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=2025#001

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

2025-001 Falcon 9 Block 5 Cape Canaveral Space Force Station						2025 Jan 4, 01:27
Thuraya 4 2025-001A 62483						in space
Comsat from the Al Yah Satellite Communications Company of the UAE to provide broadband and other data communications links across Africa, Europe, Central Asia and the Middle East. Separated from launch vehicle at 02:02 UTC. Continuously operating low thrust used to reach operational orbit. Expected location 44° east to replace Thuraya 2 (27825, 2003-026A).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Jan 5, 00:37	33644	0.7977	429	54103	1023.57	26.91	178
2025 Jan 12, 08:04	35003	0.7806	1301	55949	1086.24	24.51	181
2025 Jan 21, 18:00	36130	0.7658	2082	57421	1139.08	20.40	182
2025 Jan 29, 13:50	37689	0.7409	3385	59236	1213.60	17.14	184
2025 Feb 5, 10:58	38998	0.7172	4652	60588	1277.40	14.64	185
2025 Feb 11, 18:22	39974	0.6915	5953	61238	1325.62	12.65	187
2025 Feb 18, 07:07	40883	0.6586	7577	61432	1371.10	10.71	188
2025 Feb 25, 00:36	41578	0.6191	9460	60940	1406.22	8.93	189
2025 Mar 5, 21:32	42156	0.5684	11815	59740	1435.63	7.23	191	163°.8 E
2025 Mar 12, 00:00	42576	0.5276	13735	58659	1457.14	6.49	192
2025 Mar 19, 03:07	41639	0.4986	14498	56023	1409.31	5.03	192
2025 Mar 26, 09:29	40700	0.4676	15290	53354	1361.91	4.06	191
2025 Apr 2, 07:21	43408	0.3630	21274	52785	1500.07	3.30	195
2025 Apr 9, 18:37	43479	0.2996	24073	50128	1503.74	2.57	196
2025 Apr 16, 02:32	44114	0.2513	26651	48819	1536.80	2.02	199
2025 Apr 24, 11:59	45061	0.1863	30290	47076	1586.59	1.36	207
2025 May 1, 13:09	43038	0.1073	32043	41277	1480.93	0.84	199
2025 May 7, 00:54	43087	0.0537	34395	39022	1483.45	0.47	211
Falcon 9 second stage 2025-001B 62484						in space
Launched Thuraya 4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 6, 13:41	33491	0.7972	414	53811	1016.59	26.84	178

2025-002 CZ 3B Xichang Space Centre						2025 Jan 6, 20:00
Shijian 25 (Practice 25) 2025-002A 62485						in space
Verification mission for a satellite refuelling and life extension system, aimed to link up with a satellite already in geosynchronous orbit. Arrived alongside TJS 11 (59020. 2024-037A) on Jan 14, possibly to conduct station-keeping tests but its eventual target seems to be Shijian 21 (49330, 2021-094A) - the two orbits are co-planar.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Jan 7, 11:32	24388	0.7310	182	35838	631.73	28.48	180
2025 Jan 13, 19:03	42195	0.0064	35546	36088	1437.64	10.21	189	120°.1 E
2025 Jan 14, 15:16	42166	0.0059	35540	36036	1436.17	10.21	185	120°.0 E
2025 Jan 16, 08:07	42169	0.0058	35547	36034	1436.30	10.21	185	119°.9 E
2025 Jan 16, 18:20	42162	0.0057	35545	36022	1435.94	10.21	184	119°.9 E
2025 Mar 27, 20:57	42163	0.0059	35535	36034	1435.98	10.35	183	119°.8 E
CZ 3B fourth stage 2025-002B 62486						in space
Launched Shijian 25.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 7, 01:00	24839	0.7372	151	36772	649.33	28.46	180

2025-003 Falcon 9 Block 5 (Starlink Group 06-71) Cape Canaveral Space Force Station						2025 Jan 6, 20:43
Starlink 32713 2025-003A 62487						in space
One member of a simultaneously-launched cluster of twenty four broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 21:48 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   ( ° )
2025 Jan 14, 16:00	6680	0.0002	301	303	90.56	43.00	282
Falcon 9 second stage uncatalogued						Re-entered - 2025 Jan 6 Life <1 day
Launched twenty four Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-004 Falcon 9 Block 5 (Starlink Group 12-11) Kennedy Space Center						2025 Jan 8, 15:27
Starlink 11452 2025-004A 62511						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 16:32 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   ( ° )
2025 Jan 9, 03:44	6675	0.0003	295	299	90.47	43.01	252
Falcon 9 second stage uncatalogued						Re-entered - 2025 Jan 8 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-005 Falcon 9 Block 5 (NRO L-153) Vandenberg Space Force Base						2025 Jan 10, 03:53
USA 463 (Starshield 0073) 2025-005A 62532						in space
One of a simultaneously-launched group of twenty two US government NRO imaging reconnaissance satellites. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. All satellites were launched to a similar altitude at about 70° inclination.
Orbit classified as 'Secret' - data withheld
Falcon 9 second stage uncatalogued						Re-entered - 2025 Jan 10 Life <1 day
Launched twenty two Starshield satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-006 Falcon 9 Block 5 (Starlink Group 12-12) Cape Canaveral Space Force Station						2025 Jan 10, 19:11
Starlink 11538 2025-006A 62554						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 20:16 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   ( ° )
2025 Jan 17, 18:00	6692	0.0002	313	315	90.80	43.01	277
Falcon 9 second stage uncatalogued						Re-entered - 2025 Jan 10 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-007 Jielong 3 (Y5) Mobile floating platform, Yellow Sea - 36°.6 N, 121°.2 E						2025 Jan 13, 03:00
Wei Li Kongjiang 01-07 (Centispace 01-07) 2025-007B 62576						in space
One of ten simultaneously launched satellites for a 190 satellite constellation of an LEO navigation enhancement system from Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Also carries a demonstrator for an inter-satellite laser communication system. All ten satellites were launched into similar orbits
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 13, 11:01	7021	0.0013	634	652	97.59	54.98	297
Jielong 3 fourth stage 2025-007M 62586						Re-entered - 2025 Feb 27 Life 45 days
Launched Wei Li Kongjiang 01 cluster of ten satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 13, 10:45	6813	0.0321	216	654	93.28	54.94	359

2025-008 Falcon 9 Block 5 (Starlink Group 12-04) Cape Canaveral Space Force Station						2025 Jan 13, 16:47
Starlink 11547 2025-008A 62587						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 17:52 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   ( ° )
2025 Jan 17, 20:00	6676	0.0002	296	299	90.47	43.01	279
Falcon 9 second stage uncatalogued						Re-entered - 2025 Jan 13 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-009 Falcon 9 Block 5 (Transporter 12) Vandenberg Space Force Base						2025 Jan 14, 19:09
Satellites						in space
Payload list to follow.

2025-010 Falcon 9 Block 5 Kennedy Space Center						2025 Jan 15, 06:11
Blue Ghost 2025-010A 62716						in space
Lunar lander from US company Firefly, carrying ten experiments for NASA under its Commercial Lunar Payload Services programme. Separated from launch vehicle at 07:16 UTC. Trans-lunar injection occurred February 8, at the third apogee of its initial barycentric orbit (similar to 62719, 2025-010D). Arrival in orbit around the Moon February 14 followed a 255 seconds thruster firing commencing at 01:51 UTC. Three further thruster firings resulted in a 20 x100 kilometre orbit. A thruster firing March 2 at 08:22 UTC set up the descent trajectory resulting in touchdown at 08:34 UTC (around lunar sunrise) in the Mare Crisium. Surface operations continued until March 16 and lunar sunset after which the solar cells ceased to provide power.
Landed on the Moon
Resilience 2025-010B 62717						in space
Lunar lander from Japanese company ispace. Carries Tenacious, a micro lunar rover and together they make up the Hakuto-R mission. Separated from launch vehicle at 07:43 UTC. Arrived in the vicinity of the Moon and entered orbit around it on May 6.
In orbit around the Moon
Falcon 9 second stage 2025-010D 62719						in space
Launched Resilience and Blue Ghost towards the Moon.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 15, 07:37	187730	0.9651	176	362529	13491.54	35.17	346

2025-011 New Glenn (NG-1) Cape Canaveral Space Force Station						2025 Jan 16, 07:03
New Glenn second stage 2025-011A 62720						in space
Rocket stage with attached New Glenn Pathfinder Payload equipped with instrumentation to monitor performance of the launch vehicle whilst on the launch pad and during its six hour test mission. The stage also carries US government Department of Defense sensors to evaluate a demonstrator version of Blue Origin's planned Blue Ring orbital payload carrier.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 16, 08:37	17210	0.4894	2409	19254	374.47	30.00	267

2025-012 CZ 2D Jiuquan Space Centre						2025 Jan 17, 04:07
Tianlu 1 (DA 01) 2025-012A 62725						in space
Small Chinese satellite for middle and upper atmosphere studies. 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
2025 Jan 17, 15:20	6901	0.0008	517	529	95.08	97.48	276	10:25
Lantan 1 (Blue Carbon 1) 2025-012B 62726						in space
Small Chinese satellites for ocean studies. 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
2025 Jan 17, 15:21	6901	0.0009	517	529	95.09	97.48	281	10:25
E01 2025-012C 62727						in space
Pakistani electro optical remote sensing satellite for Earth studies to support agriculture, urban planning, environmental management, disaster management, and monitoring, deforestation, glacier recession and water resources. 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
2025 Jan 17, 15:23	6901	0.0009	517	530	95.09	97.49	270	10:25
CZ 2D second stage 2025-012D 62728						in space
Launched cluster of three satellites including Pakistan's EO1. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 17, 15:23	6902	0.0008	518	530	95.12	97.48	266

