-S as a demonstrator for a constellation of Earth observation satellites. Separated from launch vehicle at 07:52 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:13	6876	0.0013	489	506	94.56	97.41	207
Inspiresat 7 2023-054AK 56211						Re-entered - 2024 Sep 18 Life 522 days
2U Cubesat - Earth observation satellite studying the Earth's radiation budget and to demonstrate new space equipment from Le Laboratoire Atmosphères, Observations Spatiales (LATMOS) of France. Separated from launch vehicle at 07:52 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:13	6875	0.0014	488	507	94.56	97.42	215
RoseyCubesat 1 2023-054AL 56212						Re-entered - 2024 Sep 1 Life 505 days
1U Cubesat from Orbital Solutions Monaco to act as teaching aid for controlling amateur radio satellites. Payload includes an Earth observation system. Separated from launch vehicle at 07:53 UTC. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:13	6875	0.0014	487	507	94.55	97.42	214
Sapling Giganteum 2023-054AM 56213						Re-entered - 2024 Sep 18 Life 522 days
1U Cubesat from Stanford Student Space Initiative to demonstrate smart downlinking of images using a Google Coral camera and Google Coral Edge coprocessor. Replaces a similar satellite carried on the Transporter 6 flight 2023 Jan that was unable to separate from the Orbiter SN1 carrier when the latter malfunctioned. Separated from launch vehicle at 07:52 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:13	6875	0.0014	487	506	94.55	97.41	208
LacunaSat 2f 2023-054AN 56214						Re-entered - 2024 Oct 30 Life 564 days
3U Cubesat - demonstrator satellite from Lithuanian company Nanoavionics with a receiver for data from Internet connected devices. Separated from launch vehicle at 07:52 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 18, 16:13	6875	0.0014	487	506	94.55	97.41	210
VCub 1 2023-054AP 56215						Re-entered - 2025 Feb 1 Life 658 days
3U Cubesat from Visiona Tecnologia Espacial of Brazil - built as a demonstrator and test bed for space systems, including a high quality Earth imaging system and an internet-based radio system to collect data from remote stations on land and in the ocean. Released from ION SCV-010 April 22 around 22:15 UTC. Catalogue Number and designation were initially assigned to a phantom object in 670 km orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 23, 16:13	6876	0.0011	491	506	94.58	97.41	184
ELO 3 (Eutelsat LEO for Objects) 2023-054AQ 56216						Re-entered - 2024 Aug 12 Life 485 days
6U Cubesat from Eutelsat to act as a demonstrator for a broadband internet communications satellite. Released from ION SCV-010 Apr 25 at around 10:30 UTC. Catalogue Number and designation were initially assigned to a phantom object in 670 km orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 26, 12:05	6880	0.0007	497	507	94.66	97.41	183
Kepler 20 2023-054AR 56217						in space
6U Cubesat - Kepler Gen 1 satellite, part of a planned 140 satellite constellation from Kepler Aerospace carrying a high capacity communications system to provide links between other satellites and the ground, and a prototype of an Internet communications system. Released from ION SCV-010 Apr 26 at around 06:50 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 27, 14:54	6878	0.0011	492	507	94.60	97.41	190
Kepler 21 2023-054AS 56218						in space
6U Cubesat - Kepler Gen 1 satellite, part of a planned 140 satellite constellation from Kepler Aerospace carrying a high capacity communications system to provide links between other satellites and the ground, and a prototype of an Internet communications system. Released from ION SCV-010 Apr 26 at around 17:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 27, 14:55	6879	0.0009	495	508	94.64	97.41	182
LLITED B (Low-Latitude Ionosphere/Thermosphere Enhancements in Density) 2023-054AT 56219						Re-entered - 2024 Aug 22 Life 495 days
1.5U Cubesat from The Aerospace Corporation to study anomalies in the Earth's ionosphere and thermosphere. One of a simultaneously-launched pair. Part of NASA funded ELaNa 40 (Educational Launch of Nanosatellites) mission. Released from Vigoride 6 on May 15 around 23:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 18, 12:26	6877	0.0015	488	509	94.59	97.41	115
LLITED A (Low-Latitude Ionosphere/Thermosphere Enhancements in Density) 2023-054AU 56220						Re-entered - 2024 Aug 26 Life 499 days
1.5U Cubesat from The Aerospace Corporation to study anomalies in the Earth's ionosphere and thermosphere. One of a simultaneously-launched pair. Part of NASA funded ELaNa 40 (Educational Launch of Nanosatellites) mission. Released from Vigoride 6 on May 15 around 23:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 18, 14:01	6877	0.0015	488	509	94.59	97.41	115
IRIS-C (Intelligent Remote Sensing and Internet Satellite) 2023-054AV 56221						Re-entered - 2024 Oct 18 Life 552 days
3U Cubesat from the National Cheng Kung University of Taiwan to further develop satellite design and to demonstrate a star-tracking sensor. Also includes an internet-connected comms system for message relay. Released from Vigoride 6 on May 17 at about 19:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 23, 18:38	6877	0.0015	488	509	94.59	97.41	97
DISCO 1 2023-054AW 56222						Re-entered - 2025 Jan 28 Life 654 days
1U Cubesat from a consortium led by Aarhus University, Denmark to allow students to participate in programming and controlling a satellite. Also includes an amateur radio payload. Separated from Vigoride 6 on May 15 at about 23:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 2, 04:12	6876	0.0016	487	509	94.58	97.41	73
Vireo 1 2023-054AX 56223						Re-entered - 2024 Aug 8 Life 481 days
3U Cubesat from C3S, to demonstrate an Earth imaging system based artificial intelligence. Released from Vigoride 6 May 15 around 23:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 2, 05:42	6876	0.0015	487	508	94.57	97.40	70
Revela 2023-054AY 56224						Re-entered - 2025 Jan 3 Life 629 days
3U Cubesat from Italian company ARCA Dynamics. Equipped with an Earth imaging camera to act as a demonstrator for an onboard image analysis and processing system. Released from Vigoride 6 May 31 around 20:00 UTC.
EPICHyper 1 2023-054AZ 56225						in space
6U Cubesat from Wyvern Inc of Canada equipped with a wide-spectrum Earth imaging system aimed initially at the agricultural industry and use in detecting invasive plants and pests, and changes in soil chemistry. Released from ION SCV-010 late June.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 26, 13:58	6936	0.0011	551	566	95.82	97.51	251
Falcon 9 second stage uncatalogued						Re-entered - 2023 Apr 15 Life <1 day
Launched Transporter 7 multi-satellite mission. A small payload of human cremation ashes remained intentionally attached. Caused to re-enter at around 10:30 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-055 CZ 4B Jiuquan Space Centre						2023 Apr 16, 01:36
Fengyun 3G (Fengyun 3-07) 2023-055A 56232						in space
Climate studies - launched as a contribution to the international Global Precipitation Measurement programme. Released from launch vehicle at 01:48 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 16, 07:32	6790	0.0007	407	416	92.80	50.00	277
CZ 4B third stage 2023-055B 56233						Re-entered - 2023 Apr 27 Life 11 days
Launched Fengyun 3G. Initial orbit based on Chinese data. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
	6793	0.0006	410	418	92.86	50.01	130
2023 Apr 16, 07:31	6677	0.0165	189	409	90.49	50.07	9

2023-056 Falcon 9 Block 5 (Starlink Group 06-02) Cape Canaveral Space Force Station						2023 Apr 19, 14:31
Starlink 30096 2023-056A 56286						Re-entered - 2023 May 10 Life 21 days
One member of a simultaneously-launched cluster of twenty one V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:36 UTC. All satellites expected to be injected initially into similar orbits at about 360 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 24, 14:10	6710	0.0004	329	334	91.16	43.00	318
Falcon 9 second stage uncatalogued						Re-entered - 2023 Apr 19 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter at about 16:45 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-057 PSLV-CA (PSLV C-55) Satish Dhawan Space Centre						2023 Apr 22, 08:49
Lumelite 4 2023-057B 56309						in space
12U Cubesat from the Institute for Infocomm Research, Singapore National University. Carries a VDES communications payload to relay two-way messages between ships at sea and shore stations. Released from launch vehicle at 09:09 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 23, 02:00	6961	0.0009	576	589	96.32	9.99	359
TeLEOS 2 2023-057C 56310						in space
Earth observation satellite from Singapore carrying a high-resolution radar imaging system. Released from launch vehicle at 09:08 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 23, 02:00	6963	0.0006	580	589	96.37	9.99	349
PSLV upper stage + POEM 2 (PSLV Orbital Experimental Module 2) 2023-057A 56308						in space
Launched TeLEOS 2 and Lumelite 4. Also carries seven hosted space technology payloads powered by POEM's solar panels. Orbit raised in a sequence of engine firings beginning at 09:17 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 23, 05:58	6982	0.0022	588	618	96.76	9.89	234

2023-I04 Nanoracks Cubesat Deployer International Space Station						2023 Apr 24, 12:05
ARKSat 1 1998-067VC 56311						Re-entered - 2023 Oct 30 Life 189 days
1U Cubesat from the University of Arkansas - includes a test version of a balloon-based drag system for de-orbit, and a high powered Xenon flash for visual tracking.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 25, 12:39	6791	0.0009	407	419	92.83	51.63	275
ExAlta 2 1998-067VE 56313						Re-entered - 2023 Oct 31 Life 190 days
3U Cubesat from the University of Alberta, Canada - demonstrator of an imaging system and satellite operational systems, part of the Northern SPIRIT Consortium space mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 25, 12:39	6792	0.0008	408	419	92.83	51.63	269
LightCube 1 1998-067VF 56314						Re-entered - 2023 Oct 17 Life 176 days
1U Cubesat from Arizona State University, equipped with a pair of bright Xenon flash tubes to produce flashes visible to the naked eye.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 25, 12:39	6792	0.0009	408	420	92.85	51.64	255

2023-I05 Nanoracks Cubesat Deployer International Space Station						2023 Apr 24, 12:15
AuroraSat 1998-067VD 56312						Re-entered - 2023 Oct 11 Life 170 days
2U Cubesat from AURORA College, Canada - equipped with a display screen on its outer surface to show images of art items pre-programmed into the satellite. A camera then photographs the screen for transmission to Earth, part of the Northern SPIRIT Consortium space mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 25, 12:39	6791	0.0008	408	419	92.83	51.64	264
NEUDOSE (NEUtron DOSimetry & Exploration) 1998-067VG 56315						Re-entered - 2023 Nov 29 Life 219 days
2U Cubesat from McMaster University, Canada and designed to investigate charged and neutral particles in the radiation dose received by humans in LEO.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 25, 12:39	6792	0.0008	408	420	92.85	51.64	246
YukonSat 1998-067VH 56316						Re-entered - 2023 Nov 11 Life 201 days
2U Cubesat from Yukon University - equipped with a boom-mounted camera for 'selfie' photography and a radio transmitter to broadcast pre-recoded stories about northern Canada, part of the Northern SPIRIT Consortium space mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 25, 12:39	6792	0.0008	409	419	92.85	51.64	238

2023-058 Falcon 9 Block 5 (Starlink Group 03-05) Vandenberg Space Force Base						2023 Apr 26, 13:40
Starlink 6038 2023-058A 56317						in space
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 14:41 UTC. Catalogue Number to be confirmed. All satellites expected to be injected initially into similar orbits at about 360 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 3, 18:00	6726	0.0003	346	350	91.50	97.66	246
Falcon 9 second stage uncatalogued						Re-entered - 2023 Apr 26 Life <1 day
Launched forty six Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-059 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Apr 28, 22:12
O3b mPower FM04 2023-059A 56367						in space
Second generation communications satellite, owned by SES, to provide broadband links between ground stations lying in the range ±45° latitude. In addition to the broad area coverage of 1st gen satellites, mPower satellites are equipped with spot beam aerials. Released from launch vehicle Apr 29 at 00:12 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 29, 08:36	11265	0.1877	2773	7001	198.31	8.60	182
O3b mPower FM03 2023-059B 56368						in space
Second generation communications satellite, owned by SES, to provide broadband links between ground stations lying in the range ±45° latitude. In addition to the broad area coverage of 1st gen satellites, mPower satellites are equipped with spot beam aerials. Released from launch vehicle Apr 29 at 00:05 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 29, 09:55	11262	0.1880	2767	7001	198.23	8.60	182
2023 May 8, 15:52	11380	0.1827	2922	7081	201.35	8.18	208
Falcon 9 second stage 2023-059C 56369						in space
Launched pair of O3b satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Apr 29, 09:55	11259	0.1881	2764	6998	198.15	8.59	182

2023-060 Falcon Heavy Kennedy Space Center						2023 May 1, 00:26
Viasat 3 F1 (Viasat 3 Americas) 2023-060A 56370						in space
Commercial comsat providing broadband services to North America for the aviation industry, government and private consumers. Separated from launch vehicle at 04:58 UTC. Continuous thrust used to raise orbit to operating height. Jul 12 - Viasat announced that main radio reflector had not deployed properly and efforts were under way to work round the problem. It eventually entered service with reduced comms capacity. Expected location 88°.9 west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 May 3, 21:33	40983	0.0009	34568	34642	1376.16	0.06	137
2023 May 6, 19:10	41216	0.0005	34817	34859	1387.91	0.05	84
2023 May 9, 16:11	41596	0.0002	35208	35227	1407.12	0.04	357
2023 May 11, 12:00	41712	0.0005	35313	35355	1413.04	0.03	27
2023 May 12, 14:24	41879	0.0003	35490	35512	1421.52	0.03	268
2023 May 14, 14:12	42465	0.0055	35854	36319	1451.44	0.02	35
2023 May 16, 19:12	42164	0.0001	35783	35790	1436.08	0.04	139	88°.9 W
Arcturus 2023-060B 56371						in space
Small comsat built and owned by Astranis Space Technologies Corp to provide broadband connectivity to Alaska. Separated from launch vehicle at 05:12 UTC. Expected location 163° west. Moved to graveyard orbit 2024 Jan 31.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 May 3, 21:29	40956	0.0010	34537	34619	1374.79	0.06	186
2023 May 7, 20:09	42240	0.0002	35853	35870	1439.92	0.06	146	162°.1 W
2023 May 8, 21:19	42191	0.0007	35781	35844	1437.42	0.06	355	162°.8 W
2023 May 9, 19:42	42165	0.0001	35782	35792	1436.12	0.06	35	162°.9 W
2024 Jan 31, 14:16	42166	0.0003	35776	35799	1436.14	0.53	243	163°.0 W
2024 Feb 1, 17:53	42398	0.0005	36001	36040	1448.05	0.53	220
2024 Mar 1, 02:29	42399	0.0004	36002	36040	1448.10	0.60	238
GS 1 (Gravity Space 1) 2023-060C 56372						in space
6U Cubesat built by Norwegian company Space Inventor for Gravity Space, hosting multiple payloads including: Nusantara H1 A - an Indonesian 'placeholder' communications package to reserve a geosynchronous slot for a future comsat, Orbit Guard - test payload from Infinite Orbits, capable of detecting and tracking other objects in orbit. Separated from launch vehicle at 05:05 UTC. Expected location - 116°.1 east. Tracking difficulties led to a slow start in drift orbit. Arrived on station August 16. 2023 November 12 then, after fulfilling its Nusantara 'placeholder' role, commenced eastward move, arrived 166° east 2023 December 20. Made one further move, to 89°.5 east then lost station-keeping ability around 2024 June.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 May 10, 12:00	41021	0.0010	34604	34683	1378.09	0.06	66
2023 May 22, 17:16	41017	0.0009	34603	34674	1377.84	0.09	51
2023 Jun 7, 00:49	41026	0.0117	34168	35128	1378.32	0.12	74
2023 Jun 13, 19:00	41121	0.0018	34670	34815	1383.08	0.14	298
2023 Jun 20, 14:50	41217	0.0010	34796	34882	1387.96	0.15	359
2023 Jun 28, 14:41	41360	0.0011	34937	35026	1395.16	0.17	357
2023 Jul 5, 23:45	41502	0.0028	35006	35242	1402.39	0.19	327
2023 Jul 12, 15:06	41627	0.0010	35206	35292	1408.71	0.20	343
2023 Jul 19, 03:35	41753	0.0011	35327	35422	1415.09	0.21	351
2023 Jul 27, 21:57	41928	0.0013	35497	35603	1424.01	0.24	353
2023 Jul 30, 19:30	42067	0.0018	35613	35765	1431.11	0.24	293	100°.0 E
2023 Aug 8, 19:02	42103	0.0005	35703	35747	1432.95	0.26	346	111°.9 E
2023 Aug 14, 23:42	42129	0.0002	35743	35759	1434.28	0.28	357	116°.2 E
2023 Aug 16, 19:15	42163	0.0002	35776	35794	1436.03	0.28	51	116°.5 E
2023 Nov 3, 18:24	42163	0.0000	35784	35786	1436.02	0.30	239	116°.4 E
2023 Nov 12, 17:19	42152	0.0002	35767	35780	1435.42	0.28	301	116°.6 E
2023 Nov 18, 17:46	42062	0.0003	35670	35697	1430.84	0.30	279	121°.7 E
2023 Nov 22, 18:18	41982	0.0003	35592	35617	1426.79	0.31	236
2023 Dec 20, 11:33	42193	0.0002	35807	35823	1437.53	0.40	238	165°.7 E
2023 Dec 28, 15:31	42165	0.0003	35775	35799	1436.11	0.42	202	165°.5 E
2024 Mar 9, 14:49	42165	0.0002	35778	35795	1436.10	0.58	254	165°.7 E
2024 Mar 18, 11:54	42165	0.0002	35778	35795	1436.09	0.60	263	165°.7 E
2024 Mar 29, 10:46	42252	0.0004	35857	35891	1440.57	0.63	220
2024 May 14, 09:13	42226	0.0020	35761	35934	1439.21	0.75	24	90°.6 E
2024 May 26, 22:32	42165	0.0007	35758	35816	1436.11	0.79	288	89°.5 E
2025 Feb 27, 18:28	42172	0.0005	35775	35813	1436.47	1.50	260	65°.7 E
Falcon 9 upper stage 2023-060D 56373						in space
Launched Viasat 3 Americas, GS 1 and Arcturus.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 10, 14:24	40956	0.0010	34536	34619	1374.77	0.06	179

2023-061 Falcon 9 Block 5 (Starlink Group 05-06) Cape Canaveral Space Force Station						2023 May 4, 07:31
Starlink 6156 2023-061A 56374						in space
One member of a simultaneously-launched cluster of fifty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 08:35 UTC. All satellites expected to be injected initially into similar orbits at about 360 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 10, 07:41	6724	0.0002	345	348	91.46	43.01	199
Falcon 9 second stage uncatalogued						Re-entered - 2023 May 4 Life <1 day
Launched fifty six Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-062 Electron (Rocket Like A Hurricane) Rocket Lab Launch Complex, New Zealand						2023 May 8, 01:00
TROPICS 05 (Time-Resolved Observations of Precipitation structure and storm Intensity with a Constellation of Smallsats) 2023-062A 56442						in space
3U Cubesat - one of a simultaneously launched pair from NASA to to study thermodynamics of the troposphere and precipitation in storm centres within the tropical region of the Earth's atmosphere. Constellation will eventually consist of four satellites, the original aim was six satellites but two were lost in a launch failure during 2022. Released from launch vehicle at 01:33 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 8, 19:46	6925	0.0008	541	553	95.59	32.74	229
TROPICS 06 (Time-Resolved Observations of Precipitation structure and storm Intensity with a Constellation of Smallsats) 2023-062C 56444						in space
3U Cubesat - one of a simultaneously launched pair from NASA to to study thermodynamics of the troposphere and precipitation in storm centres within the tropical region of the Earth's atmosphere. Constellation will eventually consist of four satellites, the original aim was six satellites but two were lost in a launch failure during 2022. Released from launch vehicle at 01:33 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 8, 18:08	6922	0.0016	532	555	95.52	32.74	223
Electron third stage (kick stage) 2023-062B 56443						Re-entered - 2025 Apr 12 Life 705 days
Launched two satellites for NASA's TROPICS constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 8, 19:45	6923	0.0014	535	554	95.54	32.73	229
Electron second stage 2023-062D 56445						in space
Launched two satellites for NASA's TROPICS constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 8, 18:09	6928	0.0017	538	562	95.66	35.49	236

2023-063 CZ 7 (Y-7) Wenchang Space Centre						2023 May 10, 13:22
Tianzhou 6 2023-063B 56446						Re-entered - 2024 Jan 19 Life 254 days
Supplies to Chinese Space Station - support for the upcoming Shenzhou 16 mission. Initial orbit similar to the upper stage rocket. Docked with rear port of Tianhe module at 21:16 UTC on day of launch. Tianli, a 12U Cubesat was contained in a dispenser attached to its exterior, expected to be released before mission end. Undocked 2024 January 12 at 08:02 UTC. Released Dalian 1 Cubesat Jan 18 then a thruster firing January 19 at about 11:55 UTC led to destructive re-entry above the southern Pacific Ocean at 12:37 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 10, 19:12	6751	0.0004	371	375	92.01	41.51	173
2023 May 10, 22:27	6757	0.0007	374	384	92.13	41.48	231
2024 Jan 12, 03:29	6758	0.0005	377	383	92.15	41.47	92
2024 Jan 13, 18:11	6754	0.0010	369	383	92.07	41.47	120
Dalian 1 (Lianli) 2023-063C 58816						Re-entered - 2024 Apr 23 Life 349 days
12U Cubesat carried into orbit by Tianzhou 6 and then released from an external dispenser on Tianzhou 2024 January 18 after its departure from CSS. Fitted with a high resolution imaging system and acting as a demonstrator of new satellite systems including a 3D printed launch dispenser.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 Jan 19, 01:34	6755	0.0009	371	383	92.08	41.47	151
CZ 7 third stage 2023-063A 56447						Re-entered - 2023 May 21 Life 11 days
Launched Tianzhou 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 10, 23:50	6636	0.0089	199	317	89.66	41.48	177

2023-064 Falcon 9 Block 5 (Starlink Group 02-09) Vandenberg Space Force Base						2023 May 10, 20:09
Starlink 5990 2023-064A 56448						in space
One member of a simultaneously-launched cluster of fifty one LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 20:34 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 16, 16:00	6679	0.0026	284	318	90.54	70.00	160
Falcon 9 second stage uncatalogued						in space
Launched fifty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-065 Falcon 9 Block 5 (Starlink Group 05-09) Cape Canaveral Space Force Station						2023 May 14, 05:03
Starlink 5775 2023-065A 56503						in space
One member of a simultaneously-launched cluster of fifty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:08 UTC. All satellites expected to be injected initially into similar orbits at about 360 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 19, 18:00	6717	0.0002	338	340	91.32	43.01	262
Falcon 9 second stage uncatalogued						in space
Launched fifty six Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-066 CZ 3B Xichang Space Centre						2023 May 17, 02:49
Beidou 56 (Beidou-3 G-4) 2023-066A 56564						in space
On orbit spare phase 2 satellite in China's navigation satellite system. It also provides time and messaging services for the Asia-Pacific region. Probably moved to geosynchronous drift orbit May 18. Location 160° east put it alongside the 13 year old Beidou 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 May 17, 05:53	24388	0.7304	198	35823	631.73	28.42	180
2023 May 25, 14:26	42165	0.0006	35761	35813	1436.12	3.10	183	160°.0 E
CZ 3B fourth stage 2020-066B 56565						in space
Launched Beidou 56.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 17, 05:47	23658	0.7228	179	34381	603.58	28.42	179

2023-067 Falcon 9 Block 5 (Starlink Group 06-03) Cape Canaveral Space Force Station						2023 May 19, 06:19
Starlink 30122 2023-067A 56688						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 07:24 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 25, 14:00	6709	0.0002	330	332	91.16	43.00	261
Falcon 9 second stage uncatalogued						Re-entered - 2023 May 19 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-068 Falcon 9 Block 5 Vandenberg Space Force Base						2023 May 20, 13:16
OneWeb 0561 2023-068A 56710						in space
Broadband distribution satellite for the UK company OneWeb. One of 16 similar satellites carried on this launch, all initially in similar orbits. One satellite carried secondary payload, JoeySat, to test alternative communication technologies.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 23, 16:00	6998	0.0010	613	627	97.11	86.68	207
2023 May 26, 22:00	6998	0.0011	613	628	97.11	86.68	194
2023 May 28, 22:00	7010	0.0011	624	639	97.34	86.70	187
2023 May 30, 12:33	7021	0.0013	634	652	97.58	86.73	181
Iridium 181 (Iridium Next) 2023-068S 56726						in space
Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services. One of ten similar satellites on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 22, 16:28	6997	0.0013	610	628	97.08	86.67	213
Falcon 9 second stage						in space
Launched 16x OneWeb and 5x Iridium satellites.
Orbit parameters awaited

2023-069 CZ 4C Jiuquan Space Centre						2023 May 21, 08:00
Macau Science 1A 2023-069A 56731						in space
One of a simultaneously-launched pair of satellites to study the geomagnetic field at low latitudes. Equipped with high precision magnetometers. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 21, 14:22	6854	0.0031	454	497	94.12	41.00	138
Macau Science 1B 2023-069B 56732						in space
One of a simultaneously-launched pair of satellites to study the geomagnetic field at low latitudes. Equipped with a high energy particle detector and a solar x-ray telescope. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 21, 15:58	6853	0.0031	453	496	94.10	41.00	139
Luojia-2 01 2023-069C 56733						Re-entered - 2025 Mar 25 Life 674 days
Small satellite equipped with an imaging system and an intelligent processing system to prepare data before transmission to the ground. Also equipped with a (probably laser) communications system to provide links to other satellites. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 21, 14:22	6852	0.0029	454	494	94.08	41.00	136
CZ 2C second stage 2023-069D 56734						Re-entered - 2024 Apr 24 Life 339 days
Launched Macau Science 1A and 1B, and Luojia 2-01. Orbit lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 21, 17:16	6807	0.0054	392	465	93.15	41.20	40

2023-070 Falcon 9 Block 5 (Axiom 2) Kennedy Space Center						2023 May 21, 21:37
SpaceX Axiom 2 (Dragon Freedom flight #2) 2023-070A 56739						Re-entered - 2023 May 31 Life 10 days Returned to Earth
Privately funded (Axiom Space) science mission to ISS using SpaceX Crew Dragon. Crew consists of Peggy Whitson (Commander), John Shoffner, and Saudi Arabia Mission Specialists Rayyanah Barnarwi and Ali Alqarni. Separated from launch vehicle at 21:49 UTC. Docked with upward facing port of ISS Harmony module May 22 at 13:12 UTC. Undocked May 30 at 15:05 UTC carrying original crew. Retro-fire May 31 at 02:13 UTC led to splashdown in the Gulf of Mexico at 03:04 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 22, 00:56	6635	0.0070	211	303	89.64	51.65	211
2023 May 22, 06:58	6784	0.0002	405	407	92.68	51.65	322
2023 May 22, 08:03	6795	0.0005	413	420	92.90	51.64	5
2023 May 30, 05:24	6794	0.0005	412	420	92.89	51.64	36
Falcon 9 second stage uncatalogued						Re-entered - 2023 May 21 Life <1 day
Launched SpaceX Axiom 2. Caused to re- enter above the southern Pacific Ocean about 45 mins after lift-off.
Not Catalogued - orbit parameters unavailable
Crew Dragon trunk module 2023-070B 56751						Re-entered - 2023 Aug 12 Life 83 days
Released from SpaceX Axiom 2 2023 May 31 at 02:08 UTC prior to retro-fire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 3, 22:23	6734	0.0065	312	400	91.66	51.44	169

2023-071 Soyuz-2.1a Baikonur Cosmodrome						2023 May 24, 12:56
Progress MS-23 (Progress 7K-MS №453) 2023-071A 56740						Re-entered - 2023 Nov 29 Life 189 days
Supplies to ISS. Docked with the Poisk module of the ISS at 16:19 UTC, about two minutes earlier than planned. Undocked November 29 at 07:55:25 UTC. Retro-fire at 11:02 UTC above central Asia led to destructive re-entry with any surviving debris hitting the surface of the southern Pacific Ocean around 11:55 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 24, 13:25	6584	0.0028	187	224	88.61	51.63	78
2023 May 24, 19:14	6794	0.0005	413	420	92.89	51.64	15
2023 Nov 28, 18:05	6795	0.0001	416	418	92.91	51.64	353
Soyuz third stage 2023-071B 56741						Re-entered - 2023 May 26 Life 2 days
Launched Progress MS-23.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 24, 13:24	6582	0.0030	184	224	88.57	51.67	65

2023-072 KSLV-II (Nuri) Naro Space Centre, South Korea						2023 May 25, 09:24
NEXTSat 2 2023-072A 56743						in space
Small satellite from South Korea's Korea Advanced Institute of Science and Technology carrying a demonstrator payload for Earth observation using radar imaging. Separated from launch vehicle at 09:37 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 May 26, 06:03	6923	0.0007	540	550	95.55	97.54	300	18:00
SNIPE 4 (Small scale magNetospheric and Ionospheric Plasma Experiment) 2023-072B 56744						in space
6U Cubesat - one of four simultaneously-launched satellites from South Korea's Korea Astronomy and Space Science Institute. The satellites will fly in a variable formation and will study changes in plasma flows and densities in near-Earth space. Separated from launch vehicle at 09:39 UTC. One of the four failed to separate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 26, 06:02	6923	0.0007	540	550	95.55	97.55	297
SNIPE 2 (Small scale magNetospheric and Ionospheric Plasma Experiment) 2023-072C 56745						in space
6U Cubesat - one of four simultaneously-launched satellites from South Korea's Korea Astronomy and Space Science Institute. The satellites will fly in a variable formation and will study changes in plasma flows and densities in near-Earth space. Separated from launch vehicle at 09:39 UTC. One of the four failed to separate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 26, 06:03	6923	0.0007	540	550	95.54	97.55	307
SNIPE 1 (Small scale magNetospheric and Ionospheric Plasma Experiment) 2023-072G 56749						in space
6U Cubesat - one of four simultaneously-launched satellites from South Korea's Korea Astronomy and Space Science Institute. The satellites will fly in a variable formation and will study changes in plasma flows and densities in near-Earth space. Separated from launch vehicle at 09:38 UTC. One of the four failed to separate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 26, 06:02	6921	0.0009	537	550	95.51	97.53	314
JAC 2023-072xx						in space
3U Cubesat from South Korean company Justek launched to verify the design. Also carries an optical Earth-imaging payload. Separated from launch vehicle at 09:37 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
KSat3U 2023-072xx						in space
3U Cubesat from South Korean company Kairo Space for meteorogical studies. Also equipped with an air brake. Separated from launch vehicle at 09:38 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
Lumir T1 2023-072xx						in space
6U Cubesat from South Korean company Lumir, acting as a demonstrator for the company's satellite design and equipped with a cosmic ray studies payload. Separated from launch vehicle at 09:37 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
KSLV II third stage 2023-072H 56750						in space
Launched Nextsat 2 and seven Cubesats. A Cubesat, SNIPE 3 failed to separate after launch and remains attached.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 25, 22:10	6906	0.0025	511	545	95.20	97.50	17

2023-073 Electron (Coming To A Storm Near You) Rocket Lab Launch Complex, New Zealand						2023 May 26, 03:46
TROPICS 03 (Time-Resolved Observations of Precipitation structure and storm Intensity with a Constellation of Smallsats) 2023-073B 56753						in space
3U Cubesat - one of a simultaneously launched pair from NASA to to study thermodynamics of the troposphere and precipitation in storm centres within the tropical region of the Earth's atmosphere. Separated from launch vehicle at 04:19 UTC. Completes the four satellite constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 26, 11:08	6925	0.0011	539	555	95.59	32.74	232
TROPICS 07 (Time-Resolved Observations of Precipitation structure and storm Intensity with a Constellation of Smallsats) 2023-073C 56754						in space
3U Cubesat - one of a simultaneously launched pair from NASA to to study thermodynamics of the troposphere and precipitation in storm centres within the tropical region of the Earth's atmosphere. Separated from launch vehicle at 04:19 UTC. Completes the four satellite constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 26, 11:08	6922	0.0016	533	555	95.52	32.74	221
Electron third stage (kick stage) 2023-073A 56752						in space
Launched a pair of TROPICS satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 26, 11:12	6925	0.0013	537	556	95.58	32.74	218
Electron second stage 2023-073D 56755						in space
Launched a pair of TROPICS satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 26, 11:12	6920	0.0029	522	562	95.48	35.47	186

2023-074 Soyuz-2.1a + Fregat Vostochny Cosmodrome						2023 May 26, 21:14
Condor-FKA №1 2023-074A 56756						in space
Earth imaging satellite using radar. Separated from Fregat rocket stage at 22:19 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 May 27, 03:51	6888	0.0002	509	512	94.83	97.44	88	18:30
2024 Nov 26, 02:54	6885	0.0002	506	508	94.76	97.44	89	18:29
Fregat rocket stage uncatalogued						Re-entered - 2023 May 26 Life <1 day
Launched Condor-FKA №1. Fired twice after separation from launch Soyuz third stage in order to achieve desired orbit for the payload, then caused to re-enter at about 23:35 UTC above the southern Pacific Ocean.
Not Catalogued - orbit parameters unavailable

2023-075 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 May 27, 04:30
Badr 8 2023-075A 56757						in space
7th Generation comsat owned by Arabsat and serving the Middle East and North Africa. Orbit circularised from GTO using electric propulsion. Separated from launch vehicle at 05:07 UTC. Expected location 26° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 May 27, 07:42	37191	0.8176	405	61221	1189.65	27.83	180
2023 Jun 1, 16:48	37703	0.8106	763	61887	1214.31	26.45	183
2023 Jun 7, 15:49	39361	0.7973	1600	64365	1295.27	23.13	183
2023 Jun 12, 05:25	40469	0.7875	2221	65960	1350.32	20.93	184
2023 Jun 16, 00:39	41523	0.7744	2989	67301	1403.44	18.95	185
2023 Jun 23, 21:29	42881	0.7460	4512	68494	1472.84	15.72	187
2023 Jun 29, 12:00	43365	0.7171	5891	68082	1497.83	13.41	188
2023 Jul 5, 12:04	42631	0.6977	6511	65995	1460.00	11.46	188
2023 Jul 13, 23:03	43379	0.6485	8871	65130	1498.57	9.02	190
2023 Jul 20, 12:04	45021	0.5815	12462	64823	1584.44	7.43	191
2023 Jul 28, 06:08	45516	0.5204	15453	62823	1610.68	5.95	192
2023 Aug 7, 18:29	45668	0.4361	19374	59207	1618.76	4.44	195
2023 Aug 14, 20:02	45231	0.3720	22026	55680	1595.56	3.41	14
2023 Aug 21, 11:52	44877	0.3108	24552	52446	1576.89	2.71	195
2023 Aug 28, 01:50	44421	0.2456	27134	48951	1552.88	2.06	195
2023 Sep 6, 20:45	43667	0.1527	30622	43955	1513.52	1.20	15
2023 Sep 11, 17:34	43220	0.1059	32267	41417	1490.36	0.84	193
2023 Sep 19, 21:54	42349	0.0335	34554	37388	1445.53	0.27	189
2023 Sep 26, 05:02	42166	0.0002	35778	35797	1436.14	0.07	60	27°.0 E
Falcon 9 second stage 2023-075B 56758						in space
Launched BADR 8.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 27, 07:07	37337	0.8182	409	61508	1196.65	27.74	180

2023-076 GSLV Mk II F12 Satish Dhawan Space Centre						2023 May 29, 05:12
NVS 01 (IRNSS 1J) 2023-076A 56759						in space
Second generation navsat in India's Regional Navigation Satellite System to provide navigation services to the Indian subcontinent and an area extending 1500 km beyond it. Will replace IRNSS 1G (41469, 2016-027A) that suffered a failure in its navigation system payload. Expected location 129°.5 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 May 29, 11:39	26473	0.7521	184	40005	714.42	19.30	179
2023 May 30, 18:44	30504	0.5204	8250	40001	883.67	10.81	178
2023 Jun 1, 12:38	37033	0.2534	21269	40040	1182.07	6.81	177
2023 Jun 1, 14:58	36929	0.2537	21180	39921	1177.07	6.81	176
2023 Jun 5, 07:12	42275	0.0010	35855	35938	1441.74	4.97	183
2023 Jun 7, 06:44	42223	0.0010	35803	35887	1439.08	4.96	184	130°.6 E
2023 Jun 9, 15:01	42220	0.0010	35801	35883	1438.92	4.94	193	128°.9 E
2023 Jun 9, 18:56	42186	0.0009	35768	35847	1437.18	4.96	5	129°.5 E
2023 Jun 9, 19:12	42145	0.0009	35728	35805	1435.07	4.96	47	129°.6 E
2023 Jun 12, 12:19	42153	0.0009	35735	35815	1435.49	4.95	340	129°.6 E
2023 Jun 12, 17:28	42164	0.0004	35768	35804	1436.08	4.95	360	129°.6 E
GSLV upper stage 2023-076B 56760						in space
Launched NVS 01.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 29, 10:23	26435	0.7519	180	39933	712.89	19.33	179

2023-077 CZ 2F Jiuquan Space Centre						2023 May 30, 01:31
Shenzhou 16 2023-077A 56761						Re-entered - 2023 Oct 31 Life 154 days Returned to Earth
Crew to CSS - Jing Haipeng (commander), Zhu Yangzhu (pilot and flight engineer) and Gui Haichao (payload specialist). Separated from launch vehicle at 01:40 UTC. Docked with the downward-facing port of Tianhe at 08:29 UTC. Undocked carrying its original crew October 30 at 12:37 UTC. Retrofire at about 23:27 UTC led to landing about 50 km north of the Jiuquan launch site October 31 at 00:11 UTC. Initial orbit is an estimate based on Chinese data.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 30, 01:41	6659	0.0121	200	361	90.12	41.34	266
2023 May 30, 10:18	6767	0.0004	387	392	92.34	41.47	268
2023 Oct 29, 09:08	6765	0.0004	383	389	92.28	41.47	349
2023 Oct 30, 17:56	6762	0.0005	381	387	92.23	41.47	43
CZ 2F third stage 2023-077F 56766						Re-entered - 2023 Jun 12 Life 13 days
Launched Shenzhou 16.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 May 30, 10:31	6648	0.0112	196	345	89.92	41.47	129
Shenzhou 16 Orbital Module 2023-077G 58198						Re-entered - 2024 Jul 22 Life 419 days
Released from Shenzhou 16 on Oct 31 shortly before 23:20 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 31, 16:56	6761	0.0007	378	388	92.21	41.49	50

2023-F05 - failed to reach orbit Chollima 1 (Improved UNHA-3?) Sohae Launch Centre						2023 May 30, 21:27
Malligyong 1 flight model 1
North Korean government/military optical imaging satellite aimed at 500 kilometre, sun-synchronous orbit, lost when the launch vehicle second stage either failed to separate or failed to fire. Impacted the Yellow Sea still attached to the rocket.

2023-078 Falcon 9 Block 5 (Starlink Group 02-10) Vandenberg Space Force Base						2023 May 31, 06:02
Starlink 6197 2023-078A 56767						in space
One member of a simultaneously-launched cluster of fifty two LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:19 UTC. Catalogue Number to be confirmed. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 6, 16:00	6678	0.0029	281	319	90.52	70.00	162
Falcon 9 second stage uncatalogued						Re-entered - 2023 May 31 Life <1 day
Launched fifty two Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-079 Falcon 9 Block 5 (Starlink Group 06-04) Cape Canaveral Space Force Station						2023 Jun 4, 12:20
Starlink 30119 2023-079A 56823						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 13:25 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 9, 18:00	6708	0.0001	329	331	91.13	43.01	272
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jun 4 Life <1 day
Launched twenty two second generation Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-080 Falcon 9 Block 5 Kennedy Space Center						2023 Jun 5, 15:47
SpaceX Dragon 2 CRS-28 2023-080A 56845						Re-entered - 2023 Jun 30 Life 25 days Returned to Earth
Carrying a cargo to/from the ISS under NASA's Commercial Resupply Services (CRS) contract. Separated from launch vehicle at 15:59 UTC. Docked with the upward facing port of the Harmony module of ISS June 6 at 09:54 UTC. Undocked June 29 at 16:30 UTC. Retro-fire Jun 30 at about 13:41 UTC led to splash down in the Atlantic Ocean off the coast of Florida at 14:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 5, 22:08	6690	0.0129	226	398	90.76	51.57	252
2023 Jun 6, 01:11	6783	0.0003	402	407	92.65	51.65	153
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jun 5 Life <1 day
Launched Dragon CRS-28. Caused to re-enter after releasing Dragon, at about 16:45 UTC.
Not Catalogued - orbit parameters unavailable
Dragon 2 trunk module 2023-080B 57211						Re-entered - 2023 Aug 4 Life 60 days
Separated from Dragon 2 CRS-28 2023 June 28 prior to retrofire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 3, 15:07	6701	0.0106	252	394	90.99	51.63	166

2023-081 Lijian 1, Kinetica 1 (Y-2) Jiuquan Space Centre						2023 Jun 7, 04:10
Tianyi 26 2023-081F 56851						in space
Reportedly a medium resolution optical Earth-imaging satellite. Also carries a small thruster system for orbit adjustment that was operated for the first time on June 29 and for a final time om July 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 15:17	6880	0.0014	493	511	94.66	97.42	232
2023 Jun 28, 22:10	6879	0.0014	491	511	94.64	97.42	203
2023 Jun 29, 10:48	6880	0.0014	492	511	94.65	97.42	201
2023 Jul 5, 08:52	6882	0.0015	494	514	94.69	97.42	179
2023 Jul 6, 08:34	6883	0.0014	495	515	94.73	97.42	177
2023 Jul 11, 03:53	6885	0.0012	498	515	94.76	97.42	159
2023 Jul 15, 02:46	6891	0.0003	511	515	94.89	97.42	129
2023 Jul 18, 02:01	6896	0.0001	517	519	94.99	97.42	90
CXPD Cubesat 2023-081xx						in space
6U Cubesat? - equipped with an x-ray polarisation detector. Demonstrator for an instrument that will ultimately be incorporated into the Chinese space station.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0015	490	512	94.64	97.41	235	10:29
Fucheng 1 2023-081xx						in space
Commercial remote sensing satellite equipped with a radar imager from the Mianyang Fucheng Satellite Factory. Released from the launch vehicle at 04:23 UTC. First of six in a constellation referred to as "Mianyiang".
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0015	490	512	94.64	97.41	235	10:29
Shiyan 24A (Test 24A) 2023-081xx						in space
Small satellite carrying an unspecified demonstration payload, one of a pair carried on the same launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0015	490	512	94.64	97.41	235	10:29
Shiyan 24B (Test 24B) 2023-081xx						in space
Small satellite carrying an unspecified demonstration payload, one of a pair carried on the same launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0015	490	512	94.64	97.41	235	10:29
Xi'an Hangtou 8 2023-081xx						in space
First satellite in a planned constellation of 128 Earth imaging satellites. Payload includes a laser communication system. Name to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0015	490	512	94.64	97.41	235	10:29
20x unidentified satellites 2023-081						in space
Cluster of unidentified satellites reportedly carried on the 2023-081 launch. Confirmation awaited of whether all of them separated from the launch vehicle. All satellites are in similar orbits
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6879	0.0015	490	512	94.64	97.41	235
Lijian 1 third stage 2023-081Z 56869						Re-entered - 2023 Nov 2 Life 148 days
Launched a reported 26 small satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:34	6778	0.0163	289	511	92.56	97.38	342

2023-082 Kuaizhou 1A Jiuquan Space Centre						2023 Jun 9, 02:35
Longjiang 3 2023-082A 56874						in space
Small satellite from the Harbin Institute of Technology to demonstrate and test its design in the form of a flat panel. Carries a broadband internet communications system. Originally set for launch 2023 May 28 but delayed, probably by a technical issue either with the satellite or the launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 9, 10:26	6873	0.0007	490	500	94.52	49.13	265
Kuaizhou 1A third stage 2023-082B 56875						Re-entered - 2023 Jun 12 Life 3 days
Launched Longjiang 3. Orbit lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 9, 09:59	6728	0.0335	125	576	91.54	49.02	106

2023-083 Falcon 9 Block 5 (Starlink Group 05-11) Cape Canaveral Space Force Station						2023 Jun 12, 07:10
Starlink 6206 2023-083A 56876						in space
One member of a simultaneously-launched cluster of fifty two Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 08:15 UTC. Catalogue Number to be confirmed. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 16:00	6729	0.0002	350	352	91.55	43.00	259
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jun 12 Life <1 day
Launched fifty three Starlink satellites. Expected to be caused to re-enter above the Indian Ocean at about 09:15 UTC.
Not Catalogued - orbit parameters unavailable

2023-084 Falcon 9 Block 5 (Transporter 8) Vandenberg Space Force Base						2023 Jun 12, 21:35
Otter Pup 2023-084B 56933						in space
Small satellite to demonstrate rendezvous and station keeping, intended eventually re-attach itself to SN3. Released Jun 12 but was unable to carry out its mission because of the high rotation rate imparted by Orbiter SN3, and the fact that SN3 was unable to charge its batteries.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 13:14	6908	0.0009	524	536	95.24	97.51	171
GEI-SAT Precursor 2023-084C 56934						in space
Small satellite from the Satlantis company of Spain demonstrating an infrared Earth imaging system to detect methane emissions. Released from launch vehicle at L+ 01:00:44
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 14:49	6908	0.0010	523	537	95.23	97.51	198
FossaSat 2E14 (FEROX) 2023-084E 56936						Re-entered - 2024 May 30 Life 353 days
Pocketqbe satellite - details to follow. Released from launch vehicle at L+ 00:59:59. One of four similar satellites carried on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 13:13	6907	0.0009	523	535	95.22	97.51	201
EIVE (Exploratory In-Orbit Verification of an E/W-Band satcom link) 2023-084F 56937						Re-entered - 2025 Apr 15 Life 673 days
6U Cubesat from the University of Stuttgart to demonstrate radio communications in the 71-76 GigaHertz range. Released from launch vehicle at L+ 01:01:06.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 14:48	6908	0.0009	523	536	95.22	97.51	196
Tiger 4 (Layan 23) 2023-084H 56939						in space
6U Cubesat from OQ Technology equipped with a 5G internet communications payload. Released from launch vehicle at L+ 01:04:03.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:57	6907	0.0010	522	536	95.21	97.51	189
MISR B (Modular Intelligence, Surveillance, and Reconnaissance) 2023-084J 56940						Re-entered - 2024 Oct 8 Life 484 days
6U Cubesat for US Special Operations Command, payload details not available. Released from launch vehicle at L+ 01:03:51.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:56	6906	0.0011	521	536	95.20	97.51	190
XVI 2023-084L 56942						in space
12U Cubesat - demonstrator payload from Viasat of US Military "Link 16" encrypted communications system for beyond line-of-sight communications. May work with the SDA Tranche 0 satellites (launch 2023-050). Released from launch vehicle at L+ 01:03:39.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:56	6906	0.0011	520	536	95.20	97.52	190
ÑuSat 40 (Carolyn Shoemaker) 2023-084M 56943						in space
Small satellite from Satellogic of Argentina providing Earth images in the visible and infrared parts of the spectrum using real-time imaging and video. Released from launch vehicle at L+ 01:04:17. One of four similar satellites carried on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:55	6906	0.0011	520	536	95.19	97.51	185
Grégoire 2023-084Q 56946						in space
Small satellite from Belgian company Aerospacelab to demonstrate its space platform. Released from launch vehicle at L+ 01:09:43
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:54	6906	0.0012	519	536	95.18	97.51	185
ICEYE X23 2023-084T 56949						in space
Small satellite fitted with a sythetic aperture radar for Earth surface imaging. Released from launch vehicle at L+ 00:59:59. One of four similar satellites carried on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jun 20, 17:53	6905	0.0012	519	536	95.18	97.51	183	13:18
QPS-SAR 6 (Amateru-III) 2023-084V 56951						Re-entered - 2024 Nov 17 Life 524 days
Commercial satellite from Japanese company iQPS, equipped with an Earth imaging radar. First in a constellation that will ultimately consist of 36 satellites. Released from launch vehicle at L+ 01:19:30.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:53	6905	0.0013	518	536	95.17	97.51	183
Runner 1 2023-084X 56953						in space
Small satellite from Terran Orbit to be operated by Israeli company ImageSat International on behalf of the Chilean National Space Program. Carries an Earth imaging system. Released from launch vehicle at L+ 01:19:50.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:52	6905	0.0014	517	536	95.17	97.51	181
HotSat 1 2023-084Y 56954						in space
Small satellite from SatVu equipped with an infrared imaging system to provide still and video images. Released from launch vehicle at L+ 01:15:47
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:52	6905	0.0013	518	536	95.17	97.51	185
Blackjack Aces 1 2023-084AA 56956						in space
Demonstrator satellite for the US DARPA, equipped with an optical inter-satellite communication system. Released from launch vehicle at L+ 01:21:33. One of four similar satellites carried on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:51	6904	0.0013	517	536	95.16	97.51	186
ION SCV-011 (Savvy Simon) 2023-084AB 56957						in space
Satellite Carrier Vehicle built by D-Orbit. Released from launch vehicle at L+ 01:20:16. Satellites: Outpost Mission 1 - Carrying a set of hosted payloads, names unknown, released June 15, PocketQube satellites - six in total, released June 21 & 22, Speisat - released late-June, unidentified - released August 14. Other payloads to follow.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:51	6905	0.0014	517	536	95.16	97.51	184
GHOSt 3 (Global Hyperspectral Observation Satellite) 2023-084AC 56958						in space
Commercial satellite in a planned constellation of six equipped with a multi-spectral Earth imaging system. Released from launch vehicle at L+ 01:17:59
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:51	6904	0.0014	517	536	95.16	97.51	186
W-Series 1 (Photon 4) 2023-084AD 56959						Re-entered - 2024 Feb 21 Life 254 days
Satellite based on Rocket Labs Photon chassis and equipped with an automated laboratory to study formation of molecules in microgravity. Also equipped with a demonstrator re-entry vehicle to return to Earth at mission end. Released from launch vehicle at L+ 01:22:38.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:50	6904	0.0014	516	536	95.16	97.51	186
Tomorrow R2 2023-084AG 56962						in space
Small satellite from US company Tomorrow.io to demonstrate a weather radar sytem to be used in a future constellation of LEO meteorological satellites. Released from launch vehicle at 11;42 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:50	6904	0.0014	516	536	95.15	97.51	184
AFR 1 (ABA First Runner) 2023-084AJ 56964						in space
Small satellite from Azista BST Aerospace equipped with an optical remote sensing payload. Released from launch vehicle at L+ 01:07:57.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 13:04	6904	0.0015	516	536	95.15	97.51	185
Droid.001 2023-084AK 56965						in space
Small satellite from Turion Space equipped with an imaging system to detect and track satellites and debris in LEO. Released from launch vehicle at L+ 01:03:23.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:49	6904	0.0015	516	536	95.15	97.51	181
MuSat 1 2023-084AM 56967						Re-entered - 2024 Dec 11 Life 548 days
Small satellite from Muon Space to demonstrate its design of a software-defined payload. Released from launch vehicle at L+ 01:06:35.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 16:13	6903	0.0015	515	535	95.13	97.51	184
Lemur 2 (Embrionovs) 2023-084AQ 56970						in space
6U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors and a secondary payload. Lemur-2 satellites are named after development and support team members. Released from launch vehicle at L+ 01:17:59. One of three similar satellites carried on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:47	6903	0.0016	513	536	95.13	97.52	183
MISR A (Modular Intelligence, Surveillance, and Reconnaissance) 2023-084AR 56971						Re-entered - 2024 Oct 2 Life 478 days
6U Cubesat for US Special Operations Command, payload details not available. Released from launch vehicle at L+ 01:10:42,
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:47	6902	0.0015	514	535	95.12	97.51	177
Skykraft 3A 2023-084BB 56981						Re-entered - 2024 Dec 15 Life 552 days
Small satellite from Australia as a demonstrator for a 200 satellite system to provide air traffic control services in areas away from convential ground station coverage. Released from Skykraft 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 11:32	6905	0.0013	518	536	95.18	97.51	184
Skykraft 3C 2023-084BC 56228						Re-entered - 2025 Feb 21 Life 620 days
Small satellite from Australia as a demonstrator for a 200 satellite system to provide air traffic control services in areas away from convential ground station coverage. Released from Skykraft 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 06:52	6904	0.0014	517	536	95.16	97.52	133
SpaceBEE 168 2023-084BE 56984						Re-entered - 2024 Oct 7 Life 483 days
0.25U Cubesat from Swarm Technologies for two-way communications system in LEO. Swarm intends to operate a 150 satellite constellation. It also carries a GPS receiver to help determine its location. Released from launch vehicle at L+ 01:03:13. One of telve similar satellites carried on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 14:34	6902	0.0017	512	535	95.10	97.52	183
Ayris 2 2023-084BG 56986						Re-entered - 2025 May 13 Life 701 days
Mission details to follow. Released from launch vehicle at L+ 01:01:10.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:44	6902	0.0017	512	535	95.10	97.52	179
AII-DELTA 2023-084BH 56987						Re-entered - 2025 Jan 28 Life 596 days
Mission details to follow. Released from launch vehicle at L+ 01:00:31.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:44	6902	0.0017	512	535	95.10	97.51	175
Ayris 1 2023-084BJ 56988						Re-entered - 2025 May 13 Life 701 days
Mission details to follow. Released from launch vehicle at L+ 01:00:54.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:44	6902	0.0017	512	535	95.10	97.51	177
Outpost Ferry 1-01 (Mission 1) 2023-084BK 56226						in space
3U Cubesat from US company Outpost. Test of electronics and comms systems for a future recoverable and reusable satellite. Released from ION SCV 11 mid-July.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 14:33	6902	0.0012	515	532	95.11	97.51	132
Skykraft 3B 2023-084BL 56227						Re-entered - 2024 Dec 3 Life 540 days
Small satellite from Australia as a demonstrator for a 200 satellite system to provide air traffic control services in areas away from convential ground station coverage. Released from Skykraft 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 14:47	6904	0.0014	517	535	95.15	97.52	132
Skykraft 3 2023-084BN 56229						in space
Small satellite from Australia as a demonstrator for a 200 satellite system to provide air traffic control services in areas away from convential ground station coverage. Released from launch vehicle at L+01:17:17.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 06:52	6905	0.0014	517	536	95.16	97.51	132
Istanbul 2023-084BP 56230						Re-entered - 2024 Apr 9 Life 302 days
1p PocketQube - demonstrator from Turkish company Hello Space for a planned constellation of 100 internet communications satellites. Released from ION SCV 11 Jun 21.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 13:23	6906	0.0017	516	540	95.20	97.51	155
ELO 4 (Eutelsat LEO for Objects) 2023-084BS 56990						Re-entered - 2025 Jan 25 Life 593 days
6U Cubesat from Eutelsat to act as a demonstrator for a broadband internet communications satellite. Released from ION SCV-011 early-July.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 13:12	6905	0.0016	516	538	95.18	97.51	141
SpeiSat 2023-084BT 56991						Re-entered - 2025 Apr 8 Life 666 days
3U Cubesat with contributions from several participants, co-ordinated by the Italian Space Agency. Includes sensors to measure the characteristics of space in LEO and an electronic copy of "Statio Orbis", a book written by the Pope. Released from ION SCV-11 late-June.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 06:39	6902	0.0014	514	533	95.11	97.51	124
URESat 1 2023-084BU 56992						Re-entered - 2025 Feb 21 Life 620 days
1.5p PocketQube carrying an internet store/forward comms system and an amateur radio payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 11, 06:13	6908	0.0020	516	543	95.23	97.51	134
MRC 100 (Műegyetemi Rádió Club 100) 2023-084BV 56993						Re-entered - 2025 Jan 7 Life 575 days
3p PocketQube - Hungarian owned satellite to measure Earth-based radio pollution in a range of radio bands. Named in honour or MRC's 100th anniversary.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 11, 03:03	6908	0.0020	516	543	95.23	97.51	135
unidentified satellite 2023-084BY 56996						in space
Released from ION SCV 11 around August 14. Mission details and name to follow.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 23, 13:35	7027	0.0070	599	698	97.70	98.04	179
Skykraft 3D 2023-084BZ 57956						in space
Small satellite from Australia as a demonstrator for a 200 satellite system to provide air traffic control services in areas away from convential ground station coverage. Released from Skykraft 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 26, 07:38	6901	0.0012	515	531	95.08	97.52	207
Orbiter SN3 2023-084xx 56960						in space
Satellite carrier from a company called Launcher with three small satellites and several hosted payloads. Released from launch vehicle at L+ 01:11:48. A software problem resulted in excessive spin and lower than expected power from the solar panels so a decision was made to release all the satellites immediately. Satelllites: Otter Pup - released Jun 12, sat 2 - released Jun 12, sat 3 - released Jun 12. Hosted payloads include: Nightingale 1 -demonstrator for a satellite comms system for Cesium Astro, Remora - demonstrator of a satellite guidance, navigation and control system from Millenium Space Systems, payload deployer - demostrator from TR11.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 20, 17:50	6904	0.0013	517	535	95.15	97.52	193
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jun 12 Life <1 day
Launched SpaceX Transporter 8 multi-satellite mission. Caused to re-enter above the Indian Ocean near South Africa at about 23:40 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable

2023-085 CZ 2D Taiyuan Space Centre						2023 Jun 15, 05:30
Jilin-1 (Horgos 1) 2023-085xx						in space
Chinese commercial remote sensing satellite. Precise variant to be advised.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6917	0.0011	531	547	95.42	97.46	253	12:39
Jilin-1 High Resolution 03D 19 (Jilin-1 GF3D 19) 2023-085xx						in space
High resolution, multi-spectral imaging satellite. One of eight similar satellites carried on this launch, all are in similar orbits
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6917	0.0011	531	547	95.42	97.46	253	12:39
Jilin-1 Platform 02A 01 2023-085xx						in space
Chinese commercial remote sensing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6917	0.0011	531	547	95.42	97.46	253	12:39
Jilin-1 Platform 02A 02 2023-085xx						in space
Chinese commercial remote sensing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6917	0.0011	531	547	95.42	97.46	253	12:39
Jilin-1 Platform 06A 01 2023-085xx						in space
Chinese commercial remote sensing satellite. One of thirty similar satellites carried on this launch, all are in similar orbits
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6917	0.0011	531	547	95.42	97.46	253	12:39
CZ 2D second stage uncatalogued						Re-entered - 2023 Jun 15 Life <1 day
Launched forty one Jilin-1 satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-086 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Jun 18, 21:22
SATRIA (Satellite of the Republic of Indonesia) 2023-086A 57045						in space
Indonesian domestic very high throughput comsat. Expected location 146° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Jun 19, 16:53	32486	0.7869	545	51670	971.18	27.89	180
2023 Jun 21, 23:41	32711	0.7846	668	51997	981.29	27.88	181
2023 Jun 29, 13:35	33481	0.7765	1105	53100	1016.13	25.88	184
2023 Jul 3, 19:58	33853	0.7820	1001	53948	1033.13	24.95	185
2023 Jul 14, 10:43	36486	0.7470	2853	57362	1155.96	20.27	188
2023 Jul 20, 04:18	37970	0.7320	3798	59385	1227.19	18.08	190
2023 Jul 28, 02:08	40020	0.7121	5144	62139	1327.93	15.44	192
2023 Aug 7, 17:27	41602	0.6815	6872	63576	1407.44	12.25	195
2023 Aug 15, 21:45	41775	0.6485	8305	62488	1416.22	10.04	196
2023 Aug 22, 08:45	42410	0.6080	10246	61817	1448.63	8.60	197
2023 Aug 29, 15:27	44153	0.5199	14818	60732	1538.88	7.10	199
2023 Sep 6, 04:18	44390	0.4807	16671	59352	1551.27	5.86	200
Falcon 9 second stage 2023-086B 57046						in space
Launched SATRIA.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 20, 14:09	32748	0.7882	559	52180	982.94	28.19	191

2023-087 CZ 6 (Y-12) Taiyuan Space Centre						2023 Jun 20, 03:18
Shiyan 25 (Test 25) 2023-087A 57047						in space
Earth observation satellite with test or demonstration sensor payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jun 20, 10:58	6692	0.0010	307	321	90.80	96.64	269	10:30
CZ 6 third stage uncatalogued						Re-entered - 2023 Jun 20 Life <1 day
Launched Shiyan 25. Probably caused to re-enter soon after releasing satellite.
Not Catalogued - orbit parameters unavailable

2023-088 Falcon 9 Block 5 (Starlink Group 05-07) Vandenberg Space Force Base						2023 Jun 22, 07:19
Starlink 5847 2023-088A 57048						Re-entered - 2025 Feb 26 Life 615 days
One member of a simultaneously-launched cluster of forty seven Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 07:37 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 2, 04:00	6699	0.0002	319	322	90.94	43.00	253
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jun 22 Life <1 day
Launched forty seven Starlink satellites. Caused to re-enter the Earth's atmosphere after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-089 Delta 4 Heavy (NROL-68) Cape Canaveral Space Force Station						2023 Jun 22, 09:18
USA 345 (Mentor 9, Advanced Orion 9) 2023-089A 57099						in space
US government signals intelligence gathering (SIGINT) satellite. Separated from the launch vehicle in geosynchronous drift orbit.
Geosynchronous Drift Orbit - parameters awaited
Delta 4 upper stage 2023-089B 57100						in space
Launched USA 345
Geosynchronous Drift Orbit - parameters awaited

2023-090 Falcon 9 Block 5 (Starlink Group 05-12) Cape Canaveral Space Force Station						2023 Jun 23, 15:35
Starlink 6132 2023-090A 57101						in space
One member of a simultaneously-launched cluster of fifty six Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:40 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 2, 04:00	6703	0.0007	320	330	91.03	43.00	33
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jun 22 Life <1 day
Launched fifty six Starlink satellites. Caused to re-enter the Earth's atmosphere after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-091 Soyuz-2.1b + Fregat Vostochny Cosmodrome						2023 Jun 27, 11:34
Meteor M2-3 2023-091A 57166						in space
Meteorological satellite providing global observations of the Earth's surface and its atmosphere. The data acquired by the satellite is used for weather analysis and forecasting, climate change monitoring, sea water monitoring and forecasting, and space weather analysis and prediction.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jun 27, 15:25	7191	0.0005	809	816	101.14	98.76	84	09:00
StratoSatTK 1 (RS-52S) 2023-091B 57167						in space
3U Cubesat with an unspecified experiments package. 1U of the structure carries five picosats (2x 2TU, 4x 1TU) that were released around Jun 11. Also carries an amateur radio package.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:55	6935	0.0018	545	569	95.79	97.66	213
UmKA 1 (RS-40S) 2023-091G 57172						in space
3U Cubesat from the Center for Scientific Creativity of the 29th school of Podolsk, Russia. Equipped with an astronomical imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:54	6935	0.0017	545	568	95.79	97.66	213
CuBel 2 (BSUSat 2) 2023-091K 57175						in space
3U Cubesat? from Belarusian State University - purpose unknown.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 16:00	6937	0.0016	548	569	95.83	97.66	224
Zorki-2M 01 2023-091M 57177						in space
12U Cubesat from Russia's Sitronix Group, equipped with a remote sensing payload. Also equipped with an AIS system to carry short messages and position information to/from ships at sea.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:56	6935	0.0018	544	570	95.80	97.67	208
CubeSX-HSE 3 (RS-42S) 2023-091N 57178						in space
3U Cubesat equipped with an AIS system to relay messages to/from aircraft in flight. Also carries an amateur radio payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:56	6935	0.0019	544	570	95.80	97.67	207
Monitor 3 (RS-58S) 2023-091Q 57180						in space
3U Cubesat equipped with sensors to monitor deep sky x-ray flares and gamma radiation. Also carries an amateur radio payload. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:56	6935	0.0019	544	570	95.80	97.67	207
Monitor 4 (RS-57S) 2023-091S 57182						in space
3U Cubesat equipped with sensors to monitor deep sky x-ray flares and gamma radiation. Also carries an amateur radio payload. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:57	6935	0.0019	544	570	95.80	97.67	208
Monitor 2 (RS 39S) 2023-091U 57184						in space
3U Cubesat equipped with sensors to monitor deep sky x-ray flares and gamma radiation. Also carries an amateur radio payload. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:48	6933	0.0015	544	565	95.74	97.67	202
CSTP 1.2 2023-091W 57186						in space
3U Cubesat from Russian STC Company. Test vehicle for satellite systems and carrying what appears to be an ELINT payload. Equipped with a thruster system. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:46	6932	0.0014	544	563	95.72	97.67	199
Svyatobor 1 2023-091X 57187						in space
3U Cubesat equipped with a plasma thruster and a thermal imaging system with undisclosed purpose. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:47	6932	0.0015	544	564	95.73	97.67	200
Khors 1 2023-091Y 57188						in space
6U Cubesat studying galactic radiation. Also equipped with a test version of a plasma thruster. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:47	6932	0.0014	544	564	95.73	97.66	202
Vizard Meteo 2 2023-091Z 57189						in space
3U Cubesat for meteorology studies from Russian company NIS. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:45	6931	0.0014	543	563	95.71	97.67	198
Nanoprobe 1 (RS-49S) 2023-091AA 57190						in space
3U Cubesat from the Oryol State University, Russia to study 'space weathering' of an object in orbit. Also carries an amateur radio package.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:43	6931	0.0012	544	561	95.70	97.66	204
Politech Universe 3 (RS-46S) 2023-091AB 57191						in space
3U Cubesat from Peter the Great Polytechnic University, St Petersburg . Carries a payload to monitor radiation in LEO. Also carries an amateur radio payload. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:56	6935	0.0018	545	569	95.80	97.66	213
Avion (Kaluga 650) 2023-091AF 57195						in space
6U Cubesat supporting an experimental air traffic control/monitoring system and space environment sensors. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:46	6932	0.0014	544	563	95.72	97.67	203
Khors 2 2023-091AG 57196						in space
6U Cubesat studying galactic radiation. Also equipped with a test version of a plasma thruster. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:46	6932	0.0014	544	563	95.72	97.67	202
A-SEANSAT-PG 1 (Penang 1) 2023-091AH 57197						in space
6U Cubesat from Malysian company ANGKASA-X equipped with a message relay system. Also fitted with an optical Earth observation system. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 6, 15:46	6932	0.0014	544	563	95.72	97.66	204	08:55
Yarilo 3 2023-091AJ 57198						Re-entered - 2025 Apr 28 Life 671 days
3U Cubesat - one of a simultaneously-launched pair built by the Bauman Moscow State Technical University (BMSTU) to study the Earth's albedo and make measurements of the space environment. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:46	6931	0.0014	544	563	95.72	97.67	203
CSTP 1.1 2023-091AN 57202						in space
3U Cubesat from Russian STC Company. Test vehicle for satellite systems and carrying what appears to be an ELINT payload. Equipped with a thruster system. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:45	6931	0.0014	544	563	95.72	97.67	198
UTMN 2 2023-091AP 57203						in space
Small satellite from Tyumen State University, Russia studying the space environment.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:45	6931	0.0014	544	563	95.72	97.67	198
SITRO-AIS 12 2023-091AQ 57204						in space
3U Cubesat from Russian Sitronix Group. Equipped with an AIS system to carry short messages and position information to/from ships at sea. Carries a plaque to commemorate an early cosmonaut who never made a flight. One of eight similar satellites carried on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:44	6931	0.0014	543	562	95.71	97.67	198
ArcCube 01 2023-091AR 57205						in space
3U Cubesat equipped with an amateur radio package. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:44	6931	0.0013	544	561	95.71	97.66	206
KuzGTU 1 (RS-47S) 2023-091AV 57217						in space
Small satellite from Kuzbass University to study thermal effect and vibration in a satellite structure. ID information comes via radio tracking efforts of Nico Janssen.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 6, 15:56	6935	0.0018	544	570	95.79	97.67	209
StratoSatTK 1А 2023-091AW 57322						in space
"Tinysat" equipped with a camera system. Released from StratoSatTK 1 around Jun 11. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 14, 02:51	6935	0.0019	544	570	95.79	97.66	189
StratoSatTK 1Б 2023-091AX 57323						in space
"Tinysat" equipped with a camera system. Released from StratoSatTK 1 around Jun 11. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 14, 09:14	6935	0.0019	544	570	95.79	97.66	188
StratoSatTK 1В 2023-091AY 57324						in space
"Tinysat" equipped with a camera system. Released from StratoSatTK 1 around Jun 11. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 14, 09:14	6935	0.0019	544	570	95.79	97.66	187
StratoSatTK 1Г 2023-091AZ 57325						Re-entered - 2024 Dec 17 Life 539 days
"Tinysat" equipped with a camera system. Released from StratoSatTK 1 around Jun 11. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 14, 04:27	6935	0.0019	544	570	95.79	97.66	188
StratoSatTK 1д 2023-091BA 57326						in space
"Tinysat" equipped with a camera system. Released from StratoSatTK 1 around Jun 11. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 14, 09:14	6935	0.0019	544	570	95.79	97.66	188
StratoSatTK 1Е 2023-091BB 57327						in space
"Tinysat" equipped with a camera system. Released from StratoSatTK 1 around Jun 11. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 14, 12:26	6935	0.0019	544	570	95.79	97.66	187
Akhmat 1 2023-091xx						in space
3U Cubesat from the Russian Republic of Chechnya carrying an ADS-B receiver to relay short messages from aircraft in flight.
Orbit parameters awaited
Impulse 1 2023-091xx						in space
6U Cubesat to monitor solar activity. Also carries technical experiments connected with laser communication and quantum communication.
Orbit parameters awaited
Norbi 2 2023-091xx						in space
6U Cubesat from Novosibirsk State University studying the solar corona. Also testing satellite systems.
Orbit parameters awaited
PHI Demo (Payload Hosting Initiative) 2023-091xx						in space
12U Cubesat from the Mohammed Bin Rashid Space Centre, UAE as a demonstrator for its hosted payload carrier. Actual payload includes an internet communications system and a water-based thruster.
Orbit parameters awaited
Rassvet-1 1 2023-091xx						in space
Small satellite acting as demonstrator for a future constellation of internet broadband communications satellites. One of three carried on the same launch.
Orbit parameters awaited
Rassvet-1 2 2023-091xx						in space
Small satellite acting as demonstrator for a future constellation of internet broadband communications satellites. One of three carried on the same launch.
Orbit parameters awaited
Rassvet-1 3 2023-091xx						in space
Small satellite acting as demonstrator for a future constellation of internet broadband communications satellites. One of three carried on the same launch.
Orbit parameters awaited
ReshUCube 2 (RS-37S) 2023-091xx						in space
3U Cubesat from the Siberian State University carrying several undisclosed payloads. Also carries an amateur radio payload.
Orbit parameters awaited
SamSat-ION 2023-091xx						in space
Small satellite from Samara University studying radiation and magnetic components of the Earth's ionosphere.
Orbit parameters awaited
Saturn 2023-091xx						in space
6U CubeSat from Kuban State Technological University, Russia to monitor space weather in LEO.
Orbit parameters awaited
Sirius-SINP 2023-091xx						in space
3U Cubesat from Russian company BG Optics equipped with a particle detector to study electrons, protons and gamma radiation in LEO
Orbit parameters awaited
Yarilo 4 2023-091xx						in space
3U Cubesat - one of a simultaneously-launched pair built by the Bauman Moscow State Technical University (BMSTU) to study the Earth's albedo and make measurements of the space environment.
Orbit parameters awaited
Fregat rocket stage uncatalogued						Re-entered - 2023 Jun 27 Life <1 day
Launched Meteor M2-3 then descended to near-500 km orbit to release remaining satellites. Caused to re-enter above the eastern Pacific Ocean at about 17:00 UTC.
Not Catalogued - orbit parameters unavailable

2023-092 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Jul 1, 15:12
Euclid 2023-092A 57209						in space
ESA spacecraft equipped with a telescope to image galaxies and other distant objects in order to explore the composition and evolution of dark matter and dark energy in the Universe. Released from launch vehicle at 15:53 UTC. Arrived at Lagrange point 2 in the Sun-Earth system Jul 27.
Stationed near the L2 Lagrange Point in the Earth-Sun system
Falcon 9 second stage 2023-092B 57210						in space
Launched EUCLID.
Heliocentric orbit

2023-093 Ariane 5ECA (VA-261) Centre Spatiale Guyanaise						2023 Jul 5, 22:00
Heinrich Herz 2023-093A 57213						in space
German government secure military communications satellite. Separated from launch vehicle at 22:29 UTC. Expected location 17°.6 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Jul 6, 19:12	24373	0.7273	268	35723	631.15	2.97	178
2023 Jul 7, 18:01	26663	0.5783	4866	35704	722.14	1.93	178
2023 Jul 12, 00:00	38484	0.0932	28519	35693	1252.22	0.27	172
2023 Jul 13, 05:38	40137	0.0484	31816	35701	1333.75	0.14	177
2023 Jul 31, 22:00	42167	0.0001	35786	35792	1436.21	0.12	136	0°.2 E
2023 Aug 3, 22:52	42165	0.0001	35781	35792	1436.09	0.04	288	0°.5 E
2024 Mar 9, 07:09	42166	0.0001	35782	35793	1436.14	0.03	337	0°.5 E
Syracuse 4B (SYstème de RAdioCommunication Utilisant un SatellitE) 2023-093B 57214						in space
French government military secure-communications satellites for use by land-based, maritime and airborne forces. Separated from launch vehicle at 22:33 UTC. Orbit raising uses electric propulsion and it will take the satellite to its operational orbit by mid-2024. Possibly aimed at location 5° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Jul 6, 18:52	24351	0.7272	266	35681	630.30	2.97	178
2023 Jul 8, 08:15	24401	0.7250	331	35715	632.22	2.94	180
2023 Jul 13, 03:58	24611	0.7190	537	35929	640.39	2.98	183
2023 Jul 20, 21:35	25468	0.7080	1057	37122	674.13	2.90	187
2023 Jul 25, 15:40	25929	0.7015	1361	37740	692.53	2.91	188
2023 Aug 6, 05:36	27447	0.6745	2555	39583	754.22	2.80	192
2023 Aug 14, 11:33	28465	0.6578	3363	40811	796.59	2.75	193
2023 Aug 21, 02:30	29227	0.6440	4028	41670	828.77	2.68	195
2023 Aug 28, 04:17	30253	0.6260	4937	42812	872.79	2.49	197
2023 Sep 6, 13:37	31657	0.6040	6160	44398	934.25	2.29	200
2023 Sep 12, 12:59	32638	0.5891	7033	45487	978.02	2.17	202
2023 Sep 19, 12:04	33726	0.5719	8059	46637	1027.32	2.00	203
2023 Sep 25, 08:00	34703	0.5555	9047	47603	1072.29	1.88	204
2023 Oct 4, 12:11	35991	0.5249	10723	48504	1132.55	1.67	206
2023 Oct 10, 10:46	36136	0.5090	11364	48153	1139.40	1.56	208
2023 Oct 16, 20:40	35927	0.5005	11567	47532	1129.53	1.44	210
2023 Nov 2, 16:54	38353	0.3997	16644	47306	1245.83	1.15	212
2023 Nov 9, 15:37	38832	0.3625	18376	46531	1269.23	1.03	213
2023 Nov 17, 00:29	39375	0.3220	20320	45674	1295.96	0.90	213
2023 Nov 30, 11:50	40165	0.2441	23982	43593	1335.17	0.67	213
2023 Dec 7, 13:39	40991	0.2060	26170	43055	1376.53	0.55	212
2023 Dec 17, 18:25	41217	0.1366	29210	40468	1387.97	0.38	205
2023 Dec 25, 11:44	41615	0.0869	31620	38855	1408.13	0.27	196
2024 Jan 8, 18:51	42196	0.0006	35794	35842	1437.69	0.09	90	6°.5 W
2024 Jan 9, 13:45	42165	0.0000	35787	35787	1436.12	0.09	39	6°.4 W
Ariane 5 third stage 2023-093C 57215						in space
Launched Heinrich Herz and Syracuse 4B. Final Ariane 5 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 8, 05:30	24341	0.7273	260	35665	629.88	2.97	180

2023-I06 Nanoracks Cubesat Deployer (NRCSD 26) International Space Station						2023 Jul 6, 09:55
Moonlighter 1998-067VU 57316						Re-entered - 2024 Feb 10 Life 219 days
3U Cubesat from the Aerospace Corporation, USA. To be used as a testing 'sandpit' to study hacking prevention systems for objects in orbit. Released at 10:05 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 10, 17:03	6794	0.0002	414	417	92.88	51.64	340
ESSENCE (Educational Space Science and Engineering CubeSat Experiment) 1998-067xx						in space
3U Cubesat from York University, Ontario as a testbed for a wide-angle camera to observe snow and ice coverage in Northern Canada, and a proton detector to study the effects of Solar Proton Events on satellites in LEO. Released at 11:35 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6793	0.0003	413	417	92.87	51.64	305
Iris (ManitobaSat 1) 1998-067xx						in space
3U Cubesat from the University of Manitoba to study space weathering on objects in orbit. Released at 11:35 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6793	0.0003	413	417	92.87	51.64	305
RADSAT-SK 1998-067xx						in space
2U Cubesat from University of Saskatchewan, Canada, testing a radiation dosimeter and a melanin-based method of radiation protection. Released at 11:25 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6793	0.0003	413	417	92.87	51.64	305
SC-ODIN (Space Concordia - Orbital Dust Imaging Nanosatellite) 1998-067xx						in space
3U Cubesat from Concordia University, Quebec. Equipped with an imaging system to study aerosol plumes. Also fitted with sensors to monitor the space environment. Released at 09:55 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6793	0.0003	413	417	92.87	51.64	305
Ukpik 1 (Snowy Owl) 1998-067xx						in space
2U Cubesat from Canada's Western University in partnership with Nunavut Arctic College. Equipped with an imaging system capable of providing virtual reality views. Also to be used as a teaching aid in conrolling satellites. Released at 11:25 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6793	0.0003	413	417	92.87	51.64	305

2023-094 Falcon 9 Block 5 (Starlink Group 05-13) Vandenberg Space Force Base						2023 Jul 7, 19:29
Starlink 5525 2023-094A 57218						in space
One member of a simultaneously-launched cluster of forty eight Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 19:48 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 14, 18:00	6676	0.0027	281	316	90.48	43.00	200
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jul 7 Life <1 day
Launched forty eight Starlink satellites. Caused to re-enter the Earth's atmosphere at about 21:10 UTC after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-095 CZ 2C + YZ-1S Jiuquan Space Centre						2023 Jul 9, 11:00
Hulianwang Jishu Shiyan 1 (Internet Connectivity Test Satellite 1) 2023-095A 57288						in space
Test satellite for Chinese government communications system for use by Internet-connected devices. One of two carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 9, 14:35	7484	0.0014	1095	1117	107.39	86.50	301
2023 Jul 14, 13:57	7488	0.0013	1099	1119	107.46	86.50	280
2023 Jul 15, 02:29	7487	0.0016	1097	1121	107.45	86.50	286
Hulianwang Jishu Shiyan 2 (Internet Connectivity Test Satellite 2) 2023-095B 57289						in space
Test satellite for Chinese government communications system for use by Internet-connected devices. One of two carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 9, 14:35	7482	0.0012	1095	1113	107.34	86.50	304
2023 Jul 13, 23:34	7485	0.0011	1099	1115	107.41	86.50	283
2023 Jul 15, 04:48	7488	0.0016	1098	1121	107.47	86.50	287
YZ-1S rocket stage 2023-095C 57318						Re-entered - 2023 Jul 22 Life 13 days
Launched pair of Internet Connectivity Test Satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 10, 22:51	6968	0.0679	117	1063	96.48	86.39	292

2023-096 Falcon 9 Block 5 (Starlink Group 06-05) Cape Canaveral Space Force Station						2023 Jul 10, 03:58
Starlink 30198 2023-096A 57290						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:01 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 18, 18:00	6738	0.0002	358	361	91.73	43.00	271
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jul 10 Life <1 day
Launched twenty two second generation Starlink satellites. Caused to re-enter at about 06:10 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-097 Zhuque-2 (Y2) Jiuquan Space Centre						2023 Jul 12, 01:00
Zhuque 2 second stage 2023-097A 57319						Re-entered - 2024 Nov 30 Life 507 days
Instrumented rocket stage as a test vehicle on second mission of the rocket. Carried a satellite mass simulator and a simulated release command was actuated at 01:12 UTC. Earlier launch of the rocket failed 2022 December 14 when the stage did not complete its firing and fourteen satellites were lost.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 12, 03:49	6824	0.0022	431	461	93.51	97.27	280	07:21

2023-098 LVM3 (M4) Satish Dhawan Space Centre						2023 Jul 14, 09:05
Chandrayaan 3 Lander (Vikram) 2023-098A 57320						Re-entered - 2023 Aug 23 Life 40 days
Indian Lunar Lander - carried surface rover Pragyaan and a communications system to relay signals from the rover to the orbiter. Separated from the Propulsion Module August 17. Landed on the Moon, near the south pole August 23.
Landed on the Moon
Chandrayaan 3 Propulsion Module (Chandrayaan Orbiter) 2023-098C 57770						in space
Carried Chandrayaan 3 lander as far as circumlunar orbit. Apogee of the transfer orbit periodically increased until injection into lunar transfer trajectory on July 31. Entered orbit around the Moon August 5. Released lunar lander August 17. Acted as radio relay for communication with the lander on the lunar surface. Departed lunar orbit 2023 Dec 24. Space-Track applied the catalogue number and designation of 57770/2023-098C on 2024 January 4. Some Space-Track orbit data sets (the pre-2024 orbits listed below) were ascribed to 57320/2023-098A.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 14, 14:54	24601	0.7351	138	36308	640.03	21.30	178
2023 Jul 17, 14:32	27292	0.7596	184	41644	747.85	21.32	180
2023 Jul 18, 15:35	32175	0.7964	174	51420	957.28	21.33	181
2023 Jul 20, 20:38	42176	0.8434	227	71368	1436.66	21.30	182
2023 Jul 27, 14:52	70035	0.9054	247	127067	3074.21	21.34	183
2024 Jan 10, 11:06	219898	0.4157	122105	304934	17103.72	27.52	87
2024 Feb 14, 18:03	264756	0.2146	201555	315201	22595.82	28.49	81
Chandrayaan 3 Rover (Pragyaan) uncatalogued						in space
Indian Lunar Rover, departed Chandrayaan lander Aug 25.
Landed on the Moon
LVM3 third stage 2023-098B 57321						Re-entered - 2023 Nov 15 Life 124 days
Launched Chandrayaan 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 14, 17:43	24362	0.7323	142	35825	630.70	21.30	178