2025-013 Ceres 1 (Gushenxing 1 Y-16 ) Jiuquan Space Centre						2025 Jan 20, 10:11
Jitianxing A-05 2025-013A 62729						in space
Earth imaging satellite from Jitian Xingzhou Space Technology of Suzhou, China. 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
2025 Jan 21, 00:37	6917	0.0014	529	548	95.41	97.61	282	16:29
Yunyao-1 37 2025-013B 62730						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. 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
2025 Jan 21, 00:38	6916	0.0014	528	548	95.41	97.60	284	16:29
2025 Feb 1, 12:48	6918	0.0013	531	549	95.45	97.61	254	16:30
2025 Feb 2, 14:16	6920	0.0013	533	551	95.48	97.61	256	16:30
2025 Feb 3, 12:34	6921	0.0013	534	552	95.51	97.61	258	16:30
2025 Feb 4, 12:27	6922	0.0013	535	553	95.52	97.61	259	16:30
2025 Feb 6, 17:02	6924	0.0014	536	556	95.57	97.61	258	16:30
Yunyao-1 38 2025-013C 62731						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. 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
2025 Jan 21, 00:39	6916	0.0014	528	548	95.40	97.61	285	16:29
Yunyao-1 39 2025-013D 62732						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. 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
2025 Jan 21, 00:38	6916	0.0014	528	548	95.40	97.60	289	16:29
Yunyao-1 40 2025-013E 62733						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere. 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
2025 Jan 21, 05:06	6916	0.0014	528	547	95.39	97.61	284	16:29
2025 Feb 2, 14:13	6916	0.0013	529	547	95.40	97.61	244	16:30
Ceres 1 second stage uncatalogued						Re-entered - 2025 Jan 21 Life 1 day
Launched four Yunyao-1 satellites and Jitianxing A-05. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-014 Falcon 9 Block 5 (Starlink Group 13-01) Kennedy Space Center						2025 Jan 21, 05:24
Starlink 32806 2025-014A 62735						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle about 06:29 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   ( ° )
2025 Jan 24, 17:28	6692	0.0004	311	317	90.80	43.01	231
USA 485 (Starshield 0095) 2025-014X 62756						in space
One of a pair of government NRO imaging reconnaissance satellites, launched alongside 21 SpaceX starlink satellites. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Separated from launch vehicle at 06:29 UTC. Presence on launch vehicle undeclared prior to lift-off.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 24, 17:29	6689	0.0003	308	313	90.73	43.01	234
2025 Jan 29, 03:19	6696	0.0002	317	319	90.89	43.01	250
2025 Feb 1, 14:29	6691	0.0003	311	315	90.79	43.01	251
2025 Feb 11, 10:59	6723	0.0001	344	345	91.42	43.00	286
USA 486 (Starshield 0096) 2025-014Y 62757						in space
One of a pair of government NRO imaging reconnaissance satellites, launched alongside 21 SpaceX starlink satellites. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Separated from launch vehicle at 06:29 UTC. Presence on launch vehicle undeclared prior to lift-off.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 24, 17:29	6688	0.0002	309	312	90.73	43.01	253
2025 Jan 29, 03:18	6696	0.0001	317	318	90.88	43.01	251
2025 Feb 2, 08:36	6689	0.0003	310	313	90.75	43.01	249
2025 Feb 11, 14:00	6724	0.0002	344	347	91.45	43.00	213
2025 Feb 16, 12:43	6723	0.0002	343	346	91.43	43.00	255
Falcon 9 second stage uncatalogued						Re-entered - 2025 Jan 21 Life <1 day
Launched twenty one Starlink and two Starshield satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-015 Falcon 9 Block 5 (Starlink Group 11-08) Vandenberg Space Force Base						2025 Jan 21, 15:45
Starlink 33596 2025-015A 62758						in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 16:46 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   ( ° )
2025 Jan 24, 20:00	6647	0.0002	268	270	89.88	53.16	316
Falcon 9 second stage uncatalogued						Re-entered - 2025 Jan 21 Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-016 CZ 6A (Qianfan Ji Gui polar orbit group 6) Taiyuan Space Centre						2025 Jan 23, 05:15
Qianfan Ji Gui 06-01 2025-016A 62785						in space
One member of a simultaneously launched cluster of eighteen broadband distribution satellites for the Thousand Sails constellation. All satellites were injected into similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 5, 19:17	7182	0.0016	792	815	100.95	88.99	167
CZ 6A third stage 2025-016U 62803						in space
Launched eighteen Qianfan Ji Gui satellites. Perigee lowered after releasing satellites.
Orbit parameters awaited

2025-017 CZ 3B Xichang Space Centre						2025 Jan 23, 15:32
Tongxin Jishu Shiyan 14 (Communication Technology Test 14, TJS 14) 2025-017A 62804						in space
Satellite described as being mainly used for used for satellite communications, radio and television, data transmission, and other services, and carrying out related technical tests and verifications. Probably moved to Geosynchronous Drift Orbit January 24 at about 07:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Jan 23, 19:46	24376	0.7306	189	35807	631.27	28.48	180
2025 Feb 4, 14:52	42165	0.0002	35780	35794	1436.11	2.00	224	18°.3 E
CZ 3B fourth stage 2025-017B 62805						in space
Launched TJS 14.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 23, 17:24	23672	0.7249	135	34452	604.09	28.56	179

2025-018 Falcon 9 Block 5 (Starlink Group 11-06) Vandenberg Space Force Base						2025 Jan 24, 14:07
Starlink 32883 2025-018A 62806						in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:11 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   ( ° )
2025 Jan 30, 16:00	6669	0.0001	290	291	90.33	53.15	77
Falcon 9 second stage uncatalogued						Re-entered - 2025 Jan 24 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-019 Falcon 9 Block 5 (Starlink Group 12-07) Cape Canaveral Space Force Station						2025 Jan 27, 22:05
Starlink 11548 2025-019A 62829						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 23:10 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   ( ° )
2025 Feb 4, 20:00	6696	0.0002	317	319	90.89	43.00	266
Falcon 9 second stage uncatalogued						Re-entered - 2025 Jan 27 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-020 GSLV Mk II F15 Satish Dhawan Space Centre						2025 Jan 29, 00:53
NVS 02 (IRNSS 1K) 2025-020A 62850						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. Released from launch vehicle at 01:12 UTC. Intended to replace IRNSS 1E (41241, 2016-003A) at 111°.75 east but a stuck valve prevented propellant flow to its thrusters leading to it being stranded in geosynchronous transfer orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 29, 06:56	25267	0.7412	162	37615	666.16	20.75	178
GSLV Third Stage 2025-020B 62851						in space
Launched NVS 02.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 29, 06:54	25142	0.7398	164	37364	661.25	20.74	178

2025-021 Falcon 9 Block 5 Kennedy Space Center						2025 Jan 30, 01:34
Spainsat New Generation I 2025-021A 62852						in space
Military communications satellite built by a consortium led by Hisdesat for the Spanish Goverment. Released from launch vehicle at 02:05 UTC. Continuously operating low thrust used to reach operational orbit. Expected location - 29° east or 30° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 2, 09:48	40561	0.8320	437	67930	1354.97	26.85	178
2025 Feb 3, 08:24	40768	0.8286	610	68170	1365.35	26.11	178
2025 Feb 6, 04:55	41304	0.8234	917	68933	1392.32	24.72	179
2025 Feb 13, 01:32	42493	0.8071	1821	70409	1452.89	21.70	180
2025 Feb 20, 05:12	43510	0.7882	2836	71429	1505.39	18.61	181
2025 Feb 27, 13:56	44030	0.7638	4021	71283	1532.45	15.89	182
2025 Mar 7, 01:18	44242	0.7340	5389	70338	1543.50	13.36	184
2025 Mar 14, 13:23	44377	0.7032	6792	69206	1550.61	11.41	185
2025 Mar 21, 00:12	44474	0.6782	7936	68257	1555.69	9.91	186
2025 Mar 28, 13:10	44342	0.6566	8850	67079	1548.78	8.98	187
2025 Apr 3, 23:59	44301	0.6205	10434	65412	1546.62	7.60	188
2025 Apr 11, 12:36	44487	0.5801	12300	63918	1556.38	6.36	189
2025 Apr 18, 00:01	43478	0.5603	12738	61462	1503.72	5.48	189
2025 Apr 24, 12:02	43429	0.5100	14904	59199	1501.19	4.51	190
2025 May 2, 01:09	44079	0.4586	17487	57914	1534.98	3.78	192
2025 May 8, 12:17	44090	0.4107	19603	55821	1535.58	3.14	194
Falcon 9 second stage 2025-021B 62853
Launched Spainsat NG 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Jan 30, 23:21	39872	0.8335	262	66725	1320.57	26.93	177

2025-022 Falcon 9 Block 5 (Starlink Group 11-04) Vandenberg Space Force Base						2025 Feb 1, 23:02
Starlink 32868 2025-022A 62854						in space
One member of a simultaneously-launched cluster of twenty two broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle February 2 at 00:03 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   ( ° )
2025 Feb 10, 20:00	6697	0.0001	318	319	90.90	53.15	46
Falcon 9 second stage 2025-022Y 62878						Re-entered - 2025 Feb 19 Life 18 days
Engine firing intended to cause re-entry after releasing satellites did not occur.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 3, 10:47	6660	0.0012	274	290	90.15	53.17	248