2023-099 Falcon 9 Block 5 (Starlink Group 05-15) Cape Canaveral Space Force Station						2023 Jul 16, 03:50
Starlink 6290 2023-099A 57329						in space
One member of a simultaneously-launched cluster of fifty four Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:55 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 25, 14:00	6733	0.0002	353	356	91.63	43.01	259
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jul 16 Life <1 day
Launched fifty four Starlink satellites. Caused to re-enter above the Indian Ocean at about 06:00 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-100 Electron (Baby Come Back) Rocket Lab Launch Complex, New Zealand						2023 Jul 18, 01:27
Starling 4 2023-100A 57386						in space
6U Cubesat from NASA - one of four launched simultaneously on a test/demonstration mission of systems to allow satellites to fly in formation and act together without input from ground-based controllers. Released from launch vehicle at 01:16 UTC. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 18, 13:24	6953	0.0013	566	584	96.16	99.45	278
Starling 2 2023-100B 57387						in space
6U Cubesat from NASA - one of four launched simultaneously on a test/demonstration mission of systems to allow satellites to fly in formation and act together without input from ground-based controllers. Released from launch vehicle at 01:16 UTC. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 18, 12:07	6953	0.0014	566	585	96.17	99.45	286
Starling 1 2023-100C 57388						in space
6U Cubesat from NASA - one of four launched simultaneously on a test/demonstration mission of systems to allow satellites to fly in formation and act together without input from ground-based controllers. Released from launch vehicle at 01:17 UTC. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 18, 13:39	6954	0.0013	566	584	96.18	99.46	284
Starling 3 2023-100D 57389						in space
6U Cubesat from NASA - one of four launched simultaneously on a test/demonstration mission of systems to allow satellites to fly in formation and act together without input from ground-based controllers. Released from launch vehicle at 01:17 UTC. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 18, 10:32	6953	0.0013	566	585	96.17	99.45	285
Lemur-2 (Deverill M T) 2023-100E 57390						in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Released from launch vehicle at 01:18 UTC. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 18, 10:32	6952	0.0014	564	583	96.14	99.46	272
Lemur-2 (Mano) 2023-100F 57391						in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Released from launch vehicle at 01:17 UTC. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 18, 12:05	6950	0.0016	561	583	96.11	99.46	265
LEO 3 2023-100G 57392						in space
Small satellite owned by Telesat of Canada, acting as a demonstrator of a future constellation of 188 "Lightspeed" data networking satellites. Also provides continuity for customers using Telesat's recently decommissioned LEO Phase 1 satellite (43113,2018-004C). Released from launch vehicle at 03:13 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 18, 09:35	7385	0.0016	995	1019	105.27	99.44	239
Electron third stage (kick stage) 2023-100H 57393						in space
Launched seven assorted satellites. Perigee lowered after releasing LEO 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6953	0.0014	566	585	96.17	99.46	285
estimated orbit	7385	0.0016	995	1019	105.27	99.44	238
2023 Jul 18, 13:49	7116	0.0387	462	1014	99.57	99.34	197
Electron second stage 2023-100J 57394						Re-entered - 2023 Aug 4 Life 17 days
Launched seven assorted satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 18, 13:30	6767	0.0280	199	578	92.32	99.44	210

2023-I07 JEM Small Satellite Orbital Deployer International Space Station						2023 Jul 19, 07:00
Maya 5 1998-067VW 57419						Re-entered - 2023 Dec 8 Life 142 days
1U Cubesat - built under the Philippines Space Space Science and Technology Proliferation programme by the University of the Philippines Diliman (including student participation) and the DOST Advanced Science and Technology Institute. Demonstrator of systems needed for satellite-based remote data collection and optical imaging, including a near infrared camera.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 20, 18:30	6793	0.0003	413	417	92.87	51.64	178
Maya 6 1998-067VX 57420						Re-entered - 2023 Dec 12 Life 146 days
1U Cubesat - built under the Philippines Space Space Science and Technology Proliferation programme by the University of the Philippines Diliman (including student participation) and the DOST Advanced Science and Technology Institute. Demonstrator of systems needed for satellite-based remote data collection and optical imaging, including a near infrared camera.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 20, 18:30	6793	0.0003	413	417	92.87	51.64	178

2023-101 Kuaizhou 1A Jiuquan Space Centre						2023 Jul 20, 03:20
Tianmu 1-07 2023-101A 57399						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 20, 14:29	6901	0.0009	516	529	95.09	97.41	274	09:39
Tianmu 1-08 2023-101B 57400						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 20, 14:29	6902	0.0009	518	530	95.11	97.41	264	09:39
Tianmu 1-09 2023-101C 57401						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 20, 14:21	6902	0.0009	518	531	95.11	97.41	263	09:39
Tianmu 1-10 2023-101D 57402						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements. Catalogue Number and Designation letter to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 20, 14:22	6903	0.0011	517	532	95.12	97.41	249	09:39
Kuaizhou 1A third stage 2023-101E 57403						Re-entered - 2023 Jul 25 Life 5 days
Launched Tianmu 1-07 - Tianmu 1-10. Perigee lowered after releasing satellites. Launch postponed from Jul 3 and Jul 19.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 20, 14:02	6716	0.0283	148	528	91.30	97.44	39

2023-102 Falcon 9 Block 5 (Starlink Group 06-15) Vandenberg Space Force Base						2023 Jul 20, 04:09
Starlink 30240 2023-102A 57404						in space
One member of a simultaneously-launched cluster of fifteen V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:24 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 27, 16:00	6709	0.0003	328	332	91.14	43.00	162
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jul 20 Life <1 day
Launched fifteen Starlink satellites. Caused to re-enter above the central Pacific Ocean at about 05:40 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-103 Ceres 1 (Gushenxing 1 Y-6, Lemon Tree) Jiuquan Space Centre						2023 Jul 22, 05:07
Xingshidai 16 (Daiyun, Star Times 16) 2023-103A 57421						Re-entered - 2024 Aug 2 Life 377 days
Remote sensing - equipped with a multispectral Earth imaging system, from ADA Space (Chengdu Guoxing Aerospace Technology company) of China. Also carries a laser communication system and uses an artificial intelligence system to control the creation and processing of images. Part of a planned 100 satellite constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 24, 13:31	6872	0.0012	486	501	94.48	96.63	282	11:26
Qiankun 1 ((ultra LEO satellite)) 2023-103B 57422						in space
Technology verification payload described as the first ultra-low (ULEO) orbit satellite - designed to operate below 300 km. Equipped with multiple imaging devices, an image intelligent processor and other 'test payloads' including a low-thrust engine. Maintained station with Xingshidai 16 until September 28 then orbit lowered in small steps towards ULEO.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 24, 13:33	6872	0.0013	485	502	94.48	96.62	281	11:26
2023 Aug 19, 02:02	6867	0.0014	479	499	94.39	96.63	193	11:15
2023 Aug 22, 18:11	6867	0.0015	479	499	94.38	96.62	180	11:14
2023 Sep 24, 09:20	6830	0.0032	430	474	93.62	96.62	313	11:02
2023 Sep 29, 01:45	6830	0.0032	430	473	93.62	96.62	295	11:00
2023 Oct 14, 10:10	6828	0.0032	429	472	93.59	96.62	236	10:55
2023 Nov 16, 18:36	6803	0.0006	421	429	93.08	96.62	82	10:45
2023 Nov 21, 13:29	6803	0.0006	421	429	93.07	96.62	69	10:43
2024 Jan 1, 03:36	6750	0.0007	367	376	91.98	96.61	271	10:34
2024 Mar 25, 13:01	6712	0.0006	330	337	91.20	96.59	28	10:21
2024 Apr 29, 18:42	6713	0.0014	325	344	91.23	96.59	107	10:17
2024 Oct 1, 20:29	6709	0.0010	324	337	91.15	96.57	217	09:57
2024 Oct 20, 13:47	6696	0.0010	311	324	90.88	96.56	152	09:55
2024 Dec 2, 14:04	6696	0.0009	312	324	90.88	96.55	111	09:50
2024 Dec 21, 12:09	6684	0.0007	300	310	90.63	96.54	46	09:48
Ceres 1 fourth stage 2023-103C 57423						Re-entered - 2024 Nov 7 Life 474 days
Launched Qiankun 1 and Xingshidai 16. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 22, 22:18	6831	0.0062	411	495	93.65	96.63	29

2023-104 CZ 2D Taiyuan Space Centre						2023 Jul 23, 02:50
Sixiang 01 (Skylight AS 01) 2023-104A 57424						in space
Chinese commercial remote sensing satellite equipped with an infrared imaging system. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 24, 08:32	6873	0.0013	486	503	94.50	97.40	273	10:00
Lingxi 3 2023-104B 57425						in space
Demonstrator of a broadband communications system. The payload can be reconfigured to meet current comms demands through onboard software and without ground intervention. Satellite design resembles a single flat panel in order to provide a large collector area on a small satellite. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 24, 08:33	6872	0.0014	484	503	94.48	97.40	279	10:00
Sixiang 02 (Skylight AS 02) 2023-104C 57426						in space
Chinese commercial remote sensing satellite equipped with a wide field of view optical imaging system. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 24, 08:33	6872	0.0013	485	503	94.49	97.40	277	10:00
Sixiang 03 (Skylight AS 03) 2023-104F 57429						in space
Chinese commercial remote sensing satellite equipped with a thermal imaging system to monitor heat sources on the Earth's surface. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Jul 24, 08:35	6874	0.0012	488	505	94.54	97.40	262	10:00
CZ 2D second stage 2023-104D 57427						Re-entered - 2024 Oct 2 Life 437 days
Launched 3x Sixiang satellites and Lingxi 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 24, 08:34	6872	0.0013	485	503	94.50	97.40	274

2023-105 Falcon 9 Block 5 (Starlink Group 06-06) Cape Canaveral Space Force Station						2023 Jul 24, 00:50
Starlink 30189 2023-105A 57430						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 01:55 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 31, 18:00	6703	0.0006	321	329	91.02	43.00	216
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jul 24 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter above the central Pacific Ocean at about 03:10 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-106 CZ 2D Xichang Space Centre						2023 Jul 26, 20:02
Yaogan 36-05 Follower 1 2023-106A 57452						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-04 (launch 2022-100) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 27, 02:12	6875	0.0007	492	502	94.55	35.00	259
2023 Aug 16, 19:02	6877	0.0005	495	502	94.59	35.00	90
Yaogan 36-05 Follower 2 2023-106C 57454						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-04 (launch 2022-100) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 27, 05:28	6873	0.0009	489	501	94.52	34.99	274
2023 Aug 17, 01:17	6878	0.0004	497	502	94.60	35.00	53
Yaogan 36-05 Leader 2023-106E 57456						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-04 (launch 2022-100) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 27, 05:28	6872	0.0009	488	500	94.50	34.99	286
2023 Aug 4, 07:58	6873	0.0009	488	501	94.51	34.99	8
2023 Aug 17, 01:12	6878	0.0002	498	501	94.61	35.00	201
CZ 2D second stage 2023-106B 57453						Re-entered - 2024 May 12 Life 291 days
Launched Yaogan 36 Group 5. Space-Track has this erroneously Catalogued as 57455, 2023-106D.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 27, 05:27	6874	0.0009	490	502	94.53	35.00	272

2023-107 Falcon 9 Block 5 (Starlink Group 06-07) Cape Canaveral Space Force Station						2023 Jul 28, 04:01
Starlink 30165 2023-107A 57457						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:16 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 3, 18:00	6722	0.0001	343	344	91.40	43.01	225
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jul 28 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter above the IndianOcean at about 06:30 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-108 Falcon 9 Heavy Kennedy Space Center						2023 Jul 29, 03:04
Echostar 24 (Jupiter 3) 2023-108A 57479						in space
High capacity, high speed comsat covering the North and South America. Separated from launch vehicle at 06:32 UTC. Expected location - 95° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Jul 29, 07:16	28131	0.4888	8001	35505	782.59	10.39	180
2023 Aug 1, 11:26	30848	0.3573	13449	35491	898.68	6.26	180
2023 Aug 5, 17:18	38482	0.0877	28729	35477	1252.10	1.13	181
2023 Aug 10, 23:04	37413	0.0660	28566	33503	1200.30	1.09	171
2023 Aug 21, 12:46	39353	0.0656	30392	35558	1294.87	0.78	184
2023 Aug 28, 07:11	39947	0.0504	31556	35581	1324.30	0.55	187
2023 Sep 6, 15:24	40826	0.0300	33225	35671	1368.26	0.27	193
2023 Sep 13, 08:54	41493	0.0147	34507	35723	1401.93	0.14	182
2023 Sep 18, 06:42	41988	0.0038	35451	35770	1427.10	0.05	145
2023 Sep 20, 06:25	42164	0.0001	35781	35792	1436.07	0.05	167	95°.2 W
Falcon 9 Heavy third stage 2023-108B 57480						in space
Launched Echostar 24.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 29, 09:32	28100	0.4900	7952	35492	781.31	10.42	180

2023-109 PSLV-CA (PSLV C-56) Satish Dhawan Space Centre						2023 Jul 30, 01:00
DS-SAR 2023-109A 57481						Re-entered - 2025 Jan 30 Life 550 days
Indian radar imaging satellite. The radar was supplied by Israeli Aircraft Industries.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 30, 18:32	6911	0.0008	527	538	95.29	5.00	12
Velox AM (Additive Manufacturing) 2023-109B 57482						in space
Small satellite from Nanyang Technological University, Singapore. It will demonstrate an on-orbit manufacturing system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 30, 16:44	6908	0.0011	522	538	95.24	5.01	16
ORB-12 (Strider) 2023-109C 57483						in space
12U Cubesat from Indonesia carrying several test/demonstration payloads including a radar Earth imager and two thruster systems. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
Scoob 2 2023-109D 57484						in space
3U Cubesat - student built satellite from the Research Centre at Singapore's NTU School of Electrical and Electronic Engineering. Carries an unspecified technology demonstration payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 30, 16:49	6912	0.0007	529	539	95.32	5.01	357
ARCADE (Atmospheric Coupling and Dynamics Explorer, INSPIRESat-4) 2023-109E 57485						in space
Small satellite from Nanyang Technological University, Singapore for ionospheric studies. Also carries an electric propulsion system to lower the orbit to 350 km, and an Earth imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 30, 18:27	6909	0.0010	524	538	95.26	5.00	15
Galassia 2 2023-109F 57486						in space
3U Cubesat from the National University of Singapore equipped with a multi-spectral Earth imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 30, 16:51	6913	0.0007	530	539	95.33	5.01	357
NuLIoN 2023-109G 57487						Re-entered - 2024 Oct 13 Life 441 days
3U Cubesat - Broadband internet comsat from Indonesia to pass messages from ground based sensors and recording stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jul 30, 20:09	6913	0.0004	532	538	95.34	5.01	3
PSLV upper stage uncatalogued						in space
Launched DS-SAR and six small satellites. ISRO announced the orbit would be be lowered to 295 x 300 km after releasing the satellites but no data have been released by Space-Track so its fate is uncertain.
Orbit parameters awaited

2023-110 Antares 230+ Mid Atlantic Regional Space Port, Wallops Island						2023 Aug 2, 00:31
Cygnus NG-19 (SS Laurel Clark) 2023-110A 57488						Re-entered - 2024 Jan 9 Life 160 days
Northrop Grumman vehicle carrying supplies and equipment to ISS under CRS-2 contract with NASA. Initial orbit similar to launch vehicle second stage. Captured by ISS remote manipular August 4 at 09:52 UTC. Docked with the downward-facing port of the Unity module at 12:28 UTC. Undocked 2023 Dec 22 at about 10:00 UTC and released from the RMS at 13:06 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 2, 02:10	6667	0.0120	209	369	90.30	51.62	139
2023 Aug 2, 03:32	6676	0.0133	209	387	90.48	51.64	141
2023 Aug 3, 15:36	6699	0.0125	237	404	90.93	51.63	164
2023 Aug 6, 11:32	6794	0.0002	415	417	92.89	51.65	276
2023 Dec 21, 13:21	6793	0.0002	413	416	92.87	51.64	42
2023 Dec 22, 20:55	6795	0.0003	415	419	92.91	51.64	110
2023 Dec 23, 18:24	6778	0.0002	399	401	92.55	51.65	49
Antares second stage 2023-110B 57489						Re-entered - 2020 Feb 23 Life <1 day
Launched SS Laurel Clark.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 2, 03:32	6613	0.0082	181	289	89.19	51.62	141

2023-111 CZ 4C Jiuquan Space Centre						2023 Aug 3, 03:47
Fengyun 3F (Fengyun 3-06) 2023-111A 57490						in space
Second generation meteorological imaging satellite capable of producing three-dimensional analyses of weather systems. Released from launch vehicle at 04:10 UTC. Launched to replace Fengyun 3C (39260/2013-052A).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Aug 3, 08:36	7184	0.0006	802	810	100.99	98.81	244	10:00
2023 Aug 5, 08:03	7190	0.0006	808	816	101.13	98.82	321	10:00
2023 Aug 5, 14:54	7195	0.0004	814	819	101.22	98.81	243	10:00
2023 Aug 6, 16:04	7200	0.0017	810	834	101.34	98.81	355	10:00
2023 Aug 6, 19:26	7203	0.0001	824	825	101.39	98.80	229	10:00
2023 Aug 8, 05:10	7204	0.0001	826	827	101.43	98.81	122	10:00
CZ 4C third stage 2023-111B 57491						in space
Launched Fenyun 3F. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 3, 09:57	7088	0.0141	610	809	98.97	98.81	46

2023-112 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Aug 3, 05:00
Galaxy 37 (Horizons 4) 2023-112A 57493						in space
Intelsat-owned comsat covering North America and the eastern Pacific Ocean. Separated from launch vehicle at 05:33 UTC. Expected location 127° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Aug 3, 09:26	34450	0.8104	155	55989	1060.58	24.61	180
2023 Aug 5, 20:15	35549	0.7544	2351	55990	1111.72	17.65	182
2023 Aug 8, 15:45	39085	0.5985	9315	56098	1281.64	9.01	181
2023 Aug 10, 14:38	47759	0.3082	26660	56103	1731.21	2.13	176
2023 Aug 14, 12:50	52310	0.1927	35850	56014	1984.45	1.13	179
2023 Aug 16, 14:36	43122	0.0206	35855	37632	1485.27	0.11	62
2023 Aug 17, 11:22	42198	0.0010	35779	35861	1437.80	0.10	292	146°.8 W
2023 Aug 21, 16:42	42165	0.0002	35776	35797	1436.10	0.07	313	147°.9 W
2023 Sep 19, 13:56	42006	0.0003	35614	35642	1428.02	0.02	98	140°.3 W
2023 Sep 25, 11:14	42070	0.0017	35621	35763	1431.26	0.03	215	128°.5 W
2023 Sep 26, 15:37	42143	0.0003	35754	35776	1434.98	0.04	113	128°.0 W
2023 Oct 3, 01:13	42164	0.0003	35774	35798	1436.06	0.05	106	127°.0 W
Falcon 9 second stage 2023-112B 57494						Re-entered - 2023 Sep 22 Life 50 days
Launched Galaxy 37.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 22, 14:48	34341	0.8105	128	55798	1055.56	24.48	187

2023-113 Falcon 9 Block 5 (Starlink Group 06-08) Cape Canaveral Space Force Station						2023 Aug 7, 02:41
Starlink 30154 2023-113A 57495						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:46 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 15, 18:00	6699	0.0002	320	322	90.95	43.00	262
Falcon 9 second stage uncatalogued						Re-entered - 2023 Aug 7 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter above the Indian Ocean at about 06:00 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-114 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2023 Aug 7, 13:19
Cosmos 2569 (Uragan-K2 №13L) 2023-114A 57517						in space
New generation GLONASS navigation satellite to fill a space in the constellation. Separated from the launch vehicle Fregat stage at about 16:50 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 8, 07:23	25524	0.0004	19135	19156	676.35	64.79	313
2023 Aug 14, 16:34	25541	0.0004	19152	19174	677.05	64.79	72
2023 Sep 8, 10:06	25508	0.0010	19105	19154	675.72	64.80	302
Fregat rocket stage 2023-114B 57518						in space
Launched Cosmos 2569.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 9, 01:05	25440	0.0028	18991	19133	673.05	64.80	196

2023-115 Falcon 9 Block 5 (Starlink Group 06-20) Vandenberg Space Force Base						2023 Aug 8, 03:57
Starlink 30259 2023-115A 57521						in space
One member of a simultaneously-launched cluster of fifteen V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:11 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 15, 18:00	6693	0.0002	313	315	90.81	43.00	253
Falcon 9 second stage uncatalogued						Re-entered - 2023 Aug 8 Life <1 day
Launched fifteen Starlink satellites. Caused to re-enter above the central Pacific Ocean at about 05:30 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-116 CZ 4C Taiyuan Space Centre						2023 Aug 8, 22:53
Huanjing 2F (S-SAR 02) 2023-116A 57519						in space
Chinese Earth surface imaging satellite equipped with a synthetic aperture radar operating at S-band frequencies.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Aug 9, 01:45	6873	0.0011	488	503	94.52	97.39	259	06:00
2023 Oct 17, 20:08	6870	0.0010	485	499	94.46	97.40	47	06:00
2023 Oct 19, 12:13	6871	0.0009	486	499	94.47	97.39	41	06:00
2023 Dec 12, 19:15	6866	0.0007	483	493	94.36	97.39	179	06:01
2023 Dec 13, 03:18	6871	0.0001	492	493	94.46	97.39	138	06:01
2023 Dec 15, 22:58	6883	0.0001	504	505	94.71	97.39	116	06:00
CZ 2C second stage 2023-116C 57536						Re-entered - 2024 Dec 25 Life 505 days
Launched Huanjing 2F.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 9, 01:38	6836	0.0045	428	489	93.76	97.12	44

2023-117 Ceres 1 (Gushenxing 1 Y-7) Jiuquan Space Centre						2023 Aug 10, 04:03
Henan Ligong 1 (Diwei Zhineng Yingji 1) 2023-117xx						in space
Multispectral Earth imaging satellite equipped with an intelligent onboard data processing system capable of targeting ‘hot spots’ on the ground in the event of a disaster. Developed by the Diwei 2 Space Technology Co of Hangzhou.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6911	0.0014	524	543	95.30	97.52	273	10:22
Xi'an Hangtou 104 2023-117xx						in space
Satellite in a planned constellation of 128 Earth imaging satellites. Payload includes a laser communication system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6911	0.0014	524	543	95.30	97.52	273	10:22
Xi'an Hangtou 112 2023-117xx						in space
Satellite in a planned constellation of 128 Earth imaging satellites. Payload includes a laser communication system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6911	0.0014	524	543	95.30	97.52	273	10:22
Xi'an Hangtou 6 2023-117xx						in space
Satellite in a planned constellation of 128 Earth imaging satellites. Payload includes a laser communication system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6911	0.0014	524	543	95.30	97.52	273	10:22
Xi'an Hangtou 88 2023-117xx						in space
Satellite in a planned constellation of 128 Earth imaging satellites. Payload includes a laser communication system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6911	0.0014	524	543	95.30	97.52	273	10:22
Xiguang-1 01 2023-117xx						in space
Multispectral Earth imaging satellite equipped with an onboard data processing system from private company XIOPM Space (Xi'an Institute of Optics and Precision Mechanics).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6911	0.0014	524	543	95.30	97.52	273	10:22
Xingchi 1-01B 2023-117xx						in space
Technology verification satellite for a constellation of remote sensing satellites equipped with a multispectral Earth imaging system. Also carries a laser communication system. Precursor to a 100 satellite constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6911	0.0014	524	543	95.30	97.52	273	10:22
Ceres 1 fourth stage uncatalogued						Re-entered - 2023 Aug 10 Life <1 day
Launched seven small satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-118 Soyuz-2.1b + Fregat Vostochny Cosmodrome						2023 Aug 10, 23:10
Luna Glob (Luna 25) 2023-118A 57600						in space
Russian spacecraft aimed at circumlunar orbit followed by landing near lunar south pole. Separated from Fregat rocket stage on Aug 11 at 00:10 UTC. A pair of engine firings August 16, beginning at 08:57 UTC, resulted in Luna 25 entering its initial orbit of 91 x 113 kilometres at 82°.1 inclination around the Moon. At 09:03 UTC on August 18, the orbit was lowered to 100 kilometres circular in preparation for descent and landing, expected August 21. August 19 a command was sent for a thruster firing to lower perigee to 16 km. Communication was lost at about 11:57 UTC, probably when Luna 25 crashed into the lunar surface after the thruster fired for too long a time.
Impacted on the Moon
Fregat rocket stage 2023-118B 57601						Re-entered - 2024 Feb 26 Life 200 days
Carried Luna 25 lunar lander. Manoeuvred to barycentric orbit before releasing the spacecraft. A further engine firing, on Aug 11, reportedly sent it to heliocentric orbit but Space-Track continued to issue orbit data for the barycentric orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 10, 23:10	6652	0.0010	267	281	89.99	51.73	92
2023 Oct 20, 10:22	211239	0.9016	14405	395316	16103.47	48.13	199

2023-119 Falcon 9 Block 5 (Starlink Group 06-09) Cape Canaveral Space Force Station						2023 Aug 11, 05:17
Starlink 30166 2023-119A 57602						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:22 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 22, 18:00	6704	0.0004	323	329	91.05	43.00	187
Falcon 9 second stage uncatalogued						Re-entered - 2023 Jul 28 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter above the IndianOcean at about 08:40 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-120 CZ 3B Xichang Space Centre						2023 Aug 12, 17:26
Ludi Tance 04-01 (L-SAR 04-01, Land Exploration 04-01) 2023-120A 57624						in space
Earth surface studies satellite equipped with a large, high resolution, Synthetic Aperture Radar operating at L-band frequencies. Probably entered geosynchronous drift orbit on Aug 13. Launch was delayed by 30 minutes during final countdown.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Aug 12, 21:04	24380	0.7308	184	35819	631.39	28.56	180
2023 Aug 13, 09:31	24995	0.6881	1417	35817	655.44	23.77	181
2023 Aug 22, 23:11	42166	0.0004	35773	35803	1436.15	16.10	277	89°.6 E
CZ 3B fourth stage 2023-120B 57625						Re-entered - 2023 Oct 30 Life 79 days
Launched L-SAR 04-01.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 12, 22:54	23654	0.7241	149	34403	603.41	28.55	179

2023-121 Kuaizhou 1A Xichang Space Centre						2023 Aug 14, 05:32
Head 3A 2023-121A 57626						in space
Application satellite from Head Aerospace in the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications betweeninternet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 14, 08:46	7079	0.0008	695	706	98.78	45.00	243
Head 3B 2023-121B 57627						in space
Application satellite from Head Aerospace in the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications between internet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 14, 08:46	7078	0.0007	695	705	98.78	45.00	241
Head 3C 2023-121C 57628						in space
Application satellite from Head Aerospace in the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications betweeninternet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 14, 08:45	7078	0.0007	694	705	98.76	45.00	251
Head 3D 2023-121D 57629						in space
Application satellite from Head Aerospace in the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications betweeninternet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 14, 08:46	7077	0.0007	694	704	98.76	45.00	249
Head 3E 2023-121E 57630						in space
Application satellite from Head Aerospace in the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications betweeninternet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 14, 08:45	7077	0.0007	694	703	98.75	45.00	266
Kuaizhou 1A third stage 2023-121F 57631						Re-entered - 2023 Aug 15 Life 1 day
Launched cluster of five Head 3 satellites. Perigee lowered after releasing satellites and it re-entered August 15 at 08:46 UTC ±1 minute above southern Europe.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 14, 12:57	6760	0.0400	111	653	92.19	45.00	53

2023-122 Falcon 9 Block 5 (Starlink Group 06-10) Cape Canaveral Space Force Station						2023 Aug 17, 03:36
Starlink 30309 2023-122A 57632						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:41 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 25, 18:00	6685	0.0001	306	308	90.66	43.00	336
Falcon 9 second stage uncatalogued						Re-entered - 2023 Aug 17 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-123 CZ 4C Jiuquan Space Centre						2023 Aug 20, 17:45
Gaofen 12-04 2023-123A 57654						in space
Earth observation using radar and high resolution optical sensors for Earth imaging to "support land surveys, crop management, urban and road network planning".
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Aug 20, 23:39	6975	0.0004	594	600	96.63	97.90	246	00:01
CZ 4C third stage 2023-123B 57655						in space
Launched Gaofen 12-04. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 21, 05:57	6912	0.0101	464	604	95.32	97.89	55

2023-124 Falcon 9 Block 5 (Starlink Group 07-01) Vandenberg Space Force Base						2023 Aug 22, 09:37
Starlink 30267 2023-124A 57663						in space
One member of a simultaneously-launched cluster of twenty one V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 10:40 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 6, 14:00	6731	0.0001	352	354	91.60	53.05	127
Falcon 9 second stage uncatalogued						Re-entered - 2023 Aug 22 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-125 Soyuz-2.1a Baikonur Cosmodrome						2023 Aug 23, 01:08
Progress MS-24 (Progress 7K-MS №454) 2023-125A 57691						Re-entered - 2024 Feb 13 Life 174 days
Supplies to ISS. Docked with the rear port of the Zvezda module August 25 at 03:45 UTC. Undocked 2024 February 13 at 02:08 UTC. Retro-fire at 05:16 UTC led to destructive re-entry above the southern Pacific Ocean at about 06:05 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 23, 01:39	6584	0.0027	188	224	88.61	51.65	79
2023 Aug 23, 13:18	6675	0.0035	274	320	90.46	51.64	342
2023 Aug 24, 15:04	6677	0.0034	276	321	90.49	51.65	342
2023 Aug 25, 13:25	6795	0.0005	414	420	92.91	51.64	353
2024 Feb 12, 12:21	6795	0.0002	416	419	92.91	51.64	231
Soyuz third stage 2023-125B 57692						Re-entered - 2023 Aug 25 Life 2 days
Launched Progress MS-24.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 23, 01:36	6578	0.0020	187	213	88.49	51.66	54

2023-F06 - failed to reach orbit Chollima 1 (Improved UNHA-3?) Sohae Launch Centre						2023 Aug 23, 18:50
Malligyong 1 flight model 2
North Korean government/military optical imaging satellite aimed at 500 kilometre, sun-synchronous orbit. Second version of the satellite - the first one was lost in an earlier launch failure 2023 May 30. Destroyed when the launch vehicle third stage failed, possibly through suffering an explosion caused by inadvertent triggering of the emergency auto-destruct system. Impacted in the Yellow Sea.