2025-023 H-3 22S (F-5) Tanegashima Space Centre						2025 Feb 2, 08:30
Michibiki 6 (QZSS 6) 2025-023A 62876						in space
Quasi Zenith Satellite System satellite providing a timing and positioning service to improve navigational accuracy for users in Japan from a combination of equatorial GEO and inclined GEO, giving coverage to areas where the topography works against GPS reception. “Michibiki" translates into English as "Showing the Way". Separated from launch vehicle at 0859 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Feb 2, 10:49	24271	0.7212	390	35397	627.20	21.98	176
2025 Feb 3, 13:02	26371	0.5824	4634	35352	710.32	12.98	175
2025 Feb 5, 09:29	39739	0.0461	31527	35193	1313.95	0.56	170
2025 Feb 10, 20:47	42115	0.0012	35685	35790	1433.57	0.08	57	90°.3 E
2025 Feb 11, 20:31	42155	0.0003	35764	35790	1435.60	0.08	55	90°.4 E
2025 Feb 12, 14:28	42163	0.0001	35780	35791	1436.03	0.08	34	90°.4 E
2025 Feb 17, 22:43	42164	0.0001	35780	35792	1436.05	0.07	45	90°.5 E
H3 upper stage 2025-023B 62877						in space
Launched QZSS 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 2, 10:41	24245	0.7206	397	35336	626.15	21.97	175
2025 Feb 6, 01:55	24116	0.7251	251	35225	621.18	21.48	178

2025-024 Falcon 9 Block 5 (Starlink Group 12-03) Cape Canaveral Space Force Station						2025 Feb 4, 10:15
Starlink 11371 2025-024A 62879						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 11:20 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   ( ° )
2025 Feb 10, 20:00	6691	0.0001	312	314	90.78	43.00	265
Falcon 9 second stage uncatalogued						Re-entered - 2025 Feb 4 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-025 Falcon 9 Block 5 (Maxar 3) Kennedy Space Center						2025 Feb 4, 23:13
Worldview Legion 6 2025-025A 62900						in space
High resolution imaging satellite from Maxar Technologies of the US. Part of a constellation of six satellites providing images in response to customer demand. Separated from launch vehicle February 5 at 00:00 UTC. Space-Track has this tagged incorrectly as Legion 5.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 5, 01:09	7082	0.0006	700	709	98.86	45.04	97
Worldview Legion 5 2025-025B 62901						in space
High resolution imaging satellite from Maxar Technologies of the US. Part of a constellation of six satellites providing images in response to customer demand. Separated from launch vehicle February 5 at 01:03 UTC. Space-Track has this tagged incorrectly as Legion 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 5, 01:10	6828	0.0025	433	467	93.59	44.97	21
Falcon 9 second stage uncatalogued						Re-entered - 2025 Feb 4 Life <1 day
Launched pair of Worldview Legion satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-026 Soyuz-2.1v + Volga Plesetsk Cosmodrome						2025 Feb 5, 03:59
Cosmos 2581 2025-026A 62902						in space
Small, military, satellite - mission unknown but working together with Cosmos 2582. Released from Volga rocket stage mid-late morning on day of launch, at about 2000 km behind Cosmos 2582 and Cosmos 2583. Raised orbit slightly February 19.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 5, 18:17	6965	0.0011	579	594	96.41	81.99	275
2025 Feb 19, 13:30	6967	0.0011	581	596	96.45	82.00	207
Cosmos 2582 2025-026B 62903						in space
Small, military, satellite - mission unknown but working together with Cosmos 2581. Released from Volga rocket stage, together with Cosmos 2583, at about 04:30 UTC. Made rendezvous with Cosmos 2581 and moved to similar orbit February 24 probably around 21:00 UTC to begin station keeping.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 5, 11:47	6965	0.0015	576	597	96.41	81.99	260
2025 Feb 15, 12:57	6967	0.0014	580	599	96.47	81.99	219
2025 Feb 25, 12:39	6967	0.0011	581	596	96.45	82.00	187
2025 Apr 6, 22:26	6966	0.0012	579	596	96.43	82.00	64
2025 Apr 7, 14:31	6964	0.0013	576	595	96.39	82.00	54
2025 Apr 7, 17:44	6966	0.0013	579	597	96.43	82.00	55
Cosmos 2583 (payload 1) 2025-026C 62904						in space
Small, military, satellite - mission unknown. Released from Volga rocket stage, together with Cosmos 2582, at about 04:30 UTC. Made minor thruster firing on March 15 with no significant effect on the orbit. Separated from Cosmos 2583 p/l 2 March 18 at about 20:15 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 5, 19:49	6967	0.0013	580	598	96.45	81.99	267
2025 Mar 19, 13:46	6965	0.0015	576	597	96.42	82.00	126
Cosmos 2583 payload 2? (Cosmos 2588?) 2025-026F 63330						in space
Separated from Cosmos 2583 pl/1 March 18 at about 20:15 UTC. Conducting joint manoeuvres with Cosmos 2583 - mission unclear.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 18, 23:41	6966	0.0014	578	597	96.43	82.01	127
Volga rocket stage 2025-026D 62905						Re-entered - 2025 Feb 5 Life <1 day
Released Cosmos 2582 and Cosmos 2583 at about 04:30 UTC and then raised orbit. Orbit lowered when about 2000 km behind Cosmos 2582 to be followed by release of Cosmos 2581. Retro-fire at about 14:00 UTC led to destructive re-entry, at about 14:50 UTC, above the southern Pacific Ocean.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 5, 11:52	6964	0.0010	579	593	96.39	81.99	276
Soyuz second stage 2025-026E 62906						Re-entered - 2025 Mar 24 Life 47 days
Launched Cosmos 2581 - Cosmos 2583.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 5, 09:58	6772	0.0272	210	578	92.44	82.01	74

2025-027 Falcon 9 Block 5 (Starlink Group 12-09) Cape Canaveral Space Force Station						2025 Feb 8, 19:18
Starlink 11552 2025-027A 62907						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 20:23 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   ( ° )
2025 Feb 13, 14:00	6678	0.0002	299	301	90.52	43.01	269
Falcon 9 second stage uncatalogued						Re-entered - 2025 Feb 8 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-028 Electron (IOT 4 You and Me) Rocket Lab Launch Complex, New Zealand						2025 Feb 8, 20:43
Kinéis 2C (Kinéis 13) 2025-028B 62929						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Feb 10, 18:57	7021	0.0002	641	644	97.57	97.96	62	09:06
Kinéis 2D (Kinéis 14) 2025-028C 62930						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Feb 10, 20:35	7020	0.0002	641	643	97.56	97.96	48	09:06
Kinéis 2E (Kinéis 15) 2025-028D 62931						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Feb 10, 18:57	7020	0.0001	641	642	97.56	97.96	95	09:06
Kinéis 2A (Kinéis 11) 2025-028E 62932						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Feb 10, 18:56	7019	0.0001	640	642	97.54	97.96	329	09:06
Kinéis 2B (Kinéis 12) 2025-028G 62934						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Feb 11, 14:27	7019	0.0001	640	641	97.53	97.96	271	09:06
Electron third stage (kick stage) 2025-028A 62928						in space
Launched five Kinéis satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 9, 00:46	6989	0.0043	581	641	96.92	97.93	42
Electron second stage 2025-028F 62933						Re-entered - 2025 Feb 21 Life 13 days
Launched five Kinéis satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 10, 19:43	6772	0.0315	180	607	92.44	97.96	222

2025-029 Falcon 9 Block 5 (Starlink Group 11-10) Vandenberg Space Force Base						2025 Feb 11, 02:09
Starlink 32728 2025-029A 62948						in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:11 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   ( ° )
2025 Feb 18, 16:00	6682	0.0001	303	304	90.60	53.15	58
Falcon 9 second stage uncatalogued						Re-entered - 2025 Feb 11 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-030 CZ 8A Wenchang Space Centre						2025 Feb 11, 09:30
Hulianwang Digui 02-01 (Satellite Internet low orbit group 02-01) 2025-030A 62971						in space
One of nine simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation. All satellites were injected into similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 11, 15:42	7246	0.0008	863	874	102.32	50.00	257
CZ 8A upper stage 2025-30K 62980						in space
Launched group of nine Hulianwang Digui low orbit internet comsats. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 11, 15:36	7161	0.0119	698	868	100.51	50.00	83

2025-031 Falcon 9 Block 5 (Starlink Group 12-18) Cape Canaveral Space Force Station						2025 Feb 11, 18:53
Starlink 11543 2025-031A 62981						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 19:57 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   ( ° )
2025 Feb 18, 18:00	6695	0.0002	315	318	90.86	43.00	291
Falcon 9 second stage uncatalogued						Re-entered - 2025 Feb 11 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-032 Falcon 9 Block 5 (Starlink Group 12-08) Cape Canaveral Space Force Station						2025 Feb 15, 06:14
Starlink 11448 2025-032A 63005						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 07:19 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   ( ° )
2025 Feb 20, 16:00	6678	0.0001	299	300	90.51	43.01	243
Falcon 9 second stage uncatalogued						Re-entered - 2025 Feb 15 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-033 Electron (Fasten Your Seat Belts) Rocket Lab Launch Complex, New Zealand						2025 Feb 18, 23:17
BlackSky 31 (Global 31) 2025-033B 63027						in space
Third Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc. Released from kick stage February 19 at 00:12 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 19, 14:19	6851	0.0008	468	479	94.07	59.00	325
Electron third stage (kick stage) 2025-033A 63026						in space
Launched BlackSky 31 satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 19, 14:24	6852	0.0007	469	478	94.07	59.00	354
Electron second stage 2025-033C 63028						Re-entered - 2025 Feb 26 Life 8 days
Launched BlackSky 31 satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 19, 06:29	6706	0.0227	175	479	91.08	59.00	268

2025-034 Falcon 9 Block 5 (Starlink Group 10-12) Cape Canaveral Space Force Station						2025 Feb 18, 23:21
Starlink 32798 2025-034A 63029						in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle February 19 at 00:27 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   ( ° )
2025 Feb 25, 16:00	6670	0.0001	291	292	90.35	53.16	50
Falcon 9 second stage uncatalogued						Re-entered - 2025 Feb 19 Life 1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-035 Falcon 9 Block 5 (Starlink Group 12-14) Cape Canaveral Space Force Station						2025 Feb 21, 15:19
Starlink 11550 2025-035A 63052						in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 16:24 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   ( ° )
2025 Feb 27, 20:00	6663	0.0002	284	286	90.21	43.00	289
Falcon 9 second stage uncatalogued						Re-entered - 2025 Feb 21 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-036 CZ 3B Xichang Space Centre						2025 Feb 22, 12:11
Zhongxing 10R (Chinasat 10R) 2025-036A 63075						in space
Communications satellite described as providing services to users in China's transportation, emergency, energy, forestry and grassland industries, as well as to other countries in central Asia. Probably for use by government/military services. Expected location 110°.5 east to replace Zhongxing 10 (37677, 2011-026A).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Feb 22, 18:01	24372	0.7298	206	35782	631.11	27.63	179
2025 Mar 4, 19:06	42166	0.0002	35779	35796	1436.14	0.07	80	126°.0 E
CZ 3B fourth stage 2025-036B 63076						in space
Launched Zhongxing 10R.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 22, 19:04	24363	0.7303	193	35777	630.76	27.69	180

2025-037 Falcon 9 Block 5 (Starlink Group 15-01) Vandenberg Space Force Base						2025 Feb 23, 01:38
Starlink 32839 2025-037A 63077						in space
One member of a simultaneously-launched cluster of twenty two broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:39 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   ( ° )
2025 Feb 28, 16:00	6657	0.0004	276	281	90.08	69.99	275
Falcon 9 second stage uncatalogued						Re-entered - 2025 Feb 23 Life <1 day
Launched twenty two Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-038 Falcon 9 Block 5 Kennedy Space Center						2025 Feb 27, 00:16
Athena (IM-2) 2025-038A 63099						in space
Lunar landing vehicle launched under NASA's Commercial Lunar Payload Services programme. Built by US company Intuitive Machines, carrying three experiments including two surface exploration vehicles. Released from launch vehicle at 01:00 UTC. Initial Earth orbit similar to the Falcon 9 upper stage (63103, 2025-023E). A 492s thruster firing February 3 at 13:41 UTC resulted in orbit around the Moon. Multiple thruster firings on March 6 resulted in touchdown near the south pole of the Moon at 17:30 UTC about 400 metres from the aim point. Communication was established with ground stations, indicating it had toppled over. Athena was planned to operate for ten days until lunar sunset but operations ceased when battery power was exhausted March 7.
Landed on the Moon
Chimera GEO 1 2025-038B 63100						in space
GEO satellite transfer vehicle from US company Epic Aerospace. Carries a 16U Cubesat from Norwegian company Space Inventor to be released into GEO. Separated from launch vehicle at 01:04 UTC. Current status unknown - not currently being tracked by Space-Track.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	190235	0.9654	212	367501	13762.38	28.52	216
Lunar Trailblazer 2025-038C 63101						in space
NASA SIMPLEx (Small Innovative Missions for Planetary Exploration) Moon orbiter designed to map lunar resources including water. Released from launch vehicle at 01:04 UTC. Originally expected to arrive in the vicinity of the Moon 4-7 months after launch after a series of thruster firings. Radio contact was established after launch but was then lost almost immediately.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	190235	0.9654	212	367501	13762.38	28.52	216
Odin 2025-038D 63102						in space
Asteroid exploration mission from US company AstroForge. Released from launch vehicle at 01:02 UTC. Initial Earth orbit similar to the Falcon 9 upper stage (63103, 2025-023E). Planned to fly by asteroid 2022 OB5 in 2025 late-December but AstroForge was unable to establish ongoing communication in order to direct Odin towards its target.
Heliocentric orbit
Falcon 9 second stage 2025-038E 63103						in space
Launched Athena, Odin, Lunar Trailblazer and Chimera GEO 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	190235	0.9654	212	367501	13762.38	28.52	216

2025-039 Falcon 9 Block 5 (Starlink Group 12-13) Cape Canaveral Space Force Station						2025 Feb 27, 03:34
Starlink 11629 2025-039A 63104						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:39 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   ( ° )
2025 Mar 5, 20:00	6683	0.0002	304	306	90.62	43.00	256
Falcon 9 second stage						Re-entered - 2025 Feb 27 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Orbit parameters awaited

2025-040 CZ 2C Jiuquan Space Centre						2025 Feb 27, 07:08
Siwei Gaojing 1-03 (Superview Neo 1-03) 2025-040A 63125						in space
One of a simultaneously launched pair of commercial remote sensing satellites from the Siwei Surveying and Mapping Technology Co aimed at producing 3D Earth images.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Feb 27, 13:25	6876	0.0012	489	506	94.56	97.31	243	13:30
Siwei Gaojing 1-04 (Superview Neo 1-04) 2025-040B 63126						in space
One of a simultaneously launched pair of commercial remote sensing satellites from the Siwei Surveying and Mapping Technology Co aimed at producing 3D Earth images.e
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Feb 27, 13:25	6876	0.0012	489	506	94.57	97.31	241	13:30
CZ 2C second stage 2025-040C 63127						in space
Launched pair of Siwei Gaojing radar imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 27, 11:34	6869	0.0016	480	501	94.42	97.14	323

2025-041 Soyuz-2.1a Baikonur Cosmodrome						2025 Feb 27, 21:24
Progress MS-30 (Progress 7K-MS №460) 2025-041B 63129						in space
Supplies to ISS. Initial orbit similar to launch vehicle. Docked with the rearward-facing port of the ISS Zarya module March 1 at 23:02 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 28, 04:51	6691	0.0006	309	317	90.78	51.63	312
2025 Mar 2, 12:58	6796	0.0006	414	422	92.92	51.63	334
Soyuz third stage 2025-041A 63128						Re-entered - 2025 Mar 1 Life 2 days
Launched Progress MS-30.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Feb 28, 04:47	6580	0.0029	183	221	88.53	51.66	104

2025-042 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2025 Mar 2, 22:22
Cosmos 2584 (Uragan-K2 №14L) 2025-042A 63130						in space
GLONASS navigation satellite to fill a space in the constellation. Separated from the launch vehicle Fregat stage at about 04:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 3, 17:53	25526	0.0003	19140	19155	676.44	64.81	295
2025 Mar 18, 23:03	25508	0.0008	19110	19150	675.73	64.83	236
Fregat rocket stage 2025-042B 63131						in space
Launched Cosmos 2584. Minor changes in orbit may be due to venting of residual propellant.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 3, 10:58	25492	0.0011	19086	19141	675.09	64.83	263
2025 Mar 3, 16:47	25484	0.0002	19101	19110	674.77	64.84	235
2025 Mar 3, 22:55	25457	0.0017	19036	19121	673.69	64.82	198

2025-043 Falcon 9 Block 5 (Starlink Group 12-20) Cape Canaveral Space Force Station						2025 Mar 3, 02:24
Starlink 11609 2025-043A 63132						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:29 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   ( ° )
2025 Mar 7, 18:00	6674	0.0001	294	296	90.43	43.00	253
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 3 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-044 Ariane 6 (VA-263) Centre Spatiale Guyanaise						2025 Mar 6, 16:24
Composante Spatiale Optique 3 (CSO 3) 2025-044A 63156						in space
Military/Government Earth high resolution imaging satellite for the French Air and Space Forces Space Command (CDE). Third in a constellation of three satellites to replace the Helios 2 series. Aimed at 800km sun-synchronous orbit with LTDN around 01:15 near to that of CSO 1 in order to improve the revisit time over a target. Released from launch vehicle at 17:30 UTC. First commercial launch by Ariane 6. Orbit information based on data from amateur observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 19, 04:34	7181	0.0002	801	804	100.93	98.61	7	01:28
Ariane 6 third stage uncatalogued						Re-entered - 2025 Mar 6 Life <1 day
Launched CSO 3. Caused to re-enter above the south east Indian Ocean at about 19:00 UTC on the day of launch, following retro-fire.
Not Catalogued - orbit parameters unavailable

2025-045 CZ 3B Xichang Space Centre						2025 Mar 9, 17:17
Tongxin Jishu Shiyan 15 (Communication Technology Test 15, TJS 15) 2025-045A 63157						in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT). Appears to have moved from transfer orbit to GEO March 14 and then separated from 2025-045C about 24 hours later (date/time to be confirmed). Mission profile resembles that of TJS 3 (2018-110).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Mar 10, 03:50	24523	0.7327	178	36111	636.96	19.02	179
2025 Mar 17, 17:27	42165	0.0001	35785	35789	1436.12	0.01	322	90°.3 E
CZ 3B fourth stage 2025-045B 63158						in space
Launched TJS 15.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 12, 05:02	24842	0.7376	141	36787	649.44	19.04	182
apogee motor (CZ 3B fifth stage) 2025-045C 63299						in space
Moved TJS 15 from transfer orbit to geosynchronous drift orbit and (possibly) to its GEO location, then manoeuvred itself to graveyard orbit after releasing the satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	42165	0.0001	35785	35789	1436.12	0.01	322
2025 Mar 17, 16:17	42562	0.0027	36068	36299	1456.42	0.04	7

2025-046 CZ 8A (Y6) Wenchang Space Centre - Hainan Commercial Zone						2025 Mar 11, 16:38
Qianfan Ji Gui (05?)-01 2025-046A 63159						in space
One member of a simultaneously launched cluster of eighteen broadband distribution satellites for the Thousand Sails constellation. All satellites were probably injected into similar orbits at 89° inclination.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 24, 20:16	7292	0.0013	904	923	103.28	88.99	167
CZ 8A upper stage 2025-046U 63177						in space
Launched group of eighteen Qianfan Ji Gui i satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 24, 19:10	7239	0.0065	814	908	102.16	88.99	80