2023-126 Electron (We Love the Nightlife) Rocket Lab Launch Complex, New Zealand						2023 Aug 23, 23:45
Capella 11 (Acadia 1) 2023-126A 57693						in space
Third generation satellite from Capella Space carrying Synthetic Aperture Radar for Earth imaging. Member of a planned thirty satellite constellation. Released from launch vehicle August 25 at 00:43 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 26, 06:31	7023	0.0006	641	649	97.62	53.01	298
Electron third stage (kick stage) 2023-126B 57694						in space
Launched Capella 11.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 26, 06:30	7022	0.0009	638	650	97.60	53.01	286
Electron second stage 2023-126C 57695						Re-entered - 2023 Sep 11 Life 19 days
Launched Capella 11.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 24, 16:20	6797	0.0351	180	657	92.94	53.01	256

2023-127 Ceres 1 (Gushenxing 1 Y-8) Jiuquan Space Centre						2023 Aug 25, 04:59
Jilin-1 Wide Field 02A 2023-127A 57696						in space
Imaging satellite for Earth resources and land studies, particularly in relation to mining and urban construction industries.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Aug 25, 12:31	6916	0.0013	529	547	95.40	97.59	290	11:18
Ceres 1 fourth stage uncatalogued						Re-entered - 2023 Aug 25 Life <1 day
Launched Jilin-1 Wide Field 02A. Caused to re-enter after releasing the satellite.
Not Catalogued - orbit parameters unavailable

2023-128 Falcon 9 Block 5 Kennedy Space Center						2023 Aug 26, 07:27
SpaceX Dragon Crew 7 (Dragon Endurance Flight #3) 2023-128A 57697						Re-entered - 2024 Mar 12 Life 199 days Returned to Earth
Crew flight to ISS provided by SpaceX under contract to NASA. Crew members - Jasmin Moghbeli (NASA, commander), Andreas Mogensen (ESA, pilot), Satoshi Furukawa (JAXA), and Konstantin Borisov (Roscosmos). Separated from launch vehicle at 07:39 UTC. Docked with upward-facing port of the Harmony module August 27 at 13:16 UTC. Undocked, carrying original crew, 2024 March 11 at 15:20 UTC. Following a 13 minute retro-fire March 12 starting at 0856 UTC, it splashed down in the Gulf of Mexico at 09:47 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 26, 07:51	6576	0.0015	188	207	88.44	51.64	336
2023 Aug 26, 10:33	6604	0.0064	183	268	89.01	51.63	162
2023 Aug 26, 16:40	6607	0.0026	211	246	89.07	51.63	230
2023 Aug 27, 04:32	6608	0.0045	200	260	89.11	51.63	210
2023 Aug 27, 12:06	6793	0.0004	412	418	92.86	51.64	355
2023 Aug 27, 13:24	6795	0.0005	413	420	92.90	51.64	2
2024 Mar 11, 11:35	6795	0.0006	413	421	92.91	51.64	353
2024 Mar 12, 04:52	6747	0.0049	336	402	91.92	51.64	154
Falcon 9 second stage uncatalogued						Re-entered - 2023 Aug 25 Life <1 day
Launched SpaceX Dragon Crew 7. Caused to re-enter above the Indian Ocean at about 08:50 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable
Crew Dragon trunk module 2023-128B 59227						Re-entered - 2024 May 21 Life 269 days
Separated from Dragon Crew 7 2024 March 12 prior to retrofire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 Mar 12, 20:07	6747	0.0048	336	401	91.92	51.34	155

2023-129 Falcon 9 Block 5 (Starlink Group 06-11) Cape Canaveral Space Force Station						2023 Aug 27, 01:05
Starlink 30288 2023-129A 57698						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:11 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 27, 15:59	6666	0.0006	284	292	90.28	43.00	257
Falcon 9 second stage uncatalogued						Re-entered - 2023 Aug 27 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-130 CZ 2D Xichang Space Centre						2023 Aug 31, 07:36
Yaogan 39-01 Follower 1 2023-130A 57727						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-02 (launch 2022-068) and Yaogan 36-02 (launch 2022-133) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 31, 16:48	6875	0.0008	492	503	94.56	35.00	238
Yaogan 39-01 Follower 2 2023-130B 57728						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-02 (launch 2022-068) and Yaogan 36-02 (launch 2022-133) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 31, 16:48	6875	0.0009	491	503	94.55	34.99	257
Yaogan 39-01 Leader 2023-130E 57731						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-02 (launch 2022-068) and Yaogan 36-02 (launch 2022-133) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 31, 16:48	6874	0.0009	490	502	94.53	34.99	249
CZ 2D second stage 2023-130C 57729						Re-entered - 2024 Jun 23 Life 297 days
Launched Yaogan 39 Group 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Aug 31, 16:48	6875	0.0008	491	502	94.55	34.99	243

2023-131 Falcon 9 Block 5 (Starlink Group 06-13) Cape Canaveral Space Force Station						2023 Sep 1, 02:21
Starlink 30375 2023-131A 57732						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:27 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 12, 18:00	6711	0.0001	332	333	91.19	43.00	264
Falcon 9 second stage uncatalogued						Re-entered - 2023 Aug 22 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-132 PSLV-XL (PSLV C-57) Satish Dhawan Space Centre						2023 Sep 2, 06:20
Aditiya L1 2023-132A 57754						in space
Indian solar studies satellite - successive orbit raising allowed it to reach barycentric orbit from where it embarked on a trajectory to allow it to be placed in orbit around the Sun-Earth Lagrange Point 1. Apogee raised to 122,000 kilometres on September 15. Engine firing placed it in barycentric orbit September 19. Arrival in L1 halo orbit 2024 January 6.
Stationed near the L1 Lagrange Point in the Earth-Sun system
PSLV upper stage 2023-132B 57755						in space
Launched Aditiya L1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 2, 15:44	16219	0.5924	233	19449	342.61	19.19	347

2023-133 Falcon 9 Block 5 Vandenberg Space Force Base						2023 Sep 2, 14:25
Wildfire 4 (SDA Tranche 0 Data Relay 13) 2023-133A 57756						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:13	7321	0.0009	936	949	103.89	81.00	217
BB 4 (SDA Tranche 0 Target Tracker 4) 2023-133B 57757						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture", equipped with sensors to provide 'beyond line-of-sight targeting' of ships and mobile missile launchers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:21	7321	0.0009	937	949	103.90	81.00	214
Wildfire 3 (SDA Tranche 0 Data Relay 12) 2023-133C 57758						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:20	7322	0.0008	938	949	103.91	80.99	215
BB 3 (SDA Tranche 0 Target Tracker 3) 2023-133D 57760						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture", equipped with sensors to provide 'beyond line-of-sight targeting' of ships and mobile missile launchers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:18	7322	0.0008	938	949	103.92	81.00	217
Wildfire 7 (SDA Tranche 0 Data Relay 16) 2023-133E 57761						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:20	7325	0.0004	944	950	103.99	81.00	243
Checkmate 10 (SDA Tranche 0 Data Relay 9) 2023-133F 57762						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:19	7324	0.0005	941	949	103.95	81.00	220
Wildfire 6 (SDA Tranche 0 Data Relay 15) 2023-133G 57763						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:19	7324	0.0005	943	950	103.97	80.99	225
Wildfire 1 (SDA Tranche 0 Data Relay 10) 2023-133H 57764						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:14	7323	0.0006	941	949	103.94	81.00	212
Wildfire 9 (SDA Tranche 0 Data Relay 18) 2023-133J 57765						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:21	7324	0.0005	943	949	103.97	81.00	219
Wildfire 10 (SDA Tranche 0 Data Relay 19) 2023-133K 57766						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:19	7323	0.0005	941	949	103.95	81.00	218
Wildfire 2 (SDA Tranche 0 Data Relay 11) 2023-133L 57767						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:19	7325	0.0004	943	950	103.98	80.99	225
Wildfire 8 (SDA Tranche 0 Data Relay 17) 2023-133M 57768						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 07:39	7324	0.0005	942	949	103.96	80.99	223
Wildfire 5 (SDA Tranche 0 Data Relay 14) 2023-133N 57769						in space
Demonstrator for the on-orbit part of US Space Development Agency's "Proliferated Warfighter Space Architecture". Equipped with an optical communications system be used to collect data from active satellites in the constellation for onward relay to ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 3, 11:19	7324	0.0005	942	949	103.96	81.00	218
Falcon 9 upper stage uncatalogued						in space
Launched thirteen Tranche 0 satellites for the US Space Development Agency. Caused to re-enter over the south western Indian Ocean at about 16:45 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable

2023-134 Falcon 9 Block 5 (Starlink Group 06-12) Cape Canaveral Space Force Station						2023 Sep 4, 02:47
Starlink 30397 2023-134A 57771						in space
One member of a simultaneously-launched cluster of twenty one V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:52 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 8, 16:00	6680	0.0002	300	303	90.55	43.00	134
Falcon 9 second stage uncatalogued						Re-entered - 2023 Sep 4 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-135 Ceres 1S (Gushenxing 1S Y-10) Mobile floating platform, Yellow Sea - 36°.6 N, 121°.2 E						2023 Sep 5, 09:34
Tianqi 24 2023-135A 57792						in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 5, 16:04	7173	0.0011	787	802	100.76	49.97	304
Tianqi 21 2023-135B 57793						in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 5, 16:04	7172	0.0012	786	802	100.75	49.97	308
Tianqi 23 2023-135C 57794						in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 5, 16:04	7172	0.0012	785	802	100.74	49.97	310
Tianqi 22 2023-135D 57795						in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 5, 16:04	7172	0.0012	785	802	100.74	49.97	307
Ceres 1 fourth stage 2023-135E 57796						Re-entered - 2023 Sep 25 Life 20 days
Launched 4x Tianqi satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 5, 15:40	6875	0.0486	163	830	94.55	49.93	349

2023-136 CZ 4C Jiuquan Space Centre						2023 Sep 6, 18:14
Yaogan 33-03 2023-136A 57797						in space
Described as being used for remote sensing for natural resources surveys. Specific tasks include land survey, crop yield assessment, and input to disaster monitoring and prevention plans. Equipped with synthetic aperture radar for Earth imaging provided by the Institute of Space and Space Information Innovation of the Chinese Academy of Sciences. Mission is probably military or government.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Sep 7, 09:09	7062	0.0005	681	688	98.44	98.16	250	00:30
2023 Sep 23, 11:55	7067	0.0004	686	692	98.54	98.16	118	00:30
2023 Sep 24, 09:57	7074	0.0000	695	696	98.68	98.15	166	00:30
CZ 4C third stage 2023-136B 57798						in space
Launched Yaogan 33-03. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 6, 21:07	6968	0.0134	496	683	96.47	98.16	56

2023-137 H-IIA 202 (F-47) Tanegashima Space Centre						2023 Sep 6, 23:42
X-Ray Imaging and Spectroscopy Mission (XRISM) 2023-137A 57800						in space
Astronomical satellite equipped with x-ray imaging sensors to study sizeable objects such as supernova remnants and clusters of galaxies. Separated from launch vehicle at 23:56 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 7, 09:10	6952	0.0010	567	581	96.14	31.00	281
Smart Lander for Investigating the Moon (SLIM) 2023-137D 57803						Re-entered - 2024 Jan 19 Life 135 days
Lunar mission demonstrator - separated from launch vehicle September 7 at 00:30 UTC. Used its own propulsion in manoeuvres involving successive raising of apogee until transfer to barycentric orbit on September 30 following an engine firing that was completed at 17:40 UTC. It aims to enter lunar orbit and then deposit a lander on the surface about one month later. The descent vehicle is planned to eject a semi-hard landing probe just before impact in the Mare Nectaris.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 7, 20:32	55586	0.8750	569	97846	2173.72	31.06	244
2023 Sep 8, 14:41	55874	0.8799	335	98657	2190.67	30.32	244
2023 Sep 15, 16:48	62787	0.8892	581	112237	2609.56	30.99	245
H-IIA upper stage 2023-137E 57804						Re-entered - 2025 Jan 3 Life 485 days
Launched XRISM and SLIM. Initial LEO similar to XRISM then a second engine firing raised orbit to set SLIM on course for the Moon.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 7, 00:31	55569	0.8751	562	97820	2172.73	31.06	243

2023-138 Falcon 9 Block 5 (Starlink Group 06-14) Cape Canaveral Space Force Station						2023 Sep 9, 03:12
Starlink 30304 2023-138A 57808						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:28 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 13, 16:00	6674	0.0002	295	297	90.44	43.00	271
Falcon 9 second stage uncatalogued						Re-entered - 2023 Sep 9 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-139 CZ 6A (Y-5) Taiyuan Space Centre						2023 Sep 10, 04:30
Yaogan 40-01 Leader 2023-139A 57830						in space
Reported to be a remote sensing satellite monitoring the electromagnetic environment - a description that may indicate it has an electronic intelligence gathering rôle. One of three related satellites carried on the same launch. They will operate in a triangular formation separated from each other by about 120 km - a similar formation to the lower inclination Yaogan 31 satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 10, 09:19	7183	0.0010	797	812	100.97	86.00	252
2023 Sep 11, 15:18	7181	0.0011	795	811	100.94	86.00	260
2023 Sep 13, 06:17	7182	0.0011	796	811	100.95	86.00	252
2023 Sep 15, 13:35	7186	0.0011	800	816	101.04	86.00	206
2023 Sep 16, 06:49	7194	0.0019	802	829	101.21	86.00	164
2023 Sep 17, 08:04	7202	0.0029	803	845	101.37	86.00	151
2023 Sep 18, 07:58	7210	0.0018	819	845	101.54	86.00	149
2023 Sep 19, 07:34	7218	0.0015	829	852	101.73	86.00	105
2023 Sep 26, 20:54	7231	0.0002	851	854	101.98	86.00	91
2023 Nov 12, 22:13	7231	0.0002	851	854	101.98	85.99	91
Yaogan 40-01 Follower 2023-139C 57832						in space
Reported to be a remote sensing satellite monitoring the electromagnetic environment - a description that may indicate it has an electronic intelligence gathering rôle. One of three related satellites carried on the same launch. They will operate in a triangular formation separated from each other by about 120 km - a similar formation to the lower inclination Yaogan 31 satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 10, 09:34	7181	0.0011	795	811	100.93	86.00	266
2023 Sep 14, 07:32	7182	0.0010	797	812	100.96	86.00	244
2023 Sep 14, 23:00	7188	0.0006	806	814	101.09	85.99	289
2023 Sep 15, 13:36	7195	0.0003	815	820	101.24	86.00	142
2023 Sep 17, 06:24	7203	0.0019	811	839	101.40	86.00	140
2023 Sep 18, 04:25	7203	0.0015	814	836	101.40	86.00	142
2023 Sep 18, 06:04	7210	0.0008	826	837	101.54	86.00	137
2023 Sep 26, 17:30	7231	0.0002	851	854	101.99	86.00	90
2023 Nov 13, 11:50	7231	0.0002	851	854	101.98	85.99	94
Yaogan 40-01 Outlier 2023-139D 57833						in space
Reported to be a remote sensing satellite monitoring the electromagnetic environment - a description that may indicate it has an electronic intelligence gathering rôle. One of three related satellites carried on the same launch. They will operate in a triangular formation separated from each other by about 120 km - a similar formation to the lower inclination Yaogan 31 satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 10, 09:34	7181	0.0010	795	810	100.93	85.99	273
2023 Sep 15, 00:39	7178	0.0012	791	809	100.88	86.00	263
2023 Sep 15, 13:32	7173	0.0016	784	806	100.77	86.00	286
2023 Sep 16, 08:19	7169	0.0020	776	805	100.68	86.00	293
2023 Sep 17, 07:48	7165	0.0026	768	806	100.60	85.99	288
2023 Sep 17, 17:34	7165	0.0026	768	806	100.60	86.00	291
2023 Nov 13, 08:26	7231	0.0002	851	854	101.98	85.99	85
CZ 6A third stage 2023-139F 57835						in space
Launched Yaogan 40 Group 1. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 10, 09:23	7144	0.0067	718	813	100.15	86.02	8

2023-140 Atlas V 551 (NRO L-57) Cape Canaveral Space Force Station						2023 Sep 10, 12:47
USA 346 (Silent Barker 1) 2023-140A 57836						in space
Designed to observe, track, monitor and disable other countries' satellites in geosynchronous orbit. One of three simultaneously-launched satellites. Orbit parameters are classified 'secret'.
Geosynchronous Drift Orbit - parameters awaited
USA 347 (Silent Barker 2) 2023-140B 57837						in space
Designed to observe, track, monitor and disable other countries' satellites in geosynchronous orbit. One of three simultaneously-launched satellites. Orbit parameters are classified 'secret'.
Geosynchronous Drift Orbit - parameters awaited
USA 348 (Silent Barker 3) 2023-140C 57838						in space
Designed to observe, track, monitor and disable other countries' satellites in geosynchronous orbit. One of three simultaneously-launched satellites. Orbit parameters are classified 'secret'.
Geosynchronous Drift Orbit - parameters awaited
Atlas V upper stage (Centaur) 2023-140D 57839						in space
Launched USA 346, 347 & 348. Orbit parameters are classified 'secret'.
Geosynchronous Drift Orbit - parameters awaited

2023-141 Falcon 9 Block 5 (Starlink Group 07-02) Cape Canaveral Space Force Station						2023 Sep 12, 06:57
Starlink 30285 2023-141A 57840						in space
One member of a simultaneously-launched cluster of twenty one V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 08:00 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
Orbit parameters awaited
Falcon 9 second stage uncatalogued						Re-entered - 2023 Sep 12 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-142 Firefly Alpha (FLTA003) Vandenberg Space Force Base						2023 Sep 15, 02:28
Victus Nox (TacRS 3) 2023-142A 57861						Re-entered - 2025 Jan 28 Life 501 days
Satellite with a "space domain awareness mission" involving tracking other objects in orbit. Used to demonstrate rapid assembly and launch with the satellite being delivered to the launch site and the rocket being made ready for lift within 24 hours of the order being issued.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Sep 15, 07:12	6882	0.0040	476	531	94.69	97.32	239	18:04
2023 Sep 19, 17:00	6919	0.0015	530	552	95.46	97.29	81	18:03
2023 Sep 20, 17:54	6879	0.0073	451	551	94.63	97.24	57	18:03
2023 Sep 23, 03:07	6869	0.0058	450	531	94.42	97.29	50	18:03
2023 Sep 26, 03:43	6869	0.0060	450	532	94.43	97.30	39	18:03
2023 Sep 26, 17:17	6867	0.0064	445	533	94.39	97.30	47	18:03
2023 Sep 30, 11:15	6871	0.0057	454	532	94.47	97.27	38	18:03
2023 Oct 4, 17:56	6884	0.0062	463	549	94.74	97.33	23	18:03
2023 Oct 11, 22:07	6870	0.0051	457	527	94.44	97.32	15	18:03
2023 Oct 14, 18:57	6871	0.0050	458	528	94.47	97.32	8	18:03
2023 Oct 19, 09:17	6842	0.0013	455	472	93.87	97.32	305	18:03
2023 Oct 21, 13:09	6843	0.0011	457	472	93.89	97.33	290	18:03
2023 Oct 27, 10:06	6839	0.0010	454	468	93.81	97.32	294	18:03
Firefly Alpha second stage uncatalogued						in space
Launched Victus Nox. Caused to re-enter above the western Pacific Ocean at about 04:10 UTC at the end of its first circuit.
Not Catalogued - orbit parameters unavailable

2023-143 Soyuz-2.1a Baikonur Cosmodrome						2023 Sep 15, 15:44
Soyuz MS-24 (Soyuz 11F732A48 № 755) 2022-143A 57862						Re-entered - 2024 Apr 6 Life 204 days Returned to Earth
Carried crew to ISS - Oleg Kononenko (commander) and Nikolai Chub (both Roscosmos) and Loral O'Hara (NASA). Separated from launch vehicle at 11:53 UTC. Docked with the Rassvet module of ISS at 18:53 UTC. Undocked 2024 Apr 6 at 03:54 UTC carrying Oleg Novitsky (Roscosmos), Marina Vasilevskaya (Belarus) and Laural O'Hara. Retro-fire at 06:23 UTC led to landing near Karaganda, Kazakhstan at 07:17 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 15, 16:14	6591	0.0024	197	228	88.75	51.65	87
2023 Sep 15, 23:37	6797	0.0006	415	423	92.94	51.64	24
2024 Apr 5, 19:53	6795	0.0005	414	420	92.91	51.64	39
Soyuz third stage 2023-143B 57863						Re-entered - 2023 Sep 18 Life 3 days
Launched Soyuz MS-24.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 15, 23:21	6585	0.0022	192	221	88.63	51.65	71

2023-144 Falcon 9 Block 5 (Starlink Group 06-16) Cape Canaveral Space Force Station						2023 Sep 17, 03:38
Starlink 30432 2023-144A 57864						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:43 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 20, 16:00	6680	0.0002	300	303	90.55	43.00	152
Falcon 9 second stage uncatalogued						Re-entered - 2023 Sep 17 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-145 CZ 2D (Y-83) Xichang Space Centre						2023 Sep 17, 04:13
Yaogan 39-02 Follower 1 2023-145A 57886						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-03 (launch 2022-088) and Yaogan 36-04 (launch 2022-171) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 17, 16:57	6874	0.0008	491	502	94.54	35.00	267
Yaogan 39-02 Leader 2023-145D 57889						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-03 (launch 2022-088) and Yaogan 36-04 (launch 2022-171) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 17, 16:45	6872	0.0010	487	501	94.49	35.00	289
Yaogan 39-02 Follower 2 2023-145E 57890						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-03 (launch 2022-088) and Yaogan 36-04 (launch 2022-171) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 17, 20:07	6873	0.0009	489	501	94.51	35.00	283
CZ 2D second stage 2023-145B 57887						Re-entered - 2024 Jun 23 Life 280 days
Launched Yaogan 39 Group 2.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 17, 16:57	6874	0.0010	489	502	94.53	35.00	267

2023-F07 - failed to reach orbit Electron (We Love the Nightlife) Rocket Lab Launch Complex, New Zealand						2023 Sep 19, 06:55
Capella 12 (Acadia 2)
Third generation satellite from Capella Space carrying Synthetic Aperture Radar for Earth imaging. Intended member of a planned thirty satellite constellation. Aimed at 645 km, 53° orbit. Lost when the launch vehicle second stage failed to ignite.

2023-146 Falcon 9 Block 5 (Starlink Group 06-17) Cape Canaveral Space Force Station						2023 Sep 20, 03:38
Starlink 30465 2023-146A 57891						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:44 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 25, 18:00	6680	0.0005	299	306	90.56	43.00	132
Falcon 9 second stage uncatalogued						Re-entered - 2023 Sep 20 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-F08 - failed to reach orbit Ceres 1 (Gushenxing 1 Y-11, Autumn Sonata) Jiuquan Space Centre						2023 Sep 21, 04:59
Jilin-1 High Resolution 04B (Jilin-1 GF4B 01)
High resolution, multi-spectral imaging satellite. Lost when the launch vehicle first stage failed to complete its task. Aimed at sun-synchronous orbit with LTDN around 11:20.

2023-147 Falcon 9 Block 5 (Starlink Group 06-18) Cape Canaveral Space Force Station						2023 Sep 24, 03:38
Starlink 30450 2023-147A 57913						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:43 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 28, 16:00	6676	0.0004	295	300	90.47	43.00	125
Falcon 9 second stage uncatalogued						Re-entered - 2023 Sep 24 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-148 Falcon 9 Block 5 (Starlink Group 07-03) Vandenberg Space Force Base						2023 Sep 26, 08:48
Starlink 30712 2023-148A 57935						in space
One member of a simultaneously-launched cluster of twenty one V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 09:51 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 29, 14:00	6673	0.0001	294	296	90.42	53.06	104
Falcon 9 second stage uncatalogued						Re-entered - 2023 Sep 26 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-149 CZ 4C Jiuquan Space Centre						2023 Sep 26, 20:14
Yaogan 33-04 2023-149A 57958						in space
Described as being used for remote sensing for natural resources surveys. Specific tasks include land survey, crop yield assessment, and input to disaster monitoring and prevention plans. Equipped with synthetic aperture radar for Earth imaging provided by the Institute of Space and Space Information Innovation of the Chinese Academy of Sciences. Mission is probably military or government.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Sep 27, 13:46	7062	0.0005	680	688	98.44	98.07	244	02:31
2023 Sep 28, 08:22	7065	0.0002	686	688	98.50	98.07	301	02:31
CZ 4C third stage 2023-149B 57959						in space
Launched Yaogan 33-04. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 26, 23:20	6974	0.0126	509	684	96.61	98.08	54

2023-150 Qased (Messenger) Shahroud Test Centre, Dasht-e Kavir, Iran						2023 Sep 27, 05:58
Nour 3 (Light 3) 2023-150A 57962						Re-entered - 2024 Aug 16 Life 324 days
6U Cubesat (probably) - military satellite launched by the Iranian Revolutionary Guard Corps, probably for low resolution Earth imaging. Orbit height and RAAN are similar to Nour 2 but inclination is slightly different. Launch time is an estimate derived from initial orbit data.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 27, 13:47	6827	0.0010	442	456	93.57	60.02	265
Qased upper stage 2023-150B 57963						Re-entered - 2024 Dec 6 Life 436 days
Launched Nour 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Sep 27, 13:51	6832	0.0012	446	462	93.67	60.02	227

2023-151 Falcon 9 Block 5 (Starlink Group 06-19) Cape Canaveral Space Force Station						2023 Sep 30, 02:00
Starlink 30396 2023-151A 57964						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:05 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 5, 16:00	6672	0.0002	293	295	90.40	43.00	276
Falcon 9 second stage uncatalogued						Re-entered - 2023 Sep 30 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-152 CZ 2D Xichang Space Centre						2023 Oct 5, 00:24
Yaogan 39-03 Follower 2 2023-152A 57986						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-01 (launch 2021-101) and Yaogan 36-01 (launch 2022-120) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 5, 06:34	6875	0.0007	492	502	94.55	34.99	242
Yaogan 39-03 Leader 2023-152C 57988						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-03 (launch 2021-101) and Yaogan 36-04 (launch 2022-120) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 5, 06:31	6874	0.0008	490	501	94.52	34.99	262
Yaogan 39-03 Follower 1 2023-152D 57989						Re-entered - 2024 Jun 30 Life 269 days
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-03 (launch 2021-101) and Yaogan 36-04 (launch 2022-120) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 5, 06:31	6873	0.0009	489	501	94.52	34.99	266
CZ 2D second stage 2023-152B 57987						Re-entered - 2024 Aug 4 Life 304 days
Launched Yaogan 39 Group 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 5, 06:32	6874	0.0007	491	501	94.53	34.99	249

2023-153 Falcon 9 Block 5 (Starlink Group 06-21) Cape Canaveral Space Force Station						2023 Oct 5, 05:36
Starlink 30537 2023-153A 57991						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:41 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 11, 18:00	6678	0.0002	299	301	90.51	43.00	255
Falcon 9 second stage uncatalogued						Re-entered - 2023 Oct 5 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-154 Atlas V 501 (AV-104) Cape Canaveral Space Force Station						2023 Oct 6, 18:06
Kuipersat 2 (Kuiper Protoflight 2) 2023-154A 58013						Re-entered - 2025 Apr 29 Life 571 days
Comsat owned by Amazon - prototype for a planned constellation of 3236 broadband communications satellites. Target operational orbit for the constellation is 610 km ±10 km. The name is derived from the Kuiper belt and was chosen to reflect the fact that the quantity of satellites involved is a rather large number.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 8, 04:19	6872	0.0016	482	504	94.48	29.99	325
2023 Oct 22, 13:58	6869	0.0016	480	502	94.44	29.99	112
2023 Oct 23, 10:23	6870	0.0016	481	502	94.44	29.99	123
2023 Oct 27, 10:14	6870	0.0016	481	503	94.45	29.99	161
Kuipersat 1 (Kuiper Protoflight 1) 2023-154B 58014						Re-entered - 2024 Sep 29 Life 359 days
Comsat owned by Amazon - prototype for a planned constellation of 3236 broadband communications satellites. Target operational orbit for the constellation is 610 km ±10 km. The name is derived from the Kuiper belt and was chosen to reflect the fact that the quantity of satellites involved is a rather large number.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 11, 19:20	6871	0.0015	483	503	94.48	29.99	357
Atlas V upper stage (Centaur) 2023-154C 58015						in space
Launched Kuipersat 1 & 2. Initial orbit similar to satellites then engine re-start reportedly sent it to heliocentric orbit.
Heliocentric orbit

2023-155 Vega-C (VV-23) Centre Spatiale Guyanaise						2023 Oct 9, 01:36
THEOS 2 (Thailand Earth Observation System 2) 2023-155A 58016						in space
Very high resolution optical imaging satellite. Released from launch vehicle at 02:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 9, 22:48	6982	0.0001	603	605	96.77	97.93	24	10:14
2023 Oct 12, 03:53	6988	0.0001	609	611	96.89	97.93	88	10:14
Formosat 7R (Triton) 2023-155B 58017						in space
Experimental satellite designed and manufactured by TASA (Taiwan Space Agency). Carries both a science payload and a meteorological studies payload using the effect of the upper atmosphere on received GPS signals to study the upper atmosphere. It will join the existing Formosat 7 cluster on orbit. Carries a GNSS receiver to detect radio signals reflected from the upper atmosphere to be used in meteorological studies. Released from launch vehicle at 02:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 9, 22:48	6982	0.0001	603	605	96.76	97.93	39	10:14
ANSER Follower 2 (Advanced Nanosatellite Systems for Earth observation Research) 2023-155C 58018						in space
3U Cubesat - one a triplet of satellites from Spain's INTA (Instituto Nacional de Tecnica Aerospacial) carried on the same launch vehicle and working together on an optical Earth imaging system. One satellite, ANSER Leader, was lost when it failed to separate from the launch vehicle. The design uses aerodynamic surfaces to control the orbit and maintain formation with the other satellite. Released from launch vehicle at 03:19 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 10, 03:30	6949	0.0005	568	574	96.08	97.67	355	10:13
ANSER Follower 1 (Advanced Nanosatellite Systems for Earth observation Research) 2023-155D 58019						in space
3U Cubesat - one a triplet of satellites from Spain's INTA (Instituto Nacional de Tecnica Aerospacial) carried on the same launch vehicle and working together on an optical Earth imaging system. One satellite, ANSER Leader, was lost when it failed to separate from the launch vehicle. The design uses aerodynamic surfaces to control the orbit and maintain formation with the other satellite. Released from launch vehicle at 03:19 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 10, 03:30	6949	0.0006	567	575	96.08	97.67	343	10:13
N3SS (Nanosat 3U pour la Surveillance du Spectre) 2023-155E 58020						in space
3U Cubesat - from CNES and carrying a payload to detect and pinpoint locations of radio jamming stations. Release from launch vehicle scheduled at 03:19 UTC but may have remained attached.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 10, 03:24	6948	0.0005	567	574	96.07	97.67	349	10:13
CSC 2 2023-155F 58021						in space
6U Cubesat - one of a pair of multi-payload satellites carried on the same launch vehicle. Released from launch at 03:19 UTC. Catalogue number and Designation deduced by Nico Janssen using radio observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 10, 03:23	6948	0.0003	568	572	96.06	97.67	15	10:13
CSC 1 2023-155G 58022						in space
6U Cubesat - one of a pair of multi-payload satellites carried on the same launch vehicle. Released from launch vehicle at 03:19 UTC. Catalogue number and Designation deduced by Nico Janssen using radio observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 10, 03:23	6948	0.0003	568	572	96.06	97.67	20	10:13
PRETTY (Passive REflecTomeTry and dosimetrY) 2023-155H 58023						in space
3U Cubesat - demonstrator satellite carrying a GPS radio signal receiver for upper atmosphere studies. Released from launch vehicle at 03:19 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 10, 03:23	6946	0.0001	568	569	96.03	97.67	340	10:13
MACSat 2023-155J 58024						in space
6U Cubesat - on-orbit demostration of a 5G internet communication system. Released from launch vehicle at 03:19 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 10, 03:23	6946	0.0001	567	569	96.02	97.68	278	10:13
PVCC (Proba-V Companion Cubesat) 2023-155K 58025						in space
12U Cubesat - ESA mission to demonstrate a calibration system for optical imaging satellites. The onboard instrument is a spare sensor from construction of the Proba-V satellite. Released from launch vehicle at 03:19 UTC..
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 10, 03:23	6945	0.0002	566	569	96.01	97.66	232	10:13
Vega upper stage (AVUM) uncatalogued						Re-entered - 2023 Oct 9 Life <1 day
Launched THEOS 2, Formosat 7R and carried a further ten cubesats. Retro-fire at 03:26 UTC led to re-entry above the Pacific Ocean at around 04:00 UTC. Two of the cubesats remained attached and re-entered with the AVUM: ESTCube - 3U Cubesat from the University of Tartu, Estonia, equipped with a pair of Earth observation cameras and a solar sail to act as a braking device to accelerate re-entry at planned end of mission, ANSER Leader - one a triplet of 3U Cubesats from Spain's INTA (Instituto Nacional de Tecnica Aerospacial) intended to work together on an optical Earth imaging mission.
Not Catalogued - orbit parameters unavailable

2023-156 Falcon 9 Block 5 (Starlink Group 07-04) Vandenberg Space Force Base						2023 Oct 9, 07:43
Starlink 30514 2023-156A 58028						in space
One member of a simultaneously-launched cluster of twenty one V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 08:48 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 16, 22:00	6681	0.0001	302	303	90.57	53.05	80
Falcon 9 second stage uncatalogued						Re-entered - 2023 Oct 9 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-157 Falcon 9 Heavy Kennedy Space Center						2023 Oct 13, 14:19
Psyche 2023-157A 58049						in space
NASA mission to explore the origin of planetary cores by studying the metallic asteroid Psyche, from which the vehicle takes its name. Released from launch vehicle at 15:21 UTC. Asteroid arrival expected 2029 August.
Heliocentric orbit
Falcon 9 Heavy third stage 2023-157B 58050						in space
Launched Psyche. Was briefly in 157 x 797 km orbit at 30° inclination before re-ignition to send it to heliocentric orbit where it released the spacecraft.
Heliocentric orbit

2023-158 Falcon 9 Block 5 (Starlink Group 06-22) Cape Canaveral Space Force Station						2023 Oct 13, 23:01
Starlink 30568 2023-158A 58051						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle Oct 14 at 00:06 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 20, 14:00	6671	0.0002	292	294	90.38	43.00	269
Falcon 9 second stage uncatalogued						Re-entered - 2023 Oct 14 Life 1 day
Launched twenty two Starlink satellites. Caused to re-enter Oct 14 above the Indian Ocean at about 00:30 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-159 CZ 2D (Y-77) Jiuquan Space Centre						2023 Oct 15, 00:54
Yunhai-1 04 2023-159A 58073						in space
Meteorological satellite developed by the Shanghai Academy of Spaceflight Technology (SAST) to be used for observation of atmospheric, marine and space environments, disaster prevention and scientific experiments. Replacement for Yunhai 1-02 (44547, 2019-063A) that disintegrated 2021 March in a collision with a piece of orbital debris.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Oct 15, 03:57	7143	0.0012	756	773	100.13	98.60	257	07:10
2023 Oct 23, 02:28	7145	0.0015	756	777	100.18	98.59	220	07:10
2023 Oct 23, 14:12	7151	0.0007	768	778	100.30	98.59	196	07:11
2023 Oct 24, 05:22	7157	0.0003	777	781	100.43	98.59	303	07:11
2023 Oct 24, 13:10	7159	0.0000	781	781	100.48	98.59	243	07:11
CZ 2D second stage 2023-159B 58074						in space
Launched Yunhai 1-04. Orbit raised after releasing satellite, possibly through the stage being wrongly oriented. It was expected to lower perigee and maintain apogee at the altitude of the satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 15, 03:58	7174	0.0098	726	867	100.80	98.52	282

2023-160 Falcon 9 Block 5 (Starlink Group 06-23) Cape Canaveral Space Force Station						2023 Oct 18, 00:39
Starlink 30604 2023-160A 58075						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 01:44 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 23, 18:00	6675	0.0002	295	297	90.45	43.00	254
Falcon 9 second stage uncatalogued						Re-entered - 2023 Oct 18 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-161 Falcon 9 Block 5 (Starlink Group 07-05) Vandenberg Space Force Base						2023 Oct 21, 08:23
Starlink 30594 2023-161A 58097						in space
One member of a simultaneously-launched cluster of twenty one V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 09:25UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 26, 16:00	6680	0.0001	302	303	90.57	53.06	82
Falcon 9 second stage uncatalogued						Re-entered - 2023 Oct 21 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-162 Falcon 9 Block 5 (Starlink Group 06-24) Cape Canaveral Space Force Station						2023 Oct 22, 02:17
Starlink 30795 2023-162A 58118						in space
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:22 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 26, 16:00	6673	0.0002	294	296	90.42	43.01	275
Falcon 9 second stage uncatalogued						Re-entered - 2023 Oct 22 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-163 CZ 2D Xichang Space Centre						2023 Oct 23, 20:03
Yaogan 39-04 Follower 1 2023-163A 58141						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-05 (launch 2022-109) and Yaogan 36-03 (launch 2022-160) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 24, 10:15	6875	0.0008	491	502	94.55	35.00	266
Yaogan 39-04 Follower 2 2023-163C 58143						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-05 (launch 2022-109) and Yaogan 36-03 (launch 2022-160) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 24, 10:23	6874	0.0009	489	502	94.53	35.00	274
Yaogan 39-04 Leader 2023-163E 58145						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-05 (launch 2022-109) and Yaogan 36-03 (launch 2022-160) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 24, 10:27	6873	0.0009	489	501	94.51	35.00	282
CZ 2D second stage 2023-163B 58142						Re-entered - 2024 Oct 9 Life 352 days
Launched Yaogan 39 Group 4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 24, 10:15	6874	0.0009	490	502	94.54	35.00	270

2023-I08 Manual release during EVA International Space Station						2023 Oct 25, 23:20
Parus-MGTU 1998-067VZ 58173						Re-entered - 2023 Nov 12 Life 18 days
1U Cubesat from the Bauman State Technical University of Russia carrying a solar sail experiment. One, or both, of the 5 m x 0.04 m sails failed to deploy.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 30, 15:26	6777	0.0008	393	404	92.53	51.63	30

2023-164 CZ 2F Jiuquan Space Centre						2023 Oct 26, 03:14
Shenzhou 17 2023-164A 58146						Re-entered - 2024 Apr 30 Life 187 days Returned to Earth
Crew to CSS - Tang Hongbo, Tang Shengjie and Jiang Xinlin. Separated from launch vehicle at 03:23 UTC. Docked with the forward-facing port of Tianhe Oct 26 at 10:46 UTC. Initial orbit shown is derived from Chinese data. Undocked 2024 April 30 at 00:43 UTC. Retro-fire at about 08:56 UTC led to touchdown at the Dong Feng landing zone near the Jiuquan Space Centre at 09:46 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 26, 03:24	6653	0.0129	189	360	90.00	41.59	110
2023 Oct 26, 10:29	6765	0.0005	384	390	92.29	41.47	330
2024 Apr 29, 22:53	6758	0.0004	377	382	92.15	41.47	272
CZ 2F third stage 2023-164B 58147						Re-entered - 2023 Nov 3 Life 8 days
Launched Shenzhou 17.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 26, 16:53	6648	0.0113	194	345	89.90	41.48	127
Shenzhou 17 Orbital Module 2023-164C 59624						Re-entered - 2024 Dec 19 Life 420 days
Released from Shenzhou 17 on 2024 April 30 at 08:56 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 May 1, 10:24	6761	0.0007	378	387	92.20	41.48	294

2023-165 Soyuz-2.1b Plesetsk Cosmodrome						2023 Oct 27, 06:04
Cosmos 2570 (Lotos-S1 № 7) 2023-165A 58148						in space
Electronic intelligence gathering - signals intelligence (SIGINT) satellite. Vehicle is based on the design of the Yantar satellite. Orbit expected to be raised to 900 km circular. Launch time estimated from initial orbit data. Orbit raised to 900 kilometres October 29 at about 02:15 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 27, 07:46	6948	0.0475	239	900	96.06	67.14	92
2023 Oct 28, 12:45	6950	0.0471	245	899	96.11	67.14	91
2023 Oct 30, 14:47	7283	0.0015	894	915	103.08	67.14	340
2023 Oct 31, 05:07	7286	0.0011	900	915	103.15	67.16	321
2023 Nov 1, 10:18	7281	0.0008	897	908	103.05	67.15	296
Cosmos 2571 2023-165C 58172						in space
Small military/government satellite, purpose undisclosed. Separated from 2023-165C on October 29 at about 08:15 UTC and conducted multiple orbital manoeuvres including rendezvous with its own carrier vehicle 2024 December 5.It then increased its orbit height slightly to fall back at ~20 kilometres per day. Possible re-flight of the intended mission of Cosmos 2566 (54817, 2022-163D) that may have failed shortly after launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 29, 21:36	7282	0.0014	893	914	103.06	67.14	335
2024 Jan 11, 16:50	7282	0.0018	891	917	103.08	67.15	292
2024 Jan 12, 22:03	7282	0.0019	890	917	103.06	67.15	290
2024 Jan 17, 22:58	7290	0.0008	906	918	103.25	67.15	313
2024 May 29, 14:16	7288	0.0015	899	922	103.21	67.15	265
2024 Jun 19, 14:20	7287	0.0018	895	921	103.17	67.15	256
2024 Jun 26, 21:45	7290	0.0018	899	925	103.24	67.14	237
2024 Jun 28, 13:20	7291	0.0019	899	927	103.27	67.16	241
2024 Jul 7, 12:31	7291	0.0019	900	927	103.27	67.15	236
2024 Jul 31, 21:46	7282	0.0011	895	912	103.06	67.16	171
2024 Aug 16, 12:16	7277	0.0015	888	909	102.95	67.16	132
2024 Aug 20, 12:19	7265	0.0001	886	888	102.71	67.16	325
2024 Nov 20, 16:19	7269	0.0011	883	899	102.80	67.16	287
2024 Nov 22, 14:38	7277	0.0006	895	903	102.97	67.16	3
2024 Nov 26, 18:11	7280	0.0008	896	907	103.03	67.16	23
2024 Nov 29, 16:36	7281	0.0009	896	909	103.05	67.15	30
2024 Nov 30, 21:48	7281	0.0009	896	909	103.05	67.15	29
2024 Dec 3, 18:31	7283	0.0012	896	914	103.09	67.15	22
2024 Dec 4, 13:25	7282	0.0009	897	910	103.06	67.15	28
payload adaptor? 2023-165D 58428						in space
Separated from Cosmos 2570 on October 29 at around 12:00 UTC. Released Cosmos 2571 on November 23. Used as rendezvous/inspection target by Cosmos 2571 around 2024 Nov 29.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 25, 04:06	7282	0.0017	891	916	103.06	67.15	320
2024 Nov 29, 16:36	7281	0.0010	896	910	103.06	67.15	29
Soyuz third stage 2023-165B 58149						Re-entered - 2024 Apr 13 Life 169 days
Launched Cosmos 2570.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Oct 27, 07:45	6936	0.0463	236	879	95.80	67.14	92

2023-166 Falcon 9 Block 5 (Starlink Group 07-06) Vandenberg Space Force Base						2023 Oct 29, 09:00
Starlink 30802 2023-166A 58150						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 10:02 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 3, 16:00	6679	0.0001	300	301	90.53	53.06	125
Falcon 9 second stage uncatalogued						Re-entered - 2023 Oct 29 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-167 Falcon 9 Block 5 (Starlink Group 06-25) Cape Canaveral Space Force Station						2023 Oct 30, 23:20
Starlink 30753 2023-167A 58175						in space
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle on November 1 at 00:25 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 7, 18:00	6690	0.0002	310	313	90.76	43.01	274
Falcon 9 second stage uncatalogued						Re-entered - 2023 Oct 31 Life 1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-168 CZ 6A (Y-4) Taiyuan Space Centre						2023 Oct 31, 22:50
Tianhui 5A 2023-168A 58199						in space
One of a pair of satellites carried on the same launch vehicle. Second generation cartographic and imaging satellite using radar. Orbiting in close formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 1, 07:02	6987	0.0002	607	610	96.87	97.83	174	06:00
Tianhui 5B 2023-168C 58201						in space
One of a pair of satellites carried on the same launch vehicle. Second generation cartographic and imaging satellite using radar. Orbiting in close formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 1, 07:02	6986	0.0001	607	609	96.85	97.83	208	06:00
CZ 6A third stage 2023-168B 58200						in space
Launched Tianhui 5 pair of satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 1, 06:54	6932	0.0080	498	609	95.73	97.82	30

2023-169 CZ 7A (Y-6) Wenchang Space Centre						2023 Nov 3, 14:54
Tongxin Jishu Shiyan 10 (Communication Technology Test 10, TJS 10) 2023-169A 58204						in space
Described as a technology test satellite used mainly for multi-band and high-speed satellite communication technology , TJS 10 is probably military in nature and possibly with a SIGINT rôle. Released from launch vehicle at around 15:20 UTC. Propelled itself from GTO to GEO drift orbit Nov 4 at around 07:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Nov 3, 21:00	24387	0.7311	179	35838	631.68	16.96	180
2023 Nov 9, 16:41	42118	0.0041	35567	35914	1433.73	0.10	42	172°.6 E
2023 Nov 10, 19:35	42165	0.0003	35776	35798	1436.11	0.09	247	173°.3 E
CZ 7A fourth stage 2023-169B 58205						Re-entered - 2024 Jan 14 Life 72 days
Launched TJS 10.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 3, 20:58	23589	0.7249	112	34310	600.94	16.97	178

2023-170 Falcon 9 Block 5 (Starlink Group 06-26) Cape Canaveral Space Force Station						2023 Nov 4, 00:37
Starlink 30800 2023-170A 58206						in space
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 01:23 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 9, 18:00	6680	0.0002	301	303	90.56	43.01	264
Falcon 9 second stage uncatalogued						Re-entered - 2023 Nov 4 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-171 Falcon 9 Block 5 (Starlink Group 06-27) Cape Canaveral Space Force Station						2023 Nov 8, 05:05
Starlink 30861 2023-171A 58230						in space
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:10 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 14, 16:00	6689	0.0002	309	312	90.73	43.01	273
Falcon 9 second stage uncatalogued						Re-entered - 2023 Nov 8 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-172 CZ 3B Xichang Space Centre						2023 Nov 9, 11:23
Zhongxing 6E (Chinasat 6E) 2023-172A 58253						in space
Comsat providing radio, TV and general communications to mainland China and its territorial waters, and to other users in the Asia-Pacific region. Manoeuvred to geosynchronous drift orbit November 10 at about 03:30 UTC. Expected location - 115°.5 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Nov 9, 16:38	24363	0.7294	215	35755	630.77	28.40	179
2023 Nov 17, 16:43	42164	0.0003	35773	35799	1436.06	0.07	264	129°.8 E
2023 Nov 24, 21:13	42273	0.0001	35890	35899	1441.63	0.05	271
2023 Dec 5, 17:02	42182	0.0003	35791	35817	1436.97	0.03	206	115°.6 E
2023 Dec 5, 22:06	42164	0.0001	35781	35791	1436.06	0.03	223	115°.5 E
CZ 3B fourth stage 2023-172B 58254						Re-entered - 2024 Apr 22 Life 165 days
Launched Zhongxing 6E.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 9, 16:57	23682	0.7231	179	34428	604.48	28.40	179

2023-173 Falcon 9 Block 5 Kennedy Space Center						2023 Nov 10, 01:28
SpaceX Dragon 2 CRS-29 2023-173A 58255						Re-entered - 2023 Dec 22 Life 42 days Returned to Earth
Carrying a cargo to/from the ISS under NASA's Commercial Resupply Services (CRS) contract. Separated from launch vehicle at 01:37 UTC. Docked with the forward facing port of the Harmony module of ISS November 11 at 10:07 UTC. Undocked December 21 at 22:05 UTC. Retro-fire December 22 at about 16:45 UTC led to splash down in the Atlantic Ocean off the coast of Florida at 17:33 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 10, 03:22	6580	0.0014	193	211	88.53	51.65	17
2023 Nov 10, 13:43	6663	0.0113	209	360	90.21	51.65	230
2023 Nov 10, 21:13	6787	0.0004	406	412	92.74	51.64	234
2023 Nov 11, 12:24	6797	0.0001	418	420	92.95	51.64	277
2023 Dec 21, 13:21	6793	0.0002	413	416	92.87	51.64	42
2023 Dec 22, 17:13	6695	0.0126	232	401	90.86	51.64	156
Falcon 9 second stage uncatalogued						Re-entered - 2023 Nov 10 Life <1 day
Launched Dragon CRS-29. Caused to re-enter after releasing the spacecraft.
Not Catalogued - orbit parameters unavailable
Dragon 2 trunk module 2023-173B 58641						Re-entered - 2024 Jan 11 Life 62 days
Separated from Dragon 2 CRS-29 2023 December 22 prior to retrofire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 23, 12:53	6692	0.0125	230	397	90.79	51.63	160