2025-047 Falcon 9 Block 5 Vandenberg Space Force Base						2025 Mar 12, 03:10
PUNCH Narrow Field Imager (Polarimeter to Unify the Corona and Heliosphere) 2025-047A 63178						in space
One of a set of four simultaneously-launched small satellites from NASA to study the solar wind by tracking groups of electrons as they travel away from the Sun. Will orbit independently of the three wide field imager satellites. Released from launch vehicle at 04:03 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 13, 09:36	7027	0.0015	638	659	97.70	97.95	163	17:59
PUNCH Wide Field Imager 1 (Polarimeter to Unify the Corona and Heliosphere) 2025-047B 63179						in space
One of a set of four simultaneously-launched small satellites from NASA to study the solar wind by tracking groups of electrons as they travel away from the Sun. The three satellites equipped with wide field imaging systems will be distributed at 120° intervals round the orbit. Released from launch vehicle at 04:03 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 13, 09:36	7027	0.0017	637	661	97.71	97.96	160	17:59
PUNCH Wide Field Imager 3 (Polarimeter to Unify the Corona and Heliosphere) 2025-047C 63180						in space
One of a set of four simultaneously-launched small satellites from NASA to study the solar wind by tracking groups of electrons as they travel away from the Sun. The three satellites equipped with wide field imaging systems will be distributed at 120° intervals round the orbit. Released from launch vehicle at 04:03 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 13, 19:12	7028	0.0017	639	662	97.74	97.96	159	18:00
PUNCH Wide Field Imager 2 (Polarimeter to Unify the Corona and Heliosphere) 2025-047D 63181						in space
One of a set of four simultaneously-launched small satellites from NASA to study the solar wind by tracking groups of electrons as they travel away from the Sun. The three satellites equipped with wide field imaging systems will be distributed at 120° intervals round the orbit. Released from launch vehicle at 04:03 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 13, 19:12	7029	0.0017	639	663	97.75	97.96	159	18:00
SPHEREx (Spectro-Photometer for the History of the Universe, Epoch of Reionization and Ices Explorer) 2025-047E 63182						in space
NASA satellite to map the celestial sphere at infrared wavelengths. Released from launch vehicle at 03:52 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 13, 19:12	7031	0.0012	645	662	97.79	97.98	173	18:00
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 12 Life <1 day
Launched SPHEREx and four PUNCH satellites. Caused to re-enter above the southern Pacific Ocean at about 05:05 UTC.
Not Catalogued - orbit parameters unavailable

2025-048 Falcon 9 Block 5 (Starlink Group 12-21) Cape Canaveral Space Force Station						2025 Mar 13, 02:36
Starlink 11602 2025-048A 63183						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:41 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   ( ° )
2025 Mar 18, 20:00	6655	0.0002	275	278	90.04	43.01	260
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 13 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-049 Falcon 9 Block 5 Kennedy Space Center						2025 Mar 14, 23:03
SpaceX Dragon Crew 10 (Dragon Endurance Flight #4) 2025-049A 63204						in space
Crew flight to ISS provided by SpaceX under contract to NASA. Crew members: Commander - Anne McClain (NASA), Pilot - Nicole Ayers, Mission Specialists - Kirill Peskov (Roscosmos), and Takuya Onishi (JAXA). Initial orbit similar to launch vehicle upper stage. Docked with the forward-facing port of the ISS Harmony module on March 16 at 04:04 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 15, 09:54	6605	0.0025	210	243	89.03	51.65	238
2025 Mar 16, 09:41	6795	0.0006	412	421	92.90	51.64	28
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 15 Life 1 day
Launched Dragon Crew 10. Caused to re-enter after releasing the spacecraft.
Not Catalogued - orbit parameters unavailable

2025-050 Electron (The Lightning God Reigns) Rocket Lab Launch Complex, New Zealand						2025 Mar 15, 00:00
QPS-SAR 9 (Susanoo-I) 2025-050A 63205						in space
Commercial satellite from Japanese company iQPS, equipped with an Earth imaging radar. One in a constellation that will ultimately consist of 36 satellites. Separated from launch vehicle at 00:55 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 18, 08:33	6955	0.0006	573	582	96.22	42.02	290
Electron second stage 2025-050B 63206						Re-entered - 2025 Apr 9 Life 25 days
Launched QPS-SAR 9 satellite. Initially identified by Space-Track incorrectly as the third (kick) stage.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 18, 11:50	6777	0.0242	235	563	92.54	42.03	289
Electron third stage (kick stage) 2025-050C 63207						in space
Launched QPS-SAR 9 satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 21, 05:21	6953	0.0008	569	581	96.17	42.02	318

2025-051 CZ 2D Jiuquan Space Centre						2025 Mar 15, 04:11
Siwei Gaojing 3-02 (Superview Neo 3-02) 2025-051A 63208						in space
Commercial remote sensing satellites operated by Beijing Space View Technology Co. Ltd. of China. 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
2025 Mar 15, 16:59	6874	0.0009	489	502	94.53	97.49	276	10:30
Tianyan 23 2025-051B 63209						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
2025 Mar 15, 17:00	6873	0.0008	489	501	94.52	97.49	285	10:30
CZ 2D second stage uncatalogued						in space
Launched Siwei Gaojing 3-02 and Tianyan 23. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-052 Falcon 9 Block 5 (Transporter 13) Vandenberg Space Force Base						2025 Mar 15, 06:43
Satellites						in space
Payload list to follow.

2025-053 Falcon 9 Block 5 (Starlink Group 12-16) Cape Canaveral Space Force Station						2025 Mar 15, 11:35
Starlink 11654 2025-053A 63265						in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 12:40 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   ( ° )
2025 Mar 21, 20:00	6680	0.0002	301	303	90.56	43.00	271
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 15 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-054 Angara 1.2 Plesetsk Cosmodrome						2025 Mar 16, 10:50
Cosmos 2585 (Rodnik-S?) 2025-054A 63288						in space
Probable government/military system store-dump communications satellite - to be confirmed. Placed in the same orbit plane as the three Rodnik satellites from the 2015-050 launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 17, 17:26	7883	0.0015	1493	1517	116.09	82.50	344
2025 Apr 23, 17:58	7883	0.0014	1494	1516	116.09	82.50	258
2025 Apr 25, 12:32	7878	0.0018	1486	1513	115.97	82.50	234
2025 Apr 27, 16:44	7876	0.0020	1483	1513	115.94	82.50	225
2025 Apr 28, 19:48	7873	0.0023	1477	1513	115.87	82.49	218
2025 May 3, 21:31	7873	0.0024	1476	1513	115.86	82.49	206
Cosmos 2586 (Rodnik-S?) 2025-054B 63289						in space
Probable government/military system store-dump communications satellite - to be confirmed. Placed in the same orbit plane as the three Rodnik satellites from the 2015-050 launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 17, 21:18	7881	0.0014	1492	1514	116.06	82.50	336
2025 Apr 14, 16:57	7881	0.0013	1493	1514	116.06	82.50	271
2025 Apr 16, 09:34	7877	0.0015	1487	1511	115.96	82.50	246
2025 Apr 21, 13:16	7873	0.0019	1480	1510	115.87	82.49	223
2025 May 1, 18:38	7872	0.0020	1478	1510	115.86	82.49	199
Cosmos 2587 (Rodnik-S?) 2025-054C 63290						in space
Probable government/military system store-dump communications satellite - to be confirmed. Placed in the same orbit plane as the three Rodnik satellites from the 2015-050 launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 17, 17:25	7880	0.0014	1491	1513	116.04	82.50	331
2025 Apr 1, 23:05	7873	0.0013	1485	1505	115.88	82.50	257
Angara 1.2 second stage uncatalogued						in space
Launched Cosmos 2585 - Cosmos 2587. Caused to re-enter above the Atlantic Ocean, at about 12:20 UTC on the day of launch, after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-055 Ceres 1 (Gushenxing 1 Y-10) Jiuquan Space Centre						2025 Mar 17, 08:07
Yunyao-1 55 2025-055xx						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 17, 16:05	6916	0.0012	529	546	95.39	97.59	294	14:26
Yunyao-1 56 2025-055xx						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 17, 16:05	6916	0.0012	529	546	95.40	97.59	293	14:26
Yunyao-1 57 2025-055xx						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 17, 16:05	6916	0.0014	528	547	95.40	97.60	296	14:26
Yunyao-1 58 2025-055xx						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 17, 16:06	6916	0.0013	529	547	95.40	97.59	294	14:26
Yunyao-1 59 2025-055xx						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 17, 16:07	6916	0.0013	529	547	95.40	97.60	294	14:26
Yunyao-1 60 2025-055xx						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 17, 16:07	6916	0.0012	530	547	95.41	97.60	291	14:26
Zhongke 06 (Airsat 06) 2025-055xx						in space
Demonstrator satellite for an imaging constellation from AIRSAT Technology Group, China. May be carrying an imaging radar.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 17, 16:06	6917	0.0012	530	547	95.41	97.60	291	14:26
Zhongke 07 (Airsat 07) 2025-055xx						in space
Demonstrator satellite for an imaging constellation from AIRSAT Technology Group, China. May be carrying an imaging radar.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 17, 16:06	6917	0.0012	530	547	95.41	97.60	289	14:26
Ceres 1 second stage uncatalogued						Re-entered - 2025 Mar 17 Life <1 day
Launched six Yunyao-1 satellites and two Zhongke. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-056 Electron (High Five) Rocket Lab Launch Complex, New Zealand						2025 Mar 18, 01:31
Kinéis 4E (Kinéis 25) 2025-056A 63300						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 18, 15:13	7024	0.0002	644	647	97.64	97.97	104	13:53
Kinéis 4C (Kinéis 23) 2025-056B 63301						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 18, 11:58	7024	0.0002	644	647	97.64	97.97	106	13:53
Kinéis 4D (Kinéis 24) 2025-056C 63302						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 18, 15:13	7023	0.0001	645	646	97.63	97.97	154	13:53
Kinéis 4A (Kinéis 21) 2025-056D 63303						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 18, 15:13	7023	0.0001	644	645	97.61	97.97	325	13:53
Kinéis 4B (Kinéis 22) 2025-056E 63304						in space
Small satellite from French company Kinéis in a planned constellation of twenty five broadband internet communication satellites. Released from launch vehicle at about 21:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 18, 15:12	7022	0.0002	643	645	97.60	97.97	286	13:53
Electron second stage 2025-056F 63305						Re-entered - 2025 Apr 1 Life 14 days
Launched five Kinéis satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 18, 04:10	6792	0.0334	187	641	92.85	97.97	230
Electron third stage (kick stage) 2025-056G 63306						in space
Launched five Kinéis satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 18, 04:23	6992	0.0045	582	645	96.97	97.97	41

2025-057 Falcon 9 Block 5 (Starlink Group 12-25) Cape Canaveral Space Force Station						2025 Mar 18, 19:57
Starlink 11568 2025-057A 63307						in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 21:03 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   ( ° )
2025 Mar 21, 20:00	6666	0.0002	287	289	90.28	43.01	272
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 18 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-058 Falcon 9 Block 5 (NRO L-57) Vandenberg Space Force Base						2025 Mar 21, 06:49
USA 487 (Starshield 0097) 2025-058A 63333						in space
One of a simultaneously-launched group of eleven US government NRO imaging reconnaissance satellites. Design is related the SpaceX Starlink satellites and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. All satellites were launched to a similar altitude at about 70° inclination.
Orbit classified as 'Secret' - data withheld
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 21 Life <1 day
Launched eleven Starshield satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-059 Ceres 1 (Gushenxing 1 Y-17) Jiuquan Space Centre						2025 Mar 21, 11:07
Yunyao-1 43 2025-059A 63344						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 21, 19:08	6918	0.0011	532	547	95.44	97.59	300	17:25
Yunyao-1 44 2025-059B 63345						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 21, 19:00	6920	0.0009	536	548	95.48	97.60	322	17:25
Yunyao-1 45 2025-059C 63346						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 21, 19:00	6916	0.0013	529	546	95.39	97.60	287	17:25
Yunyao-1 46 2025-059D 63347						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 21, 19:00	6916	0.0012	529	546	95.40	97.60	290	17:25
Yunyao-1 47 2025-059E 63348						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 21, 19:08	6917	0.0012	531	547	95.43	97.60	311	17:25
Yunyao-1 48 2025-059F 63349						in space
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 21, 19:08	6916	0.0012	530	547	95.41	97.60	294	17:25
Ceres 1 second stage uncatalogued						Re-entered - 2025 Mar 21 Life <1 day
Launched six Yunyao-1 satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-060 Falcon 9 Block 5 (NRO L-69) Cape Canaveral Space Force Station						2025 Mar 24, 17:48
USA 498 (NOSS 3-10?) 2025-060A 63350						in space
US government satellite from the National Reconnissance Office. Probably a NOSS ocean surveillance mission. Initial orbit is an estimate created from pre-launch data and published images/descriptions of the Falcon 9 upper stage venting propellant as it passed across Europe on its first orbit. Subsequent orbits are based on precise amateur observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 24, 20:00	7480	0.0015	1091	1113	107.30	64.00	110
2025 Mar 27, 21:03	7486	0.0128	1012	1204	107.44	63.45	180
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 24 Life <1 day
Launched USA 498. Caused to re-enter above the southern Indian Ocean at about 20:50 UTC, after releasing the payload.
Not Catalogued - orbit parameters unavailable

2025-061 Electron (Finding Hot Wildfires Near You) Rocket Lab Launch Complex, New Zealand						2025 Mar 26, 15:30
OroraTech Constellation Phase 1 001 2025-061xx						in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 26, 18:12	6915	0.0020	523	551	95.38	97.52	354	03:52
OroraTech Constellation Phase 1 002 2025-061xx						in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 26, 18:13	6916	0.0022	523	552	95.39	97.51	356	03:52
OroraTech Constellation Phase 1 003 2025-061xx						in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 26, 18:12	6915	0.0018	524	549	95.37	97.51	356	03:52
OroraTech Constellation Phase 1 004 2025-061xx						in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 26, 18:10	6916	0.0021	523	552	95.39	97.52	359	03:52
OroraTech Constellation Phase 1 005 2025-061xx						in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 26, 18:11	6918	0.0024	523	556	95.43	97.52	1	03:52
OroraTech Constellation Phase 1 006 2025-061xx						in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 26, 18:10	6917	0.0023	523	555	95.42	97.52	359	03:52
OroraTech Constellation Phase 1 007 2025-061xx						in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 26, 18:12	6919	0.0022	525	556	95.46	97.52	10	03:52
OroraTech Constellation Phase 1 008 2025-061xx						in space
6U Cubesat from Orbital Oracle Technologies (OroraTech), one of a simultaneously-launched group of eight. Built and operated by Spire and equipped with thermal imaging equipment to detect, monitor and report on wildfires on the Earth's surface. Released from launch vehicle during a short sequence beginning at 16:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Mar 26, 18:12	6925	0.0028	527	566	95.58	97.52	22	03:52
Electron third stage (kick stage) 2025-061J 63359						in space
Launched eight OroraTech satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 26, 18:11	6889	0.0048	477	544	94.84	97.51	301
Electron second stage 2025-061K 63360						Re-entered - 2025 Apr 4 Life 9 days
Launched eight OroraTech satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 26, 18:09	6732	0.0255	182	525	91.61	97.50	226

2025-062 CZ 3B Xichang Space Centre						2025 Mar 26, 15:55
Tianlian 2-04 2022-062A 63361						in space
Second Generation data communications satellite to provide a data relay, and measurement and control service for Chinese satellites and space stations. Probably moved to geosynchronous drift orbit March 27 at around 08:15 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Mar 26, 19:07	24394	0.7308	190	35841	631.94	27.11	179
2025 Apr 4, 14:59	42160	0.0032	35649	35916	1435.87	5.50	359	80°.0 E
CZ 3B fourth stage 2025-062B 63362						in space
Launched Tianlian 2-04.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 26, 19:14	23793	0.7248	169	34661	608.76	27.08	179

2025-063 Falcon 9 Block 5 (Starlink Group 11-07) Vandenberg Space Force Base						2025 Mar 26, 22:11
Starlink 32840 2025-063A 63363						in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 23:13 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   ( ° )
2025 Apr 2, 16:00	6686	0.0001	308	309	90.68	53.16	48
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 26 Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-064 CZ 7A (Y-11) Wenchang Space Centre						2025 Mar 29, 16:05
Tongxin Jishu Shiyan 16 (Communication Technology Test 16, TJS 16) 2025-064A 63397						in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT). Probably entered geosynchronous drift orbit Mar 30 at around 08:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Mar 29, 23:01	24392	0.7318	164	35864	631.89	19.52	180
2025 Apr 7, 17:16	42165	0.0001	35783	35790	1436.09	0.06	106	152°.5 E
CZ 7A fourth stage 2025-064B 63398						in space
Launched TJS 16.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Mar 30, 17:45	23621	0.7252	113	34372	602.14	19.52	179

2025-065 Falcon 9 Block 5 (Starlink Group 06-80) Cape Canaveral Space Force Station						2025 Mar 31, 19:52
Starlink 33531 2025-065A 63399						in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 20:57 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   ( ° )
2025 Apr 8, 20:00	6669	0.0002	289	292	90.32	43.00	275
Falcon 9 second stage uncatalogued						Re-entered - 2025 Mar 31 Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-066 Falcon 9 Block 5 Kennedy Space Center						2025 Apr 1, 01:46
SpaceX Fram2 (Dragon Resilience flight #4) 2025-066A 63427						Re-entered - 2025 Apr 4 Life 3 days Returned to Earth
Science mission to polar orbit, the highest orbital inclination flown by a piloted vehicle since Soyuz 22 (1976-093A). Crew consists of Mission Commander Chun Wang, Vehicle Commander Jannicke Mikkelsen, Vehicle Pilot Rabea Rogge, and Mission Specialist and Medical Officer Eric Philips. Separated from launch vehicle at 01:56 UTC. Sixteen minutes of retro-fire, commencing April 4 at 15:26 UTC was followed by separation of the Trunk module at 15:43 UTC. Dragon splashed down in the Pacific Ocean near the coast of southern California at 16:19 UTC. Mission duration was determined by the crew's total radiation dose on orbit. Previous re-entries - the Trunk module was discarded BEFORE retro-fire and remained in orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Apr 1, 03:15	6685	0.0158	202	413	90.67	90.01	92	20:35
2025 Apr 1, 12:00	6808	0.0004	427	432	93.16	90.00	76	20:33
2025 Apr 4, 09:54	6785	0.0038	381	433	92.70	90.01	80	20:22
2025 Apr 4, 14:46	6774	0.0055	359	434	92.49	89.63	82	20:20
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 1 Life <1 day
Launched SpaceX Dragon Fram 2 mission. Caused to re-enter above the Indian Ocean at about 02:40 UTC, after releasing the spacecraft.
Not Catalogued - orbit parameters unavailable

2025-067 CZ 2D (Y-78) Jiuquan Space Centre						2025 Apr 1, 04:00
Hulianwang Xin Jishu Shiyan 0001 (Internet New Technology Test Satellite 0001) 2025-067A 63428						in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 1, 15:02	6831	0.0008	447	458	93.64	55.00	282
Hulianwang Xin Jishu Shiyan 0002 (Internet New Technology Test Satellite 0002) 2025-067B 63429						in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 1, 14:59	6828	0.0010	443	456	93.58	55.00	301
Hulianwang Xin Jishu Shiyan 0003 (Internet New Technology Test Satellite 0003) 2025-067C 63430						in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 1, 15:00	6829	0.0009	445	457	93.60	54.99	299
Hulianwang Xin Jishu Shiyan 0004 (Internet New Technology Test Satellite 0004) 2025-067D 63431						in space
Second generation test satellite for Chinese government communications system for use by Internet-connected devices. One of four carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 1, 14:59	6830	0.0008	446	457	93.62	55.00	285
CZ 2D second stage uncatalogued						Re-entered - 2025 Apr 1 Life <1 day
Launched cluster of four Hongtu 3 internet connectivity satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-068 CZ 6 (Y-14) Taiyuan Space Centre						2025 Apr 3, 02:12
Tianping 3A-02 2025-068A 63432						in space
Reportedly for space environment studies in LEO and acting as calibration targets for ground-based visual and radar tracking equipment. May also be equipped with an Earth imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 4, 13:21	7001	0.0244	452	794	97.17	43.01	111
CZ 6 third stage uncatalogued						in space
Launched Tianping 3A-02. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable

2025-069 Falcon 9 Block 5 (11-13) Vandenberg Space Force Base						2025 Apr 3, 13:02
Starlink 33682 2025-069A 63433						in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 14:02 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   ( ° )
2025 Apr 9, 20:00	6667	0.0000	289	289	90.30	53.15	47
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 3 Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-070 Falcon 9 Block 5 (Starlink Group 06-72) Cape Canaveral Space Force Station						2025 Apr 6, 03:07
Starlink 33679 2025-070A 63460						in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 04:12 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   ( ° )
2025 Apr 11, 16:00	6672	0.0001	293	295	90.40	43.00	233
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 6 Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-071 Falcon 9 Block 5 (Starlink Group 11-11) Vandenberg Space Force Base						2025 Apr 7, 23:06
Starlink 33828 2025-071A 63493						in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle April 8 at 00:05 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   ( ° )
2025 Apr 11, 18:00	6669	0.0001	290	291	90.32	53.16	53
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 8 Life 1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-072 Soyuz-2.1a Baikonur Cosmodrome						2025 Apr 8, 05:47
Soyuz MS-27 (Soyuz 11F732A48 № 758) 2025-072A 63520						in space
Crew to ISS - Sergei Ryzhikov and Alexei Zubritsky (both Roscosmos) and Jonathan Kim (NASA) . Separated from launch vehicle at 05:56 UTC. Docked with ISS Prichal module at 08:57:43 UTC. Initial orbit similar to launch vehicle upper stage.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 8, 11:42	6797	0.0005	415	422	92.94	51.64	22
Soyuz third stage 2025-072B 63521						Re-entered - 2025 Apr 10 Life 2 days
Launched Soyuz MS-27.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 8, 14:28	6594	0.0028	197	234	88.81	51.66	78

2025-073 CZ 3B Xichang Space Centre						2025 Apr 10, 16:47
Tongxin Jishu Shiyan 17 (Communication Technology Test 17, TJS 17) 2025-073A 63524						in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT). Probably entered geosynchronous drift orbit April 12 at around 15:15 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Apr 10, 21:00	24528	0.7325	184	36116	637.17	18.99	180
2025 Apr 21, 16:55	42165	0.0001	35783	35790	1436.09	0.04	119	152°.8 E
CZ 3B fourth stage 2025-073B 63525						in space
Launched TJS 17.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 10, 19:44	24855	0.7374	149	36804	649.95	19.02	180
apogee motor (CZ 3B fifth stage) 2025-073C 63629						in space
Moved TJS 17 from transfer orbit to geosynchronous drift orbit and (possibly) to its GEO location, then manoeuvred itself to graveyard orbit after releasing the satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 22, 01:53	42565	0.0010	36142	36231	1456.58	0.04	208

2025-074 Falcon 9 Block 5 (NRO L-192) Vandenberg Space Force Base						2025 Apr 12, 12:25
USA 499 (Starshield 0108) 2025-074A 63526						in space
One of a simultaneously-launched group of twenty two US government NRO intelligence gathering (probably imaging) satellites. Design is related the SpaceX Starlink satellites and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6678	0.0010	293	306	90.51	69.90	155
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 12 Life <1 day
Launched twenty two Starshield satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-075 Falcon 9 Block 5 (Starlink Group 12-17) Kennedy Space Center						2025 Apr 13, 00:53
Starlink 11669 2025-075A 63548						in space
One member of a simultaneously-launched cluster of twenty one broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 01:58 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   ( ° )
2025 Apr 18, 16:00	6676	0.0002	297	299	90.48	43.01	248
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 13 Life <1 day
Launched twenty one Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-076 Falcon 9 Block 5 (Starlink Group 06-73) Cape Canaveral Space Force Station						2025 Apr 14, 04:00
Starlink 32959 2025-076A 63569						in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 05:05 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   ( ° )
2025 Apr 22, 18:00	6692	0.0002	312	315	90.80	43.00	264
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 14 Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-077 Minotaur 4 (NRO L-174) Vandenberg Space Force Base						2025 Apr 16, 19:33
USA 521 2025-077A 63596						in space
US government satellite, either for intelligence gathering or testing of sensors/equipment for future missions. Orbit height unknown but inclination about 63°.
Orbit classified as 'Secret' - data withheld
USA 522 2025-077B 63597						in space
US government satellite, either for intelligence gathering or testing of sensors/equipment for future missions. Orbit height unknown but inclination about 63°.
Orbit classified as 'Secret' - data withheld
Minotaur 4 fourth stage 2025-077C 63598						in space
Launched two US government satellites.
Orbit parameters awaited

2025-078 CZ 6A (Y-11) Taiyuan Space Centre						2025 Apr 18, 22:51
Shiyan 27-01 (Test 27-01) 2025-078A 63599						in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Apr 19, 09:12	7383	0.0006	1000	1009	105.21	99.69	229	06:00
Shiyan 27-02 (Test 27-02) 2025-078B 63600						in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Apr 19, 09:12	7383	0.0006	1000	1009	105.22	99.69	222	06:00
Shiyan 27-03 (Test 27-03) 2025-078C 63601						in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Apr 19, 09:12	7383	0.0007	1000	1011	105.23	99.69	229	06:00
Shiyan 27-04 (Test 27-04) 2025-078D 63602						in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Apr 19, 09:13	7384	0.0008	1000	1011	105.24	99.70	215	06:00
Shiyan 27-05 (Test 27-05) 2025-078E 63603						in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Apr 19, 09:13	7385	0.0009	1000	1013	105.26	99.69	227	06:00
Shiyan 27-06 (Test 27-06) 2025-078F 63604						in space
Purpose unknown - described as "mainly used for space environment detection" but probably has an Earth imaging mission. Orbit is co-planar with Shijian 6-03 (48157, 2021-028A) launched 2021 April 8.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 Apr 19, 09:13	7385	0.0009	1000	1013	105.26	99.70	225	06:00
CZ 6A third stage 2025-078G 63605						in space
Launched Shiyan 27 group. Orbit lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 19, 09:14	7290	0.0107	834	990	103.25	99.70	108

2025-079 Falcon 9 Block 5 (NRO L-145) Vandenberg Space Force Base						2025 Apr 20, 12:29
USA 523 (Starshield 0130) 2025-079A 63606						in space
One of a simultaneously-launched group of twenty two US government NRO intelligence gathering (probably imaging) satellites. Design is related the SpaceX Starlink satellites and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications.
Orbit classified as 'Secret' - data withheld
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 20 Life <1 day
Launched twenty two Starshield satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-080 Falcon 9 Block 5 Kennedy Space Center						2025 Apr 21, 08:15
SpaceX Dragon 2 CRS-32 2024-080A 63628						in space Returned to Earth
Carrying cargo to/from the ISS under NASA's Commercial Resupply Services (CRS) contract. Docked with the forward-facing port of the ISS Harmony Module April 22 at 12:40 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 21, 11:35	6671	0.0115	216	370	90.38	51.65	225
2025 Apr 22, 14:40	6795	0.0005	413	421	92.91	51.64	64
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 21 Life <1 day
Launched SpaceX Dragon 2 CRS-32. Caused to re-enter after releasing the spacecraft.
Not Catalogued - orbit parameters unavailable

2025-081 Falcon 9 Block 5 (Bandwagon 3) Cape Canaveral Space Force Station						2025 Apr 22, 00:48
Korea 425-04 2025-081A 63630						in space
Radar imaging satellite owned by the South Korean government specifically targetting activity across the Korean peninsula.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 22, 21:08	6955	0.0005	573	580	96.20	45.40	172
Tomorrow S7 (Tomorrow Microwave Sounder 7) 2025-081B 63631						in space
6U Cubesat from US company Tomorrow.io, designed to measure temperature and humidity profiles within the Earth's atmosphere. Catalogue Number, Designation and orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 22, 09:55	6955	0.0007	572	581	96.21	45.41	196
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 22 Life <1 day
Launched Korea 425-04 & Tomorrow S7. Caused to re-enter after releasing the satellites. Following retro-fire, Atmos Space's Phoenix 1 prototype re-entry vehicle equipped with an inflatable heat shield, separated and conducted a successful mission including splashdown about 2.5 hrs after lift-off.
Not Catalogued - orbit parameters unavailable

2025-082 CZ 2F Jiuquan Space Centre						2025 Apr 24, 09:17
Shenzhou 20 2025-082A 63632						in space
Crew to CSS - Chen Dong (commander), Chen Zhongrui (pilot) and and Wang Jie (flight engineer). Separated from launch vehicle at 09:27 UTC. Docked with the downward-facing port of the Tianhe module at 15:49 UTC on the day of launch. Initial orbit listed is based on Chinese data.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 24, 09:20	6650	0.0119	193	352	89.96	41.46	125
2025 Apr 24, 16:32	6761	0.0002	381	384	92.21	41.46	223
CZ 2F third stage 2025-082B 63633						Re-entered - 2025 May 3 Life 9 days
Launched Shenzhou 20.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 24, 19:37	6646	0.0113	193	343	89.86	41.46	127

2025-083 Falcon 9 Block 5 (Starlink Group 06-74) Cape Canaveral Space Force Station						2025 Apr 25, 01:52
Starlink 33879 2025-083A 63634						in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:57 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   ( ° )
2025 May 5, 18:00	6690	0.0002	310	313	90.75	43.00	265
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 25 Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-084 CZ 3B Xichang Space Centre						2025 Apr 27, 15:54
Tianlian 2-05 2022-084A 63662						in space
Second Generation data communications satellite to provide a data relay, and measurement and control service for Chinese satellites and space stations. Probably moved to geosynchronous drift orbit April 28 at around 08:15 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 Apr 27, 20:43	24385	0.7304	196	35818	631.62	27.15	180
2025 May 12, 13:55	42165	0.0002	35778	35796	1436.12	5.47	151	20°.4 E
CZ 3B fourth stage 2025-084B 63663						in space
Launched Tianlian 2-05.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 Apr 27, 20:08	23778	0.7244	175	34625	608.18	27.09	179

2025-085 Falcon 9 Block 5 (Starlink Group 12-23) Cape Canaveral Space Force Station						2025 Apr 28, 02:09
Starlink 11651 2025-085A 63664						in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:14 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   ( ° )
2025 May 5, 18:00	6691	0.0002	312	314	90.79	43.01	258
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 28 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-086 CZ 5B + YZ-2 Wenchang Space Centre - Hainan Commercial Zone						2025 Apr 28, 20:10
Hulianwang Digui 03-01 (Satellite Internet low orbit group 03-01) 2025-086A 63687						in space
One of ten simultaneously-launched internet communication satellites. Designed to fly in relatively-low orbit as part of a large constellation. All satellites were injected into similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 May 3, 12:14	7485	0.0012	1099	1116	107.42	86.50	295
YZ-2 rocket stage uncatalogued						Re-entered - 2025 Apr 28 Life <1 day
Launched ten internet comsats. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-087 Falcon 9 Block 5 (Starlink Group 11-09) Vandenberg Space Force Base						2025 Apr 28, 20:42
Starlink 33894 2025-087A 63697						in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 21:41 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   ( ° )
2025 May 5, 12:38	6663	0.0000	285	286	90.22	53.16	9
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 28 Life <1 day
Launched twenty seven Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-088 Atlas V 551 (KA-01, Kuiper Atlas 1) Cape Canaveral Space Force Station						2025 Apr 28, 23:01
Kuiper 00008 2025-088A 63724						in space
One member of a simultaneously-launched cluster of twenty seven broadband and mobile telephone communications satellites from US company Amazon. All satellites expected to be injected initially into similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 May 5, 20:00	6841	0.0011	456	470	93.86	51.86	139
Atlas V third stage (Centaur) uncatalogued						Re-entered - 2025 Apr 28 Life <1 day
Launched twenty seven Kuiper satellites.
Not Catalogued - orbit parameters unavailable

2025-089 Falcon 9 Block 5 (Starlink Group 12-10) Kennedy Space Center						2025 Apr 29, 02:34
Starlink 11677 2025-089A 63751						in space
One member of a simultaneously-launched cluster of twenty three broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:39 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   ( ° )
2025 May 5, 20:00	6686	0.0002	307	309	90.68	43.01	256
Falcon 9 second stage uncatalogued						Re-entered - 2025 Apr 29 Life <1 day
Launched twenty three Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-090 Vega-C (VV-26) Centre Spatiale Guyanaise						2025 Apr 29, 08:15
Biomass 2025-090A 63772						in space
Earth Explorer mission from the European Space Agency. Carries a radar imaging system capable of penetrating forest canopy to measure the height and mass of its undergrowth in order to to estimate its carbon content. The radar can also be used for mapping the geology of many kinds of ground type. Separated from launch vehicle at 09:13 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 May 1, 20:10	7045	0.0001	666	668	98.09	98.07	64	18:00
Vega upper stage (AVUM+) uncatalogued						Re-entered - 2025 Apr 29 Life <1 day
Launched Biomass. Caused to re-enter after releasing the satellite.
Not Catalogued - orbit parameters unavailable

2025-091 Falcon 9 Block 5 (Starlink Group 06-75) Cape Canaveral Space Force Station						2025 May 2, 01:51
Starlink 33932 2025-091A 63775						in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:56 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   ( ° )
2025 May 5, 20:00	6664	0.0002	285	287	90.24	43.00	208
Falcon 9 second stage uncatalogued						Re-entered - 2025 May 2 Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-092 Falcon 9 Block 5 (Starlink Group 06-84) Kennedy Space Center						2025 May 4, 08:54
Starlink 33909 2025-092A 63804						in space
One member of a simultaneously-launched cluster of twenty nine broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 09:59 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   ( ° )
2025 May 7, 18:00	6661	0.0002	282	284	90.17	43.00	253
Falcon 9 second stage uncatalogued						Re-entered - 2025 May 4 Life <1 day
Launched twenty nine Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-093 Falcon 9 Block 5 (Starlink Group 06-93) Cape Canaveral Space Force Station						2025 May 7, 01:17
Starlink 34018 2025-093A 63836						in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:22 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   ( ° )
2025 May 12, 18:00	6684	0.0002	304	307	90.63	43.00	270
Falcon 9 second stage uncatalogued						Re-entered - 2025 May 7 Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-094 Falcon 9 Block 5 (Starlink Group 15-03) Vandenberg Space Force Base						2025 May 10, 00:19
Starlink 2024-094A 63864						in space
One member of a simultaneously-launched cluster of twenty six broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 01:21 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   ( ° )
2025 May 15, 16:00	6671	0.0004	290	296	90.38	70.00	274
Falcon 9 second stage uncatalogued						Re-entered - 2025 May 10 Life <1 day
Launched twenty six Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-095 Falcon 9 Block 5 (Starlink Group 06-91) Cape Canaveral Space Force Station						2025 May 10, 06:28
Starlink 2025-095A 63890						in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 07:33 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   ( ° )
2025 May 15, 16:00	6667	0.0001	288	289	90.29	43.00	253
Falcon 9 second stage uncatalogued						Re-entered - 2025 May 10 Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-096 CZ 6A (Y-9) Taiyuan Space Centre						2025 May 11, 13:27
Yaogan 40-02 Leader 2025-096A 63918						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. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 May 12, 14:33	7181	0.0011	795	811	100.94	86.00	262
Yaogan 40-02 Follower 2025-096B 63919						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. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 May 12, 14:32	7181	0.0011	795	811	100.93	86.00	264
Yaogan 40-02 Outlier 2025-096C 63920						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. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 May 12, 15:50	7180	0.0011	794	810	100.92	86.00	269
CZ 6A third stage 2025-096E 63922						in space
Launched Yaogan 40 Group 2. Orbit lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 May 12, 15:11	7059	0.0072	631	732	98.38	86.02	66

2025-097 CZ 3C Xichang Space Centre						2025 May 12, 18:09
Tongxin Jishu Shiyan 19 (Communication Technology Test 19, TJS 19) 2025-097A 63924						in space
Probably military in nature and maybe intended for signals intelligence gathering (SIGINT). Probably entered geosynchronous drift orbit May 13 at around 10:25 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2025 May 12, 21:24	24382	0.7311	178	35830	631.49	28.58	180
CZ 3C upper stage 2025-097B 63925						in space
Launched TJS 19.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2025 May 12, 21:31	24304	0.7328	117	35734	628.44	28.60	179

2025-098 Falcon 9 Block 5 (Starlink Group 15-04) Vandenberg Space Force Base						2025 May 13, 01:15
Starlink 2025-098A 63926						in space
One member of a simultaneously-launched cluster of twenty six broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:16 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 - 2025 May 13 Life <1 day
Launched twenty six Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-099 Falcon 9 Block 5 (Starlink Group 06-83) Kennedy Space Center						2025 May 13, 05:02
Starlink 2025-099A 63952						in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:07 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 - 2025 May 13 Life <1 day
Launched twenty eight Starlink satellites. Caused to re-enter after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2025-100 CZ 2D Jiuquan Space Centre						2025 May 14, 04:12
Taikong Jisu 2025-100A 63982						in space
One of a cluster of twelve satellites from ADA Space of China. The group consists of several differing satellite designs and it is unclear whether they all have the same purpose, described as offering a computing service to other satellites in order to avoid bottlenecks caused by having to transmit data via ground stations before analysis. All satellites were injected initially into similar orbits
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2025 May 14, 21:14	6876	0.0010	491	505	94.57	97.41	261	10:30
CZ 2D second stage uncatalogued						Re-entered - 2025 May 14 Life <1 day
Launched Taikong Jisu cluster of four twelve satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2025-101 Falcon 9 Block 5 (Starlink Group 06-67) Cape Canaveral Space Force Station						2025 May 14, 16:38
Starlink 2025-101A 63994						in space
One member of a simultaneously-launched cluster of twenty eight broadband and mobile telephone communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 17:43 UTC. All satellites expected to be injected initially into similar orbits at about 300 km altitude.
Orbit parameters awaited
Falcon 9 second stage						in space
Launched twenty eight Starlink satellites. Expected to be caused to re-enter after releasing the satellites.
Orbit parameters awaited