2023-174 Falcon 9 Block 5 (Transporter 9, Cosmic Wander)) Vandenberg Space Force Base						2023 Nov 11, 18:49
Connecta T3.1 2023-174A 58256						in space
6U Cubesat from Turkish company Plan-S as a demonstrator for a constellation of Earth observation satellites. Carries a demonstrator payload for an inter-satellite comms system. Released from launch vehicle at 19:48 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:24	6903	0.0010	517	532	95.12	97.48	220
MANTIS (Mission and Agile Nanosatellite for Terrestrial Imagery Services) 2023-174B 58257						in space
12U Cubesat from ESA equipped with a high resolution imaging system to study natural resources. Released from launch vehicle at 19:43 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:29	6903	0.0012	517	534	95.13	97.48	226	10:32
GHGSat C9 (Lemur-2 Bass, Juba) 2023-174D 58259						in space
Small satellite in a constellation being built by Spire Global for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground. Released from launch vehicle at 19:43 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:28	6904	0.0012	517	534	95.14	97.48	222
Lemur-2 (Dilightful) 2023-174E 58260						in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Released from launch vehicle at 19:45 UTC. One of seven similar satellites carried on the Transporter 9 upper stage. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:27	6903	0.0012	517	533	95.13	97.48	223
Platero 2023-174G 58262						in space
6U Cubesat equipped with Earth imaging cameras for monitoring the occurrence of hazardous environmental events such as toxic water discharges from ships Funded through Spain's Andalusian Agricultural and Fisheries Management Agency (AGAPA). Released from launch vehicle at 19:43 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:29	6904	0.0013	517	534	95.14	97.48	222
BRO 11 (Breizh Reconnaissance Orbiter 11) 2023-174J 58264						in space
6U Cubesat from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Released from launch vehicle at 19:47 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:27	6903	0.0012	517	534	95.14	97.49	222
Connecta T3.2 2023-174N 58268						in space
6U Cubesat from Turkish company Plan-S as a demonstrator for a constellation of Earth observation satellites. Carries a demonstrator payload for an inter-satellite comms system. Released from launch vehicle at 19:48 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 03:44	6903	0.0011	517	532	95.13	97.48	223
IRIS-C2 (Intelligent Remote-Sensing and Internet Satellite) 2023-174P 58269						in space
3U Cubesat from the National Cheng Kung University of Taiwan to further develop satellite design and to demonstrate a star-tracking sensor. Also includes an internet-connected comms system for message relay. Released from launch vehicle at 19:44 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:22	6902	0.0012	516	532	95.11	97.49	215	10:32
Flock 4Q-1 2023-174Q 58270						in space
3U Cubesat - part of Planet's Flock 4Q cluster of second generation imaging satellites. Released from launch vehicle at 19:48 UTC. One of thirty six similar satellites carried on the Transporter 9 launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:21	6902	0.0011	517	532	95.11	97.48	213	10:32
Tiger 6 2023-174S 58272						in space
6U Cubesat from OQ Technology equipped with a 5G internet communications payload. Released from launch vehicle at 20:04 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:21	6902	0.0009	518	530	95.11	97.48	206
Protométhée 1 2023-174T 58321						in space
16U Cubesat from a French company of the same name equipped with an imaging system and a thruster system to maintain the orbit. Released from launch vehicle at 19:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:05	6899	0.0011	514	529	95.05	97.48	188	10:32
GenMat 1 2023-174W 58276						in space
6U Cubesat from US Company Quantum Generative Materials equipped with a hyperspectral imaging system aimed a detecting mineral dposits on the Earth's surface. Released from launch vehicle at 19:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 14:46	6902	0.0009	518	531	95.12	97.48	212	10:32
Tiger 5 2023-174X 58277						in space
6U Cubesat from OQ Technology equipped with a 5G internet communications payload. Released from launch vehicle at 20:04 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:20	6902	0.0009	518	530	95.11	97.48	203
ÆTHER 1 2023-174AB 58281						in space
Small satellite from Kepler communications of Canada. Believed to be a demonstrator of a high speed broadband comm system for a future constellation. Released from launch vehicle at 20:04 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:16	6901	0.0010	516	530	95.09	97.48	206	10:32
ICEYE X31 2023-174AJ 58288						in space
Small satellite fitted with a sythetic aperture radar for Earth surface imaging. Released from launch vehicle at 20:05 UTC. One of four similar satellites carried on the Transporter 9 launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:14	6901	0.0010	516	529	95.08	97.48	206	10:32
Falconsat 10 2023-174AM 58291						in space
Small satellite from the USAF Academy carrying five experimental payloads that will be operated by cadets of the Academy. Released from launch vehicle at 20:14 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:16	6901	0.0010	516	530	95.10	97.48	200	10:32
Umbra 08 2023-174AN 58292						in space
Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Released from launch vehicle at 20:05 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:12	6900	0.0010	515	528	95.06	97.48	202
SpaceVan 001 2023-174AR 58295						in space
Orbital transfer vehicle from US company Exotrail that will release a number of satellites into differing orbits. Released from launch vehicle at 20:14 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:14	6901	0.0011	516	530	95.09	97.48	201
Pelican 1 2023-174AS 58296						in space
Small satellite from Planet Labs to demonstrate its new generation of Earth observation satellites. Released from launch vehicle at 20:13 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:14	6901	0.0011	515	530	95.09	97.48	202
Umbra 07 2023-174AT 58297						in space
Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Released from launch vehicle at 20:06 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:09	6899	0.0011	513	528	95.05	97.48	200
SPIP (multiSPectral Imagery Prototype) 2023-174AU 58298						in space
Small Earth imaging satellite - purpose unclear. Released from launch vehicle at 20:06 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:12	6901	0.0011	515	531	95.08	97.48	202	10:32
ÆTHER 2 2023-174AV 58299						in space
Small satellite from Kepler communications of Canada. Believed to be a demonstrator of a high speed broadband comm system for a future constellation. Released from launch vehicle at 20:04 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:10	6900	0.0011	514	529	95.06	97.48	199	10:32
ION SCV-013 (Ultimate Hugo) 2023-174AW 58300						in space
Satellite Carrier Vehicle built by D-Orbit. Released from launch vehicle at L+ 01:20:16. Will reportedly perform 11 satellite releases including: Lemur 2 (Nanaz) - 3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting - released 2023 December 22, , Intuition 16U Cubesat from KP Labs, equipped with a high resolution imaging system for agricultural studies - released 2023 November 25, Ymir 1 - 3U Cubesat from Saab & Orbcomm equipped with a VDES messaging system for use by ships at sea, EPICHyper 3 - 3U Cubesat equipped with a high resolution Earth imaging system, 9x PiCo-IoT - 0.3U Cubesat from Italian company Apageo Space as part of a 100 satellite constellation to provide a broadband, internet messaging system - all satellites released 2023 November 29, Crypto 3 - 3U Cubesat carrying a computing system to undertake blockchain financial transactions - released 2024 January 8, OSW Cazoria -3U Cubesat from Odyssey Spaceworks acting as an on-orbit laboratory for a pharmaceutical experiment and carrying a musical sythesiser that will transmit its sounds to Earth - released 2023 December 6. Hosted Payloads include: Radiosat & Beamasat - testbed for high speed radio transponder and aerial, Antelope - demonstration of an AI system for satellite payload monitoring and control, GEN 03 - demonstrator of new type thruster system from the Genergo company, AlbaPod 6p - carrying multiple PockeQube satellites - details awaited.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:12	6901	0.0012	515	531	95.08	97.48	202
Impulse 1 (LEO Express-1) 2023-174AX 58301						in space
Small satellite from Impulse Space with an undisclosed payload. It will act as a testbed for the design, including operation of its thruster system. Released from launch vehicle at 20:04 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 16:10	6900	0.0012	514	530	95.08	97.48	201	10:32
Observer-1A 2023-174BV 58323						in space
16U Cubesat from Nara Space of South Korea - equipped with an Earth observation system. Released from launch vehicle at 19:44 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 03:24	6899	0.0013	513	530	95.06	97.49	193
PiCo-IoT 01-A 2023-174BY 58326						in space
0.3U Cubesat from Italian company Apogeo Space as part of a 100 satellite constellation to provide a broadband, internet messaging system. Released from ION SCV-013 2023 November 29. One of nine similar satellites carried on this launch and released simultaneously from ION-SCV. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 16:20	6902	0.0010	517	531	95.11	97.48	211
BRO 10 (Breizh Reconnaissance Orbiter 10) 2023-174CD 58331						in space
6U Cubesat from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Released from launch vehicle at 19:45 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 15:59	6898	0.0010	513	527	95.02	97.48	182
GHGSat C11 (Lemur-2 JK0903EM1407, Vanguard) 2023-174CJ 58336						in space
Small satellite in a constellation being built by Spire Global for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground. Released from launch vehicle at 19:44 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 15:59	6898	0.0010	513	527	95.03	97.48	180
Barry 1 2023-174CL 58338						Re-entered - 2025 Apr 12 Life 518 days
Small satellite fromRogue Space Systems Corporation to demonstrate artificial intelligence for control and operation. Equipped with sensors to measure such as radiation, temperature fluctuations, and atmospheric dynamics. Released from launch vehicle at 19:44 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 14:21	6897	0.0011	512	526	95.01	97.48	180
Platform 5 2023-174CM 58339						Re-entered - 2025 Apr 22 Life 528 days
Mission details to follow. Released from launch vehicle at 19:44 UTC.
Orbit parameters awaited
GHGSat C11 (Lemur-2 MJR092620, Elliot) 2023-174CN 58340						in space
Small satellite in a constellation being built by Spire Global for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground. Released from launch vehicle at 19:43 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 28, 14:21	6898	0.0011	512	527	95.02	97.48	179
NinjaSat 2023-174CP 58341						in space
6U Cubesat from Japan's Mitsui Bussan Aerospace, carrying an x-ray observatory. Released from launch vehicle at 19:43 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 28, 15:55	6897	0.0010	512	526	95.01	97.48	177	10:32
Intuition 1 2023-174CW 58565						in space
6U Cubesat from ESA equipped with an AI system fror satellite control and a hyperspectral Earth imaging system. Released from ION SCV-13 around Dec 10.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 12, 18:03	6901	0.0015	513	533	95.09	97.48	156
Aman 1 2023-174xx						in space
3U Cubesat owned by the Sultanate of Oman and equipped with an Earth imaging system for studying natural resources. Replaces a satellite with the same name lost in the Virgin Orbit launch failure 2023 Jan 9. Released from launch vehicle at 19:53 UTC.
Orbit parameters awaited
Djibouti 1A 2023-174xx						in space
1U Cubesat designed to collect and relay data from remote weatherstations in Djibouti . Released from launch vehicle at 19:43 UTC.
Orbit parameters awaited
Foxconn PEARL-1C 2023-174xx						in space
6U Cubesat as a demonstrator for a broadband communications system. Released from launch vehicle at 19:45 UTC.
Orbit parameters awaited
Foxconn Pearl-1H 2023-174xx						in space
6U Cubesat as a demonstrator for a broadband communications system. Released from launch vehicle at 19:48 UTC.
Orbit parameters awaited
Hello Test 1 2023-174xx						in space
1p PocketQube from Turkish company Hello Space equipped as part of a planned constellation of Internet comsats. Released from launch vehicle at 19:48 UTC.
Orbit parameters awaited
Hello Test 2 2023-174xx						in space
1p PocketQube from Turkish company Hello Space equipped as part of a planned constellation of Internet comsats. Released from launch vehicle at 19:48 UTC.
Orbit parameters awaited
Heron Mark II 2023-174xx						in space
3U Cubesat from Canada's University of Toronto Aerospace Team equipped with an amateur radio system. Released from launch vehicle at 20:04 UTC.
Orbit parameters awaited
JinjuSat 1 2023-174xx						in space
2U Cubesat from Jinju City Testing Laboratory and Gyeongsang National University of South Korea. Equipped with an Earth imaging camera system. Released from launch vehicle at 19:48 UTC.
Orbit parameters awaited
KAFASat (Korea Air Force Academy Satellite) 2023-174xx						in space
3U Cubesat from South Korea's Air Force Academy to be used to give cadets the experience of operating an Earth observation satellite. Released from launch vehicle at 20:09 UTC.
Orbit parameters awaited
OMNI-LER1 2023-174xx						in space
Small satellite, possibly a Cubesat, to demonstrate blockchain financial transactions in orbit. Released from launch vehicle at 19:49 UTC.
Orbit parameters awaited
OrbAstro PC1 2023-174xx						in space
Mission details to follow. Released from launch vehicle at 19:48 UTC.
Orbit parameters awaited
OrbAstro TR1 2023-174xx						in space
6U Cubesat from OrbAstro, built for an undisclosed customer. Purpose currently unknown. Released from launch vehicle at 19:44 UTC.
Orbit parameters awaited
Outpost Ferry 1-02 (Mission 2: Debug As You Go) 2023-174xx						in space
3U Cubesat from US company Outpost. Test of electronics and comms systems for a future recoverable and reusable satellite. Carries the GasPak payload for NASA Langley - a cool gas generator developed to support NASA’s inflatable heat shield technology. Also carries a GPS system from ETH Zurich to get flight experience. Released from launch vehicle at 19:46 UTC.
Orbit parameters awaited
Picacho 2023-174xx						in space
?U Cubesat as a test of sensors to be used in a future water and mineral detecting satellite constellation from the Lunasonde company. Released from launch vehicle at 19:48 UTC.
Orbit parameters awaited
Veronika 2023-174xx						in space
1U Cubesat - privately funded and named after the owner's daughter. Carries Earth imaging cameras and an amateur radio package.. Released from launch vehicle at 19:43 UTC.
Orbit parameters awaited
Falcon 9 second stage						in space
Launched SpaceX Transporter 9 satellite cluster.
Orbit parameters awaited

2023-175 Falcon 9 Block 5 Cape Canaveral Space Force Station						2023 Nov 12, 21:08
O3b mPower FM05 2023-175A 58346						in space
Second generation communications satellite, owned by SES, to provide broadband links between ground stations lying in the range ±45° latitude. In addition to the broad area coverage of 1st gen satellites, mPower satellites are equipped with spot beam aerials. Released from launch vehicle at 23:08 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 14, 10:51	11180	0.1970	2600	7005	196.08	9.00	185
2023 Dec 7, 20:21	11626	0.1597	3391	7105	207.94	6.83	246
2024 Jan 9, 21:24	12563	0.1199	4679	7691	233.56	4.59	321
O3b mPower FM06 2023-175B 58347						in space
Second generation communications satellite, owned by SES, to provide broadband links between ground stations lying in the range ±45° latitude. In addition to the broad area coverage of 1st gen satellites, mPower satellites are equipped with spot beam aerials. Released from launch vehicle at 23:15 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 13, 12:00	11179	0.1971	2598	7004	196.05	9.02	182
2023 Dec 7, 23:02	11613	0.1611	3365	7106	207.58	6.93	247
2024 Jan 9, 21:24	12670	0.1068	4939	7644	236.54	3.90	322
Falcon 9 second stage 2023-175C 58348						in space
Launched pair of 03b satellites..
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 14, 02:46	11176	0.1972	2594	7001	195.96	9.00	184

2023-176 CZ 2C + YZ-1S Jiuquan Space Centre						2023 Nov 16, 03:55
Haiyang 3-01 (Ocean 3-01) 2023-176A 58349						in space
Ocean and inland water colour studies environmental satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 16, 19:03	7156	0.0014	768	788	100.42	98.65	305	10:11
YZ-1S rocket stage 2023-176B 58350						Re-entered - 2023 Nov 21 Life 5 days
Launched Haiyang 3-01. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 16, 19:42	6816	0.0469	118	758	93.35	98.59	301

2023-177 Falcon 9 Block 5 (Starlink Group 06-28) Cape Canaveral Space Force Station						2023 Nov 18, 05:05
Starlink 30901 2023-177A 58351						Re-entered - 2024 May 2 Life 166 days
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:11 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 24, 20:00	6682	0.0002	303	305	90.60	43.01	281
Falcon 9 second stage uncatalogued						Re-entered - 2023 Nov 18 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-178 Falcon 9 Block 5 (Starlink Group 07-07) Vandenberg Space Force Base						2023 Nov 20, 10:30
Starlink 30911 2023-178A 58374						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 11:33 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 24, 20:00	6675	0.0001	296	297	90.45	53.06	73
Falcon 9 second stage uncatalogued						Re-entered - 2023 Nov 20 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-179 Chollima 1 (Improved UNHA-3?) Sohae Launch Centre						2023 Nov 21, 13:42
Malligyong 1 (Malligyong 1 flight model 3) 2023-179A 58400						in space
North Korean government/military optical imaging satellite, also testing new orbit adjustment thruster. Released from launch vehicle at 13:54 UTC. Made a series of daily orbit adjustments 2024 February 19-23. Orbit adjusted again 2024 June 3 with thruster firing at around 14:30 UTC. Third and final orbit adjustment took place 2024 early September when the thruster was fired five times. Third version of the satellite - the first two were lost in launch failures 2023 May 30 & August 23.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 22, 00:14	6881	0.0014	493	512	94.67	97.43	279	22:00
2024 Feb 19, 13:36	6877	0.0015	488	508	94.58	97.42	328	22:00
2024 Feb 19, 23:04	6877	0.0014	489	508	94.59	97.42	327	22:00
2024 Feb 20, 14:51	6877	0.0014	489	508	94.58	97.42	324	22:00
2024 Feb 20, 19:35	6877	0.0014	490	508	94.59	97.42	324	22:00
2024 Feb 21, 19:15	6878	0.0012	492	508	94.62	97.42	319	22:00
2024 Feb 22, 22:31	6879	0.0009	495	508	94.64	97.42	312	22:00
2024 Feb 24, 04:45	6880	0.0007	497	507	94.66	97.42	306	22:00
2024 May 24, 12:17	6876	0.0009	492	504	94.57	97.41	358	22:00
2024 Jun 3, 15:09	6875	0.0008	492	502	94.56	97.41	318	22:00
2024 Jun 4, 02:54	6876	0.0007	494	503	94.58	97.40	318	22:00
2024 Sep 6, 14:09	6876	0.0001	498	499	94.58	97.39	133	21:59
2024 Sep 7, 12:14	6877	0.0003	498	501	94.60	97.39	132	21:59
2024 Sep 8, 05:36	6879	0.0004	498	504	94.63	97.39	130	21:59
2024 Sep 8, 21:23	6880	0.0006	497	506	94.65	97.39	129	21:59
2024 Sep 9, 21:20	6881	0.0009	496	509	94.68	97.39	131	21:59
2024 Sep 10, 19:20	6882	0.0011	496	512	94.70	97.39	128	21:59
2025 Jan 16, 03:39	6875	0.0009	490	503	94.54	97.38	54	21:57
2025 Jan 19, 05:50	6882	0.0005	500	508	94.70	97.38	139	21:57
Chollima 1 upper stage 2023-179B 58401						in space
Launched Malligyong 1-03.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 22, 00:12	6868	0.0033	467	512	94.40	97.41	302

2023-180 Falcon 9 Block 5 (Starlink Group 06-29) Cape Canaveral Space Force Station						2023 Nov 22, 07:47
Starlink 30964 2023-180A 58402						in space
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 08:53 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 29, 20:00	6686	0.0002	307	309	90.68	43.01	253
Falcon 9 second stage uncatalogued						Re-entered - 2023 Nov 22 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-181 CZ 2D + YZ-3 Xichang Space Centre						2023 Nov 23, 10:00
Hulianwang Jishu Shiyan 3 (Internet Connectivity Test Satellite 3) 2023-181A 58425						in space
Test satellite for Chinese government communications system for use by Internet-connected devices. One of three carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 24, 00:26	7479	0.0013	1091	1110	107.28	49.96	299
2023 Nov 29, 02:55	7479	0.0013	1092	1111	107.29	49.96	315
2023 Dec 22, 22:59	7483	0.0012	1095	1114	107.36	49.96	26
2024 Apr 16, 21:02	7482	0.0014	1094	1114	107.35	49.96	20
Hulianwang Jishu Shiyan 4 (Internet Connectivity Test Satellite 4) 2023-181B 58426						in space
Test satellite for Chinese government communications system for use by Internet-connected devices. One of three carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 24, 00:30	7478	0.0011	1092	1108	107.26	49.96	299
2023 Dec 2, 15:28	7482	0.0011	1096	1113	107.35	49.96	328
2024 Apr 16, 21:12	7482	0.0012	1095	1113	107.35	49.96	22
Hulianwang Jishu Shiyan 5 (Internet Connectivity Test Satellite 5) 2023-181C 58427						in space
Test satellite for Chinese government communications system for use by Internet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 24, 00:30	7477	0.0011	1090	1107	107.23	49.96	289
2023 Nov 28, 19:42	7477	0.0011	1091	1107	107.24	49.96	305
2023 Dec 5, 14:19	7482	0.0011	1096	1112	107.35	49.96	326
2024 Apr 16, 21:06	7482	0.0012	1095	1113	107.35	49.96	13
YZ-3 rocket stage uncatalogued						in space
Launched three Internet Connectivity Test Satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2023-182 Soyuz-2.1b Plesetsk Cosmodrome						2023 Nov 25, 20:58
Cosmos 2572 2023-182A 58435						in space
Military satellite, manoeuvrable, mission unknown but probably intelligence gathering. Mass/cross section ratio is relatively low so it experiences high drag. Frequent operation of low thrust engine maintains orbit height near 299 km.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Nov 26, 09:06	6689	0.0015	301	322	90.75	96.63	64	12:30
2023 Dec 6, 09:15	6679	0.0014	292	311	90.55	96.62	21	12:29
2023 Dec 7, 07:54	6681	0.0015	293	313	90.57	96.62	7	12:29
2023 Dec 20, 20:38	6680	0.0022	287	316	90.55	96.62	298	12:28
2023 Dec 25, 07:51	6678	0.0023	284	315	90.52	96.63	283	12:28
2024 Jun 1, 06:18	6678	0.0015	289	309	90.51	96.70	203	12:28
2024 Nov 1, 05:30	6678	0.0024	283	316	90.51	96.69	219	12:29
Soyuz third stage 2023-182B 58436						Re-entered - 2024 Mar 2 Life 98 days
Launched Cosmos 2572.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Nov 26, 09:04	6688	0.0013	302	318	90.72	96.63	65

2023-183 Falcon 9 Block 5 (Starlink Group 06-30) Cape Canaveral Space Force Station						2023 Nov 28, 04:20
Starlink 30869 2023-183A 58437						in space
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:25 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 4, 20:00	6678	0.0002	299	302	90.53	43.00	273
Falcon 9 second stage uncatalogued						Re-entered - 2023 Nov 22 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-184 Soyuz-2.1a Baikonur Cosmodrome						2023 Dec 1, 09:25
Progress MS-25 (Progress 7K-MS №455) 2023-184A 58460						Re-entered - 2024 May 28 Life 179 days
Supplies to ISS. Docked with the Poisk module of ISS December 3 at 11:18:34 UTC with the final stage of the approach under control of the ISS crew. Undocked 2024 May 28 at 08:39 UTC. Retro-fire at 11:48 UTC led to re-entry above the southern Pacific Ocean at 12:29 UTC with any surviving debris hitting the ocean surface a few minutes later.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 1, 15:34	6651	0.0013	264	282	89.97	51.64	352
2023 Dec 3, 12:29	6795	0.0001	416	417	92.90	51.64	18
Soyuz third stage 2023-184B 58461						Re-entered - 2023 Dec 3 Life 2 days
Launched Progress MS-25.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 1, 15:29	6580	0.0028	183	220	88.53	51.65	62

2023-185 Falcon 9 Block 5 Vandenberg Space Force Base						2023 Dec 1, 18:19
GNOMES 4 (GNSS Navigation and Occultation Measurement Satellite) 2023-185A 58462						in space
Small satellite from PlanetiQ, equipped with radio receivers to observe occultations of MEO navsat signals in order to study the Earth's upper atmosphere and contribute to weather forecasting.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 1, 21:24	6940	0.0011	554	570	95.90	97.65	245	10:00
Korea 425-01 2023-185B 58463						in space
Radar imaging satellite owned by the South Korean government specifically targetting activity across the Korean peninsula. Catalogue Number and Designation to be confirmed. Released from launch vehicle at about 19:35 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 1, 23:21	6940	0.0011	554	569	95.89	97.65	249	10:00
Khoyo 2023-185C 58464						in space
Small satellite from Kanazawa University carrying an astronomical x-ray imager designed to provide early warning gamma-ray and gravitational wave bursts.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 1, 21:29	6939	0.0010	553	568	95.87	97.65	254
Bane 2023-185D 58465						in space
Small satellite from US company York Space Systems, possibly for the US government.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 1, 22:57	6896	0.0010	512	525	94.99	97.46	254
uHETSat 2023-185E 58466						in space
?U Cubesat equipped with an electric thruster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 1, 23:01	6895	0.0011	509	525	94.97	97.46	252
IRIS-E (Intelligent Remote-Sensing and Internet Satellite, Lilium 1) 2023-185F 58467						in space
3U Cubesat from the National Cheng Kung University of Taiwan. Equipped with an Earth imaging system and a demonstrator for an internet comms system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 1, 23:02	6895	0.0012	508	525	94.96	97.45	257	09:59
SpIRIT (Space Industry Responsive Intelligent Thermal) 2023-185G 58468						in space
6U Cubesat from the University of Melbourne with a payload that includes a gamma and x-ray instrument from Italy. Also equipped with an electric thruster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 2, 00:34	6894	0.0013	507	525	94.95	97.46	253
ION SCV-012 (Daring Diego) 2023-185H 58469						in space
Satellite Carrier Vehicle built by D-Orbit carrying a number of satellites and, possibly, hosted payloads.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 2, 06:59	6940	0.0011	554	569	95.89	97.65	246
Alisium 1 2023-185M 58562						in space
Details awaited
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 12, 19:54	6937	0.0008	554	564	95.83	97.66	230
Unicorn-2N 2023-185N 58642						Re-entered - 2025 Jan 3 Life 399 days
2p PocketQube satellite. Mission details to follow.
Orbit parameters awaited
EirSat (Educational Irish Research Satellite) 2023-185xx						in space
2U Cubesat from University College, Dublin carrying a gamma-ray detector, an experimental attitude control system and an experiment to test a range of surface coatings (paints?) in space. Separated from launch vehicle at about 18:36 UTC. Catalogue Number and Designation to be confirmed.
Orbit parameters awaited
ENSO (Expleo Nanosat for Solar-irradiance Observations) 2023-185xx						in space
1U Cubesat from the Space Center, University of Montpellier, France for ionosphere studies.
Orbit parameters awaited
Hayasat 2023-185xx						in space
1U Cubesat developed by Bazoomq Space Research Laboratory and the Center for Scientific Innovation and Education of Armenia equipped with a suite of instruments to measure the health of the satellite.
Orbit parameters awaited
Hello Test 3 2023-185xx						in space
1p PocketQube from Turkish company Hello Space equipped as part of a planned constellation of Internet comsats.
Orbit parameters awaited
Hello Test 4 2023-185xx						in space
1p PocketQube from Turkish company Hello Space equipped as part of a planned constellation of Internet comsats.
Orbit parameters awaited
ISL 48 2023-185xx						in space
Small satellite from Space BD, purpose not known.
Orbit parameters awaited
Name awaited 2023-185xx						in space
2p PocketQube from Alba orbital - name and purpose not disclosed.
Orbit parameters awaited
Unicorn-2L 2023-185xx						in space
2p PocketQube satellite. Mission details to follow.
Orbit parameters awaited
Unicorn-2M 2023-185xx						in space
2p PocketQube satellite. Mission details to follow.
Orbit parameters awaited
unidentified satellite 2023-185xx						in space
Details awaited
Orbit parameters awaited
unidentified satellite 2023-185xx						in space
Details awaited
Orbit parameters awaited
unidentified satellite 2023-185xx						in space
Details awaited
Orbit parameters awaited
unidentified satellite 2023-185xx						in space
Details awaited
Orbit parameters awaited
unidentified satellite 2023-185xx						in space
Details awaited
Orbit parameters awaited
unidentified satellite 2023-185xx						in space
Details awaited
Orbit parameters awaited
Falcon 9 second stage uncatalogued						Re-entered - 2023 Dec 1 Life <1 day
Carried South Korea's first project 425 satellite and 24 other payloads. Caused to re-enter, still carrying three satellites that failed to separate from it, above southern Pacific Ocean around 20:00 UTC.
Not Catalogued - orbit parameters unavailable

2023-186 Falcon 9 Block 5 (Starlink Group 06-31) Cape Canaveral Space Force Station						2023 Dec 3, 04:00
Starlink 30947 2023-186A 58473						in space
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:06 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 11, 18:00	6700	0.0002	320	323	90.96	43.00	275
Falcon 9 second stage uncatalogued						Re-entered - 2023 Dec 3 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-187 CZ 2C Jiuquan Space Centre						2023 Dec 4, 04:10
Xingchi 1-02A 2023-187A 58496						in space
Remote sensing - equipped with a multispectral Earth imaging system. Also carries a laser communication system. Part of a planned 100 satellite constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 4, 10:07	7013	0.0011	627	642	97.41	98.01	272	10:30
MisrSat 2 2023-187B 58497						in space
Egyptian high resolution remote sensing satellite. The payload was developed and assembled in Egypt, and integrated into the satellite body by China.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 4, 10:07	7013	0.0011	627	643	97.41	98.01	266	10:30
2023 Dec 8, 09:58	7013	0.0011	627	643	97.42	98.01	255	10:30
Xingchi 1-02B 2023-187C 58498						in space
Remote sensing - equipped with a multispectral Earth imaging system. Also carries a laser communication system. Part of a planned 100 satellite constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 4, 10:07	7013	0.0011	627	642	97.41	98.00	267	10:30
CZ 2C second stage 2023-187D 58499						in space
Launched MisrSat 2 and pair of Xingchi satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 4, 10:05	6987	0.0039	582	637	96.88	98.14	356

2023-188 TLV (Test Launch vehicle) Maritime launch platform, Jeju Island, South Korea						2023 Dec 4, 05:00
S-STEP 1 (Small SAR Technology Experimental Project) 2023-188A 58500						in space
Small satellite from Hanwha Systems of South Korea, equipped with an Earth imaging radar. The design is a flat panel incorporating solar cells on one side and an SAR panel on the other. Carried on test flight of new launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 4, 09:43	7023	0.0012	636	653	97.62	46.98	331
TLV fourth stage 2023-188B 58501						in space
Launched S-STEP 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 4, 10:59	6916	0.0166	424	653	95.41	46.92	7

2023-189 Ceres 1 (Gushenxing 1 Y-9, We won't stop!) Jiuquan Space Centre						2023 Dec 4, 23:33
Tianyan 16 2023-189A 58502						in space
Small satellite equipped with a remote sensing payload. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 5, 04:01	6882	0.0012	495	512	94.69	97.46	286	05:52
Xingchi 1-01A 2023-189B 58503						in space
Remote sensing - equipped with a multispectral Earth imaging system. Also carries a laser communication system. Part of a planned 100 satellite constellation. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 5, 05:23	6881	0.0013	494	511	94.67	97.47	291	05:52
Ceres 1 fourth stage 2023-189C 58504						Re-entered - 2024 Sep 30 Life 301 days
Launched Tianyian 16 and Xinchi 1-01A.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 5, 04:17	6878	0.0016	489	511	94.62	97.46	308

2023-190 Jielong 3 (Y1) Mobile floating platform, South China Sea near 21°.5 N, 112°.0 E						2023 Dec 5, 19:24
Hulianwang Jishu Shiyan 6 (Internet Connectivity Test Satellite 6) 2023-190A 58505						in space
Test satellite for Chinese government communications system for use by Internet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 5, 22:14	7291	0.0012	904	922	103.26	86.49	300
Jielong 3 fourth stage 2023-190B 58506						in space
Launched Internet Technology Test satellite. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 5, 22:24	7019	0.0400	360	921	97.54	86.58	15

2023-191 Falcon 9 Block 5 (Starlink Group 06-33) Cape Canaveral Space Force Station						2023 Dec 7, 05:07
Starlink 31026 2023-191A 58508						in space
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:12 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 14, 20:00	6699	0.0002	319	322	90.94	43.00	271
Falcon 9 second stage uncatalogued						Re-entered - 2023 Dec 7 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-192 Falcon 9 Block 5 (Starlink Group 07-08) Vandenberg Space Force Base						2023 Dec 8, 08:03
Starlink 31012 2023-192A 58531						in space
One member of a simultaneously-launched cluster of twenty two V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 09:06 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 15, 05:14	6691	0.0001	312	313	90.77	53.16	142
Falcon 9 second stage uncatalogued						Re-entered - 2023 Dec 8 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-193 Zhuque-2 (Y3) Jiuquan Space Centre						2023 Dec 8, 23:39
Honghu 1 2023-193A 58553						Re-entered - 2025 May 6 Life 515 days
Demonstrator satellite for systems to be used in satellites for an LEO communications network.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 9, 05:40	6825	0.0021	433	461	93.53	97.26	270	06:00
2025 Jan 29, 13:40	6730	0.0012	344	360	91.58	97.23	163	06:37
Honghu 2 2023-193B 58554						Re-entered - 2025 Mar 4 Life 452 days
Demonstrator satellite for systems to be used in satellites for an LEO communications network.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 9, 05:22	6826	0.0020	433	461	93.53	97.26	270	06:00
2024 Feb 6, 04:22	6839	0.0011	453	469	93.81	97.26	59	06:01
2025 Jan 29, 14:17	6694	0.0005	312	319	90.84	97.23	143	06:30
Tianyi 33 2023-193C 58555						in space
Demonstrator satellite for future space systems.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 9, 05:56	6826	0.0020	433	461	93.53	97.26	270	06:00
2024 Jan 21, 23:31	6867	0.0028	470	508	94.39	97.26	111	06:00
2024 Mar 14, 02:33	6828	0.0028	431	470	93.59	97.26	294	05:58
2024 May 7, 12:45	6930	0.0035	527	576	95.68	97.26	101	05:53
2024 Jul 27, 22:53	6822	0.0035	420	468	93.46	97.25	182	05:44
2024 Sep 10, 01:26	6914	0.0036	511	560	95.35	97.26	31	05:41
2024 Dec 18, 15:12	6830	0.0041	424	480	93.62	97.26	42	05:33
2025 Jan 29, 13:37	6902	0.0036	499	549	95.11	97.26	249	05:31
Zhuque 2 second stage 2023-193D 58556						Re-entered - 2025 Feb 2 Life 422 days
Launched cluster of three satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 9, 21:22	6819	0.0024	425	458	93.41	97.27	294

2023-194 CZ 2D Xichang Space Centre						2023 Dec 10, 01:58
Yaogan 39-05 Follower 1 2023-194A 58557						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-04 (2022-100) and Yaogan 36-05 (2023-106) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 10, 11:25	6875	0.0008	491	502	94.55	35.00	264
2023 Dec 22, 10:55	6878	0.0011	492	507	94.61	35.00	10
Yaogan 39-05 Leader 2023-194B 58558						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-04 (2022-100) and Yaogan 36-05 (2023-106) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 10, 11:25	6873	0.0008	489	500	94.50	35.00	281
2023 Dec 19, 14:08	6875	0.0004	494	500	94.56	34.99	52
2023 Dec 22, 08:09	6879	0.0002	500	502	94.63	34.99	287
Yaogan 39-05 Follower 2 2023-194C 58559						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the Yaogan 35-04 (2022-100) and Yaogan 36-05 (2023-106) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 10, 11:26	6874	0.0008	490	501	94.52	34.99	272
2023 Dec 20, 10:00	6875	0.0004	494	500	94.56	35.00	14
2023 Dec 22, 08:01	6879	0.0003	499	503	94.63	34.99	282
CZ 2D second stage 2023-194D 58561						Re-entered - 2024 Sep 24 Life 289 days
Launched Yaogan 39 Group 5.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 10, 11:23	6874	0.0008	490	502	94.54	35.00	265

2023-195 CZ 2F/G Jiuquan Space Centre						2023 Dec 14, 14:10
Reusable Spacecraft Test Vehicle Flight 3 2023-195A 58573						Re-entered - 2024 Sep 6 Life 267 days Returned to Earth
Small re-usable spaceplane designed for long duration missions. Launch time is an estimate and is ±1 minute. Released an unidentified companion object, probably 2024 May 24 and conducted rendezvous operations with it. Retro-fire 2024 Sep 6 led to a landing on the Lop Nor runway at about 01:05 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 14, 16:47	6718	0.0011	333	348	91.34	49.99	263
2024 Jan 5, 05:44	6715	0.0012	328	345	91.26	49.99	11
2024 Jan 5, 16:24	6724	0.0021	332	359	91.45	49.99	52
2024 Jan 19, 15:20	6720	0.0020	328	356	91.38	49.99	112
2024 Jan 20, 13:01	6844	0.0192	334	597	93.91	49.99	88
2024 Jan 27, 11:28	6984	0.0005	602	609	96.80	49.99	270
2024 Mar 28, 22:34	6983	0.0004	602	608	96.79	49.99	161
2024 May 25, 13:36	6983	0.0004	602	608	96.79	49.99	24
2024 May 25, 15:13	6984	0.0004	603	609	96.81	49.99	42
2024 Jun 5, 22:05	6975	0.0010	590	604	96.63	49.99	3
2024 Jun 7, 11:06	6983	0.0002	603	606	96.78	50.00	109
2024 Jul 18, 16:47	6983	0.0005	601	608	96.78	50.00	232
2024 Jul 19, 12:44	6723	0.0008	339	350	91.43	49.99	254
2024 Sep 5, 21:51	6720	0.0001	341	343	91.37	49.98	55
unidentified satellite 2023-195G 59884						in space
Released from the spaceplane probably 2024 May 24. May be similar to a small satellite released from, and retrieved by, a spaceplane on the previous mission (2022-093) that conducted multiple rendezvous operations with it.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 May 26, 17:01	6983	0.0004	602	607	96.79	49.99	28
2025 Jan 16, 14:11	6977	0.0004	596	602	96.67	49.99	219
CZ 2F third stage 2023-195B 58574						Re-entered - 2024 Mar 10 Life 87 days
Launched experimental spaceplane.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 14, 16:47	6717	0.0014	329	348	91.30	49.99	293

2023-196 Electron (The Moon God Awakens) Rocket Lab Launch Complex, New Zealand						2023 Dec 15, 04:05
QPS-SAR 5 (Tsukuyomi-I) 2023-196A 58578						in space
Commercial satellite from Japanese company iQPS, equipped with an Earth imaging radar. Second satellite in a constellation that will ultimately consist of 36 satellites. Released from launch vehicle at 05:03 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 15, 06:45	6957	0.0006	574	583	96.24	42.02	275
Electron third stage (kick stage) 2023-196B 58579						in space
Launched QPS-SAR 5 (Tsukuyomi-I).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 15, 06:33	6958	0.0003	578	582	96.27	42.01	222
Electron second stage 2023-196C 58580						Re-entered - 2024 Jan 12 Life 28 days
Launched QPS-SAR 5 (Tsukuyomi-I).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 15, 06:24	6782	0.0251	234	574	92.64	42.01	261

2023-197 CZ 5 (Y6) Wenchang Space Centre						2023 Dec 15, 13:41
Yaogan 41 2023-197A 58582						in space
High resolution Earth imaging from GEO. Probably moved from transfer orbit to GEO drift orbit December 16 at around 06:00 UTC then arrived on location around December 26.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Dec 27, 16:23	42163	0.0013	35732	35839	1436.03	4.98	174	123°.2 E
CZ 5 second stage 2023-197B 58583						in space
Launched Yaogan 41.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 15, 16:38	23524	0.7211	182	34109	598.44	19.48	179
2023 Dec 20, 08:55	23575	0.7173	287	34106	600.39	19.11	182

2023-198 Soyuz-2.1b + Fregat Baikonur Cosmodrome						2023 Dec 16, 09:17
Arktika-M 2 2023-198A 58584						in space
Meteorological imaging satellite that also provides communication links for messaging systems and communication links for research stations in Arctic regions. Also carries COSPAS-SARSAT search and rescue receivers. Design based on the Elektro-L geosynchronous orbit meteorological satellite. Separated from the Fregat stage at 14:01 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 17, 10:53	26776	0.7050	1520	39276	726.76	63.30	270
2023 Dec 26, 00:27	26710	0.7089	1397	39267	724.06	63.26	270
2024 Jan 7, 23:33	26563	0.7066	1416	38955	718.09	63.29	270
Fregat rocket stage 2023-198B 58585						in space
Launched Arktika-M 2. First listed orbit was before release of the satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 16, 13:40	26127	0.7460	257	39241	700.48	62.78	269
2023 Dec 16, 16:50	26689	0.7101	1359	39264	723.22	63.29	270

2023-199 Hyperbola 1 (Y7) Jiuquan Space Centre						2023 Dec 17, 07:00
Dier 1 (Liangxi) 2023-199A 58586						in space
Two part satellite developed by Beijing Ziwei Yutong Technology Co to carry a range of on-orbit payloads. This version is a demonstrator for the company's planned B300 satellite and carries an Earth observation system as well as several life sciences experiments. The latter will later be returned to Earth in the Dier 1 re-entry module.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 17, 11:33	6876	0.0010	491	505	94.57	97.40	257	13:20
Hyperbola 1 fourth stage 2023-199B 58587						Re-entered - 2024 Apr 7 Life 112 days
Perigee lowered after releasing satellites. Orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 17, 11:25	6763	0.0171	269	500	92.25	97.69	10

2023-I09 JEM Small Satellite Orbital Deployer International Space Station						2023 Dec 18, 08:35
BEAK (complicated acronym based on an acronym) 1998-067WD 58612						Re-entered - 2024 Jun 28 Life 193 days
3U Cubesat from the University of Tokyo in Kashiwa and the Institute of Space and Astronautical Science, Japan reportedly carrying an aerobraking device.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 19, 10:44	6791	0.0003	411	415	92.82	51.64	320

2023-I10 JEM Small Satellite Orbital Deployer International Space Station						2023 Dec 18, 10:15
Clarke sat-1 1998-067WE 58613						Re-entered - 2024 Apr 23 Life 127 days
1U Cubesat from the Clark Memorial International High School of Japan, equipped with an Earth imaging system and an amateur radio package.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 19, 10:44	6791	0.0005	410	417	92.83	51.64	356

2023-200 Falcon 9 Block 5 (Starlink Group 06-34) Cape Canaveral Space Force Station						2023 Dec 19, 04:01
Starlink 31044 2023-200A 58589						in space
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:06 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 27, 16:00	6696	0.0002	317	319	90.89	43.00	273
Falcon 9 second stage uncatalogued						in space
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-201 Soyuz-2.1a Plesetsk Cosmodrome						2023 Dec 21, 08:48
Cosmos 2573 (Bars-M №5) 2023-201A 58614						in space
Russian government optical imaging satellite for use in cartography. Initial orbit co-planar with Cosmos 2556/Bars-M №3 (2022-054A. At the time of launch, Russian news media reported that the launch vehicle was Soyuz-2 1B which was inconsistent with earlier Bars-M missions.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 21, 10:38	6797	0.0118	338	499	92.94	97.57	72	00:31
2023 Dec 22, 20:37	6799	0.0115	343	499	92.99	97.56	69	00:31
2023 Dec 23, 15:25	6810	0.0098	365	498	93.21	97.56	65	00:31
2023 Dec 25, 12:23	6831	0.0066	408	498	93.65	97.56	57	00:31
2023 Dec 29, 02:40	6881	0.0010	495	510	94.67	97.56	283	00:32
2024 Feb 5, 21:31	6880	0.0014	492	511	94.64	97.56	135	00:35
2024 Oct 31, 03:51	6866	0.0010	482	495	94.37	97.57	279	00:58
Soyuz third stage 2023-201B 58615						Re-entered - 2024 Jul 15 Life 207 days
Launched Cosmos 2573.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 21, 10:38	6796	0.0118	338	498	92.92	97.55	72

2023-202 Firefly Alpha (FLTA004, Fly the Lightning ) Vandenberg Space Force Base						2023 Dec 22, 17:32
Tantrum 2023-202A 58616						Re-entered - 2024 Feb 10 Life 50 days
Small satellite from Lockheed Martin carrying a demonstrator payload consisting of an Electronically Steered Antenna (ESA). Launch itself was used to demonstrate rapid assembly and launch with the satellite being delivered to the pad and the rocket being made ready for lift off within 24 hours of the order being issued. Orbit was intended to be circular at 520 km but second, apogee firing, of upper stage did not occur.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 22, 21:42	6748	0.0227	216	523	91.94	140.02	153
Firefly Alpha upper stage 2023-202B 58617						Re-entered - 2024 Jan 19 Life 28 days
Launched payload for Lockheed Martin.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 22, 21:42	6747	0.0229	214	523	91.92	140.02	153

2023-203 Falcon 9 Block 5 (Starlink Group 06-32) Cape Canaveral Space Force Station						2023 Dec 23, 05:33
Starlink 31119 2023-203A 58618						Re-entered - 2023 Dec 26 Life 3 days
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:38 UTC. Failed to activate at the start of the mission and re-entered soon after launch. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 26, 08:00	6578	0.0020	187	213	88.49	43.00	195
Falcon 9 second stage uncatalogued						Re-entered - 2023 Dec 23 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-204 Falcon 9 Block 5 Vandenberg Space Force Base						2023 Dec 23, 13:11
SARah 2 2023-204A 58643						in space
One of a simultaneously-launched pair of German military satellites carrying an imaging radar system. Released from launch vehicle at around 13:36 UTC and reportedly aimed at sun-synchronous orbit with LTDN around 04:50 in order to fly in formation with the existing SARah 1 (52887, 2022-063A). Orbital elements classified as 'secret'. Mid 2024, it was reported that a design defect had prevented the SAR aerial from unfurling on both SARah 2 and SARah 3, preventing both satellites from becoming operational. Orbital elements are classified 'secret' so orbit information comes from amateur observers, with exception of the first one listed that was inadvertently published by Space-Track. The inclination does not place them in the reported formation with SARah 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 Oct 22, 06:49	6883	0.0009	498	510	94.71	88.19	43
2025 Feb 14, 18:57	6876	0.0009	492	504	94.57	88.21	324
SARah 3 2023-204B 58644						in space
One of a simultaneously-launched pair of German military satellites carrying an imaging radar system. Released from launch vehicle at around 13:36 UTC and reportedly aimed at sun-synchronous orbit with LTDN around 04:50 in order to fly in formation with the existing SARah 1 (52887, 2022-063A). Orbital elements classified as 'secret'. Mid 2024, it was reported that a design defect had prevented the SAR aerial from unfurling on both SARah 2 and SARah 3, preventing both satellites from becoming operational. Orbital elements are classified 'secret' so orbit information comes from amateur observers, with exception of the first one listed that was inadvertently published by Space-Track. The inclination does not place them in the reported formation with SARah 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 Oct 23, 04:33	6882	0.0008	499	510	94.70	88.20	37
2025 Feb 13, 20:27	6876	0.0006	494	502	94.57	88.21	305
Falcon 9 second stage uncatalogued						in space
Launched SARah 2 & SARah 3. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-205 Kuaizhou 1A Jiuquan Space Centre						2023 Dec 25, 01:00
Tianmu 1-11 2023-205A 58645						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 25, 07:14	6901	0.0010	516	530	95.09	97.42	271	07:21
Tianmu 1-12 2023-205B 58646						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 25, 07:14	6902	0.0010	517	531	95.11	97.42	265	07:21
Tianmu 1-13 2023-205C 58647						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 25, 07:14	6903	0.0012	517	533	95.12	97.42	263	07:21
Tianmu 1-14 2023-205D 58648						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 25, 07:05	6902	0.0011	516	532	95.11	97.41	267	07:21
Kuaizhou 1A third stage 2023-205E 58649						Re-entered - 2024 Feb 14 Life 51 days
Launched Tianmu 1-11 - Tianmu 1-14. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 25, 07:13	6764	0.0229	231	541	92.28	97.42	37

2023-206 CZ 11H Mobile floating platform, South China Sea near 21°.5 N, 112°.0 E						2023 Dec 25, 22:39
Shiyan 24C-01 (Test 24C-01) 2023-206A 58650						in space
Small satellite carrying an unspecified demonstration payload, one of three carried on the same launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 26, 03:01	6927	0.0009	542	555	95.62	97.33	287	05:59
2024 Jan 7, 03:20	6925	0.0010	540	554	95.58	97.34	225	05:57
Shiyan 24C-02 (Test 24C-02) 2023-206B 58651						in space
Small satellite carrying an unspecified demonstration payload, one of three carried on the same launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 26, 02:57	6925	0.0009	541	553	95.59	97.34	300	05:59
2024 Jan 7, 03:19	6925	0.0009	541	553	95.58	97.34	250	05:57
Shiyan 24C-03 (Test 24C-03) 2023-206C 58652						in space
Small satellite carrying an unspecified demonstration payload, one of three carried on the same launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 26, 03:01	6925	0.0011	540	554	95.59	97.33	294	05:59
2024 Jan 7, 03:20	6925	0.0010	540	554	95.59	97.33	247	05:57
CZ 11 fourth stage 2023-206D 58653						Re-entered - 2024 Jan 18 Life 24 days
Launched Shiyan 24C group. Perigee lowered after releasing the satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 26, 01:28	6776	0.0336	170	626	92.52	97.19	338

2023-207 CZ 3B + YZ-1 Xichang Space Centre						2023 Dec 26, 03:26
Beidou 57 (Beidou-3 M-28) 2023-207A 58654						in space
Phase 2 operational satellite in China's navigation satellite system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 26, 10:24	28240	0.0117	21532	22193	787.16	54.97	178
2024 Jan 19, 12:00	27906	0.0004	21518	21538	773.23	55.00	253
Beidou 58 (Beidou-3 M-26) 2023-207B 58655						in space
Phase 2 operational satellite in China's navigation satellite system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 26, 10:24	28234	0.0119	21520	22191	786.90	55.00	178
2024 Jan 5, 20:19	27969	0.0317	20705	22476	775.83	54.65	69
2024 Jan 23, 20:21	27906	0.0005	21515	21541	773.23	54.99	245
YZ-1 rocket stage 2023-207C 58656						in space
Launched Beidou 57 & Beidou 58. Apogee raised after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 26, 10:16	28643	0.0026	22191	22339	804.05	54.96	351
CZ 3B fourth stage 2023-207D 58657						in space
Launched Beidou 57 & Beidou 58.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 26, 10:05	15721	0.5814	202	18483	326.94	54.95	170

2023-208 Kuaizhou 1A Jiuquan Space Centre						2023 Dec 27, 06:50
Tianmu 1-19 2023-208A 58660						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 27, 13:03	6904	0.0012	517	534	95.15	97.41	268	13:11
Tianmu 1-20 2023-208B 58661						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 27, 13:04	6902	0.0010	517	531	95.12	97.40	264	13:11
Tianmu 1-21 2023-208C 58662						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 27, 12:55	6902	0.0010	517	531	95.12	97.39	265	13:11
Tianmu 1-22 2023-208D 58663						in space
Small meteorological satellite using occultation by the Earth's atmosphere of navsat signals to take weather-related measurements.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 27, 13:03	6901	0.0009	517	530	95.09	97.40	260	13:11
Kuaizhou 1A third stage 2023-208E 58664						Re-entered - 2024 Jan 4 Life 8 days
Launched Tianmu 1-19 - Tianmu 1-22. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 27, 12:59	6730	0.0288	158	546	91.58	97.37	40

2023-209 Soyuz-2.1v Plesetsk Cosmodrome						2023 Dec 27, 07:03
Cosmos 2574 2023-209A 58658						in space
Russian military satellite - mission details awaited. Orbit lowered by about 2.5 km after a series of thruster firings 2024 January 25 - January 29.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2023 Dec 27, 16:25	6733	0.0008	349	360	91.63	96.76	46	22:40
2024 Jan 25, 08:57	6728	0.0004	347	353	91.54	96.75	285	22:38
2024 Jan 26, 18:51	6727	0.0004	346	351	91.51	96.75	273	22:38
2024 Jan 28, 01:31	6726	0.0004	345	350	91.49	96.75	261	22:37
2024 Feb 8, 19:18	6724	0.0008	341	351	91.46	96.76	178	22:37
2024 Feb 22, 14:09	6719	0.0008	335	346	91.35	96.75	145	22:36
2024 Oct 31, 17:34	6673	0.0004	292	297	90.41	96.69	147	22:38
2025 Feb 28, 03:05	6703	0.0006	321	329	91.03	96.68	100	22:36
Soyuz third stage 2023-209B 58659						Re-entered - 2024 May 3 Life 128 days
Launched Cosmos 2574.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 27, 11:43	6731	0.0006	349	357	91.60	96.77	43
Debris item 2023-209C 59022						Re-entered - 2024 Mar 5 Life 69 days
Separated from Cosmos 2574, probably on February 22. Rapid orbit decay indicates it is a low density item - either a fabric cover from an external device or something that broke away.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 Feb 24, 18:08	6710	0.0011	325	339	91.17	96.74	128
2024 Mar 4, 23:29	6568	0.0013	181	198	88.28	96.78	177

2023-210 Falcon 9 Heavy Kennedy Space Center						2023 Dec 29, 01:07
USA 349 (OTV-7, X-37B#2 Flight 4) 2023-210A 58666						Re-entered - 2025 Mar 7 Life 434 days Returned to Earth
Flight of USAF/Boeing X-37B space plane. Mission not disclosed but it carries sensors to study/monitor other satellites in orbit and a NASA materials science payload to expose materials to the space environment. Initially located on orbit by amateur visual observer Tomi Simola 2024 February then tracked by the amateur community. 2024 mid-October, perigee of its elliptical orbit was lowered to create significant drag in order to reduce apogee to a few hundred kilometres and conduct its ongoing mission in LEO. Landed on the runway at Vandenberg SFB 2025 March 7 at 07:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 Feb 9, 17:00	25959	0.7418	323	38838	693.73	59.12	167
2024 Feb 13, 03:45	25822	0.7421	282	38606	688.24	59.10	168
2024 Mar 7, 18:44	25494	0.7366	337	37895	675.18	59.27	169
2024 Oct 4, 18:07	24334	0.7277	248	35664	629.63	58.98	183
2024 Nov 2, 20:15	21474	0.6983	100	30092	521.95	58.01	169
Falcon 9 upper stage uncatalogued						Re-entered - 2023 Dec 29 Life <1 day
Launched USA 349. Caused to re-enter near 42° north, 144° west at about 13:00 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable

2023-211 Falcon 9 Block 5 (Starlink Group 06-36) Cape Canaveral Space Force Station						2023 Dec 29, 04:01
Starlink 31130 2023-211A 58667						Re-entered - 2024 Jan 4 Life 6 days
One member of a simultaneously-launched cluster of twenty three V2 Mini LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:07 UTC. This particular satellite re-entered following a de-orbit routine, probably initiated when its comms payload failed to activate. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2024 Jan 2, 15:19	6633	0.0010	248	262	89.60	43.00	240
2024 Jan 4, 11:03	6566	0.0005	185	191	88.25	43.00	248
Falcon 9 second stage uncatalogued						Re-entered - 2023 Dec 29 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2023-212 CZ 2C + YZ-1S Jiuquan Space Centre						2023 Dec 30, 00:13
Hulianwang Jishu Shiyan 7 (Internet Connectivity Test Satellite 7) 2023-212A 58691						in space
Test satellite for Chinese government communications system for use by Internet-connected devices. One of three carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 30, 05:03	7314	0.0007	931	941	103.75	50.00	305
2024 Jan 4, 11:43	7317	0.0007	934	945	103.82	50.01	320
2024 Mar 12, 06:14	7317	0.0008	933	945	103.82	50.00	187
2024 Apr 9, 19:19	7457	0.0001	1078	1079	106.81	50.01	268
2024 Apr 27, 23:33	7481	0.0000	1103	1103	107.33	50.00	60
Hulianwang Jishu Shiyan 8 (Internet Connectivity Test Satellite 8) 2023-212B 58692						in space
Test satellite for Chinese government communications system for use by Internet-connected devices. One of three carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 30, 05:03	7311	0.0005	930	937	103.70	50.00	283
2024 Jan 10, 04:08	7317	0.0007	934	944	103.81	49.99	338
2024 Mar 12, 06:07	7317	0.0005	936	943	103.82	50.00	176
2024 Apr 13, 12:31	7482	0.0000	1104	1104	107.35	50.00	223
Hulianwang Jishu Shiyan 9 (Internet Connectivity Test Satellite 9) 2023-212C 58693						in space
Test satellite for Chinese government communications system for use by Internet-connected devices. One of three carried on the same launch vehicle. Commenced orbit raising 2024 March 12 simultaneously with the other two satellites from the launch. It tracked closely 2023-212B and reached steady height 2024 April 12 simultaneously with it.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Dec 30, 05:03	7313	0.0007	930	940	103.73	50.00	285
2024 Jan 9, 10:17	7317	0.0007	934	944	103.82	50.00	320
2024 Mar 12, 06:09	7317	0.0007	934	944	103.82	50.00	170
2024 Apr 13, 00:46	7482	0.0000	1104	1104	107.35	50.00	244
YZ-1S rocket stage uncatalogued						Re-entered - 2023 Dec 30 Life <1 day
Launched three Internet Connectivity Test Satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable