2019 - Satellite & Spacecraft Launches and Detailed Orbits

Listed are launches, irrespective of outcome, that were irretrievably committed to flight towards orbit or intended to accelerate the payload to escape velocity. The following notes should help with understanding the launch lists.

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, and the source observations can often be found in the web-based Seesat-L discussion group. Occasionally, orbits are estimated by myself from public data.

Space-Track occasionally fails to allocate names to objects in its catalogue. In these cases, the names are derived from public information.

Apogee and perigee are measured against a spherical Earth with a radius of 6378.145 km assumedto 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=2019#001

2019-001 CZ 3B Xichang Space Centre						2019 Jan 10, 17:11
Zhongxing 2D (Chinasat 2D) 2019-001A 43920						in space
Chinese military or government communications satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Jan 10, 20:10	24378	0.7309	182	35818	631.34	27.11	180
2019 Jan 21, 21:15	42166	0.0002	35780	35795	1436.15	0.06	73	130° east

CZ 3B fourth stage 2019-001B 43921						Re-entered - 2019 Jul 3 Life 174 days
Launched Zhonxing 2D.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jan 10, 22:45	23644	0.7242	142	34389	603.02	27.08	179

2019-003 Epsilon Uchinoura Space Center, Japan						2019 Jan 18, 00:50
RAPIS-1 (Rapid Innovative Payload Demonstration Satellite 1) 2019-003A 43932						Re-entered - 2024 Sep 25 Life 2077 days
mall satellite developed by Axelspace in collaboration with JAXA. Demonstrator for a set of seven systems for potential use by future satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jan 18, 18:19	6882	0.0009	498	510	94.71	97.30	261

OrigamiSat 1 2019-003B 43933						Re-entered - 2022 Apr 30 Life 1198 days
3U Cubesat built as a demonstrator for a “multifunctional” membrane panel about 1.5m square and deployed from a 1m mast . Thin-film devices attached throughout the membrane will demonstrate designs for low-mass array aerials and solar arrays. The structure acted as an air brake resulting in relatively-rapid orbit decay and a relatively-short orbit life compared with other satellites from the launch. Also carries an amateur radio payload.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jan 18, 22:32	6880	0.0016	490	513	94.65	97.30	254

RISESat (Rapid International Scientific Experiment Satellite) 2019-003C 43934						Re-entered - 2023 Mar 14 Life 1516 days
Small earth-observation and science/ technology demonstrator carring eqipment from Sweden, The Czech Republic, Hungary, Taiwan, Vietnam, USA and Germany.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jan 18, 22:53	6879	0.0015	490	511	94.63	97.30	245
2023 Feb 13, 13:06	6769	0.0009	385	397	92.38	97.11	48

MicroDragon 2019-003D 43935						Re-entered - 2024 Oct 1 Life 2083 days
Small satellite from Vietnamese in collaboration with Japanese universities carrying sensors for Ocean colour remote sensing and aerosol polarisation remote sensing.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jan 19, 01:53	6878	0.0017	489	512	94.62	97.30	246
2023 Feb 13, 01:08	6855	0.0017	465	488	94.13	97.12	44

Nexus 2019-003F 43937						Re-entered - 2023 Nov 9 Life 1756 days
Small satellite carrying an experimental high-speed comunications sytem.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jan 18, 19:29	6874	0.0023	480	512	94.54	97.30	240

ALE 1 (Astro Live Experiences 1) 2019-003G 43938						Re-entered - 2023 Oct 4 Life 1720 days
Satellite aimed to create artificial meteors in a selection of colours (white, green, pink and orange) partly as performance art. Deployed a drag device in the fom of a tether 2019 Dec, several months later than planned. Reached meteor-release height of 410 km 2022 Jul 26 and released the tether at about 19:00 UTC in order to maintain a steady orbital altitude.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jan 18, 19:25	6874	0.0024	480	513	94.54	97.31	245
2019 Dec 27, 10:00	6873	0.0027	477	514	94.52	97.26	118
2020 Dec 21, 09:37	6865	0.0022	472	502	94.35	97.21	287
2021 Dec 21, 02:03	6848	0.0022	454	485	93.99	97.17	70
2022 Jul 28, 08:58	6787	0.0012	401	417	92.75	97.14	1
2023 Feb 13, 02:25	6761	0.0009	377	388	92.20	97.11	338

Velox IV 2019-003J 43940						Re-entered - 2023 Mar 24 Life 1526 days
Small satellite carring a super-high-resolution atmospheric imager.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jan 19, 05:00	6874	0.0023	480	512	94.54	97.30	240
2023 Feb 13, 04:24	6754	0.0008	370	381	92.06	97.10	358

Epsilon upper stage 2019-003E 43936						Re-entered - 2024 Nov 12 Life 2125 days
Launched a cluster of small satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jan 18, 19:34	6875	0.0023	481	513	94.56	97.30	252

ALE 1 de-orbit mechanism (DOM tether) 2019-003K 53314						Re-entered - 2022 Aug 3 Life 1293 days
Released from ALE 1 2022 July, when the orbit was down to 400 km - ALE 1's planned operational altitude.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2022 Jul 28, 07:23	6776	0.0011	390	405	92.51	97.13	348

2019-004 Delta 4 Heavy Vandenberg Air Force Base						2019 Jan 19, 19:10
USA 290 (KH-11 Block-5 F-1/Crystal) 2019-004A 43941						in space
KH-11 reconnaissance satellite. First of its type not to be aimed at sun-synchronous orbit. Orbital elements not released by Spacetrack so parameters are based on amateur observation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Feb 01, 06:33	6786	0.0019	395	420	92.71	73.61	49
2019 Sep 29, 18:43	6784	0.0023	390	421	92.68	73.58	193
2019 Nov 12, 18:13	6786	0.0023	392	424	92.73	73.58	77
2020 Apr 27, 18:55	6785	0.0014	398	417	92.71	73.59	74
2020 May 01, 20:19	6786	0.0014	398	417	92.72	73.59	64
2021 Jan 27, 17:37	6784	0.0012	397	414	92.68	73.58	117
2021 Apr 01, 21:02	6786	0.0012	400	416	92.72	73.59	293

Delta 4 upper stage uncatalogued						in space
Launched USA. Caused to re-enter above the Pacific Ocean about two hours after launch.
Not Catalogued - orbit parameters unavailable

2019-010 Soyuz ST-B + Fregat-M (VS-21) Centre Spatiale Guyanaise						2019 Feb 27, 21:37
OneWeb 0012 2019-010A 44057						in space
Broadband distribution satellite for the UK company OneWeb. One of 36 similar satellites carried on this launch.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Feb 28, 08:04	7378	0.0015	988	1011	105.11	87.77	250

2019-012 CZ 3B Xichang Space Centre						2019 Mar 9, 16:28
Zhongxing 6C (Chinasat 6C) 2019-012A 44067						in space
Comsat providing radio, TV and general communications to mainland China and its territorial waters, and to other users in the Asia-Pacific region. Expected location.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Mar 10, 11:16	27361	0.7594	205	41761	750.68	24.61	180
2019 Mar 19, 14:21	42165	0.0004	35772	35801	1436.09	0.12	36	130° east
2023 Feb 13, 13:43	42165	0.0004	35769	35805	1436.12	0.03	332	130° east

CZ 3B fourth stage 2019-012B 44068						Re-entered - 2023 Dec 17 Life 1744 days
Launched Zhongxin 6C.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Mar 11, 23:23	26768	0.7548	186	40594	726.42	24.61	180

2019-016 Electron (Two Thumbs Up) Rocket Lab Launch Complex, New Zealand						2019 Mar 28, 23:27
R3D2 (Radio Frequency Risk Reduction Deployment Demonstration) 2019-016A 44073						Re-entered - 2021 May 23 Life 787 days
Small satellite from US Defense Advanced Research Projects Agency to space-qualify a kapton radio reflector for use as part of a radio aerial.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Mar 29, 21:38	6808	0.0012	422	438	93.18	39.52	276

Electron third stage (kick stage) 2019-016B 44074						Re-entered - 2021 Jun 25 Life 820 days
Launched R3D2.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Mar 29, 23:10	6804	0.0015	415	436	93.09	39.52	290

Electron second stage 2019-016C 44075						Re-entered - 2019 Apr 15 Life 18 days
Launched R3D2.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Mar 29, 05:59	6696	0.0175	201	435	90.89	39.52	265

2019-020 Soyuz ST-B + Fregat-MT (VS-22) Centre Spatiale Guyanaise						2019 Apr 4, 17:03
O3b FM20 2019-020A 44112						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Apr 05, 14:22	14203	0.0010	7810	7839	280.74	0.04	173

O3b FM19 2019-020B 44113						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Apr 05, 14:22	14207	0.0008	7818	7839	280.87	0.04	177

O3b FM17 2019-020C 44114						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Apr 05, 14:23	14213	0.0004	7830	7840	281.05	0.04	147

O3b FM18 2019-020D 44115						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Apr 05, 14:23	14218	0.0001	7838	7841	281.20	0.04	52

2019-022 Antares 230 Wallops Flight Facility						2019 Apr 17, 20:46
Cygnus NG-11 (SS Roger Chaffee) 2019-022A 44188						Re-entered - 2019 Dec 6 Life 233 days
Northrop Grumman vehicle carrying supplies to ISS. Captured by RMS Remote Manipulator Apr 19, 0928 UTC, docked with downward- facing port of Unity at 11:31 UTC. Undocked Aug 6 at 13:30 UTC, released from Remote Manipulator at 16:15 UTC. Launched several Cubesats after departing ISS. Destructive re-entry above the southern Pacific Ocean 2019 Dec 6, probably at around 16:55 UTC followed retrofire about 40 minutes earlier.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Apr 17, 22:24	6711	0.0071	285	380	91.18	51.64	305
2019 Apr 18, 20:48	6780	0.0002	401	403	92.60	51.63	228
2019 Apr 18, 22:21	6782	0.0001	403	404	92.64	51.64	85
2019 Apr 19, 07:52	6783	0.0007	400	410	92.67	51.69	119
2019 Apr 19, 12:21	6787	0.0001	408	410	92.75	51.64	194
2019 Aug 05, 05:22	6792	0.0006	409	418	92.84	51.64	219
2019 Aug 06, 20:59	6825	0.0047	415	479	93.52	51.63	318
2019 Aug 06, 22:33	6853	0.0050	440	509	94.10	51.66	8
2019 Aug 16, 22:23	6853	0.0012	466	483	94.09	51.64	294
2019 Sep 16, 11:48	6852	0.0014	465	484	94.09	51.64	45
2019 Sep 17, 09:43	6842	0.0006	459	468	93.86	51.64	309
2019 Oct 08, 18:30	6844	0.0006	462	470	93.92	51.63	352
2019 Oct 18, 12:53	6794	0.0007	411	421	92.89	51.64	160
2019 Oct 20, 18:19	6844	0.0006	462	470	93.91	51.63	38
2019 Dec 01, 22:20	6844	0.0005	462	469	93.91	51.63	177

Aerocube 10B (Dougsat) 2019-022C 44484						Re-entered - 2023 May 16 Life 1490 days
1.5U Cubesat - released from SS Roger Chaffee after departure from the ISS - equipped with a water powered thruster system and used to demonstrate station keeping and other close manoeuvres in the vicinity of Aerocube 10A.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 14, 23:28	6856	0.0009	472	484	94.17	51.64	285

Aerocube 10A (Jimsat) 2019-022D 44485						Re-entered - 2023 May 4 Life 1478 days
1.5U Cubesat released from SS Roger Chaffee after departure from ISS - carrying a dispenser containing 28 drag spheres to be used for atmosphere density studies. Also equipped with a low power laser diode to be detected by Aerocube 10B during proximity operations.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 10, 01:50	6856	0.0010	472	485	94.17	51.64	271

NARSSCube 2019-022E 44415						Re-entered - 2024 Apr 9 Life 1819 days
0.25U Cubesat released from SS Roger Chaffee after departure from ISS.. One of four launched as a 1U Cubesat stack that were to separated from each other after release from Cygnus. No further ones were catalogued.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 13, 14:30	6856	0.0011	470	485	94.15	51.64	291

Quantum-Radar 3 2019-022F 44416						Re-entered - 2023 Mar 7 Life 1420 days
3U Cubesat released from SS Roger Chaffee after departure from ISS - passive satellite covered with optical reflectors for tracling by students using collimated laser telescopes. Orbit measurements will be used to study satellite decay characteristics and provide data for future Cubesat lifetime estimates.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 13, 11:22	6856	0.0011	470	485	94.15	51.64	290

RFTSat 2019-022G 44417						Re-entered - 2023 Jun 21 Life 1526 days
3U CubeSat from Northwest Nazarene University, Tanpa, Indiana released from SS Roger Chaffee after departure from ISS - to demonstrate the application of radio frequency (RF) energy harvesting and backscatter communication to collecting data from sensors in space. A small RF tag mounted on a boom on the side of the satellite contains a temperature sensor. It is powered by energy emitted from an RF reader inside the satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 14, 09:19	6856	0.0011	470	485	94.15	51.64	292

OrCa 1 (Orbital Calibration) 2019-022H 44418						Re-entered - 2022 Jan 14 Life 1003 days
12U Cubesat from the Georgia Institute of Technology, USA released from SS Roger Chaffee after departure from ISS - designed, built, and tested in a little over six weeks, OrCa is intended to provide optical calibration capabilities for sensors that will, in turn, improve the tracking and identification of space objects.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 13, 14:30	6855	0.0011	469	485	94.15	51.64	290

Aerocube 10A Probe (Venturini) 2019-022J 44516						Re-entered - 2020 Feb 10 Life 299 days
One of 28 aluminium 98mm diameter 'spheres' created from three orthogonal disks. Released from Aerocube 10. The rate of its orbital decay was used to measure atmospheric density. Catalogued 2019 Aug 30.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 29, 14:47	6856	0.0010	472	485	94.17	51.64	345

Seeker 2019-022K 44533						Re-entered - 2023 Dec 5 Life 1693 days
3U Cubesat from NASA released from SS Roger Chaffee after departure from ISS - to demonstrate an ultra-low cost sayellite inspection capability using SS Roger Chaffee as its target.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 16, 23:10	6854	0.0013	466	485	94.11	51.64	33

Aerocube 10A Probe (Gangestad) 2019-022L 45174						Re-entered - 2020 Aug 7 Life 478 days
One of 28 aluminium 98mm diameter 'spheres' created from three orthogonal disks. Released from Aerocube 10. The rate of its orbital decay was used to measure atmospheric density. Catalogued 2020 Feb 14.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 13, 00:13	6854	0.0010	469	483	94.12	51.64	217

Aerocube 10A Probe (Fuller) 2019-022M 45528						Re-entered - 2020 Oct 15 Life 547 days
One of 28 aluminium 98mm diameter 'spheres' created from three orthogonal disks. Released from Aerocube 10. The rate of its orbital decay was used to measure atmospheric density. Catalogued 2020 Apr 22.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Apr 21, 20:35	6852	0.0010	467	481	94.09	51.65	112

Aerocube 10A Probe (Golf) 2019-022N 46928						Re-entered - 2021 Feb 13 Life 668 days
One of 28 aluminium 98mm diameter 'spheres' created from three orthogonal disks. Released from Aerocube 10. The rate of its orbital decay was used to measure atmospheric density. Catalogued 2020 Nov 19.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Nov 19, 02:57	6853	0.0010	469	482	94.11	51.64	116

Aerocube 10A Probe (Jackie) 2019-022P 48156						Re-entered - 2021 Jul 8 Life 813 days
One of 28 aluminium 98mm diameter 'spheres' created from three orthogonal disks. Released from Aerocube 10. The rate of its orbital decay was used to measure atmospheric density. Catalogued 2021 Apr 9.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2021 Apr 08, 08:42	6847	0.0010	462	476	93.98	51.64	286

Antares second stage 2019-022B 44206						Re-entered - 2019 Apr 28 Life 11 days
Launched SS Roger Chaffee (Cygnus NG-11). Initial orbit not published by Space-Track but probably approx 190 x 275 km.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Apr 24, 15:25	6588	0.0032	188	230	88.68	51.61	166

2019-023 CZ 3B Xichang Space Centre						2019 Apr 20, 14:41
Beidou 44 (Beidou-3 IGEO-1) 2019-023A 44204						in space
Phase 2 operational satellite in China's navigation satellite system. It also provides time and messaging services for the Asia-Pacific region from inclined geosynchronous orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Apr 20, 20:37	24369	0.7303	193	35788	630.98	28.47	180
2019 May 01, 16:47	42156	0.0016	35710	35845	1435.65	54.92	184	111° east
2019 Jul 25, 00:32	42163	0.0017	35714	35857	1436.03	55.03	178	115° east
2019 Nov 22, 17:29	42157	0.0016	35712	35845	1435.69	55.20	186	112° east
2023 Feb 12, 12:09	42160	0.0021	35692	35871	1435.83	56.92	209	119° east

CZ 3B fourth stage 2019-023B 44205						in space
Launched Beidou-3 IGEO-1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )

2019-024 CZ 4B Taiyuan Space Centre						2019 Apr 29, 22:52
Tianhui 2-01A 2019-024A 44207						in space
Second generation Cartographic and imaging satellite using radar. One of a pair flying close together to undertake stereoscopic imaging using synthetic aperture radar (SAR). Equipped with orbit adjustment engine to maintain formation within a few kilometres of its companion.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Apr 30, 16:14	6889	0.0011	503	519	94.84	97.45	269	05:59
2019 May 08, 12:44	6894	0.0002	514	517	94.94	97.45	82	05:59
2021 Aug 19, 03:12	6894	0.0002	514	517	94.94	97.45	95	05:50

Tianhui 2-01B 2019-024C 44209						in space
Second generation Cartographic and imaging satellite using radar. One of a pair flying close together to undertake stereoscopic imaging using synthetic aperture radar (SAR). Equipped with orbit adjustment engine to maintain formation within a few kilometres of its companion.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Apr 30, 17:53	6887	0.0012	501	518	94.81	97.45	282	05:59
2019 May 07, 09:47	6894	0.0001	515	517	94.94	97.45	98	05:59
2021 Aug 16, 18:22	6894	0.0002	514	517	94.94	97.46	91	05:51
2023 Feb 13, 11:49	6894	0.0002	514	517	94.94	97.47	87	05:47

CZ 4B third stage 2019-024D 44210						Re-entered - 2020 Jul 4 Life 432 days
Launched pair of Tianhui2 satellites. Perigee lowered after releasing satellites in order to accelerate decay.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Apr 30, 13:46	6772	0.0173	276	511	92.43	97.53	10

2019-026 Electron (That's a Funny Looking Cactus) Rocket Lab Launch Complex, New Zealand						2019 May 5, 06:00
Falcon ODE ( Falcon Orbital Debris Experiment, AFOTEC-1) 2019-026A 44225						Re-entered - 2024 Mar 20 Life 1781 days
1U Cubesat to provide targets for visual and radar tracking. The plan involved release of two solid metal spheres to act as the actual targets. Their deployment was not announced and neither was Catalogued so success or otherwise is not known.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 May 06, 09:15	6883	0.0010	499	512	94.73	40.01	275

SPARC-1 (Space Plug and play Architecture Research CubeSat) 2019-026B 44226						Re-entered - 2023 Jun 26 Life 1513 days
6U Cubesat from the University of New Mexico - joint US/Sweden payload. US contribution is an Agile Space Radio - a software defined receiver transmitter to demonstrate a range of modulation and encoding techniques. Swedish payload is an imaging system to detect and characterise other objects in orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 May 05, 13:07	6880	0.0013	494	511	94.66	40.03	268

Harbinger 2019-026E 44229						Re-entered - 2024 Mar 9 Life 1770 days
Small satellite sponsored by the US Army Space and Missile Defense Command - equipped with the ICEYE X3 sythetic aperture radar for Earth surface imaging.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 May 06, 08:10	6883	0.0009	498	511	94.71	40.02	276

Electron third stage (kick stage) 2019-026C 44227						Re-entered - 2023 Sep 15 Life 1594 days
Launched Falcon ODE, SPARC 1 and Harbinger.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 May 06, 08:10	6881	0.0011	495	510	94.67	40.03	279

Electron second stage 2019-026D 44228						Re-entered - 2019 May 17 Life 12 days
Launched Falcon ODE, SPARC 1 and Harbinger.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 May 05, 09:32	6723	0.0254	174	515	91.43	40.02	260

2019-027 CZ 3C Xichang Space Centre						2019 May 17, 15:48
Beidou 45 (Beidou-2 G-8) 2019-027A 44231						in space
Phase 1 operational satellite in China's navigation satellite system. It also provides time and messaging services for the Asia-Pacific region from geosynchronous orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 May 18, 07:45	24349	0.7299	198	35743	630.19	19.36	180
2019 May 29, 20:58	42164	0.0003	35773	35799	1436.06	1.85	132	80° east
2023 Feb 13, 05:26	42164	0.0005	35764	35809	1436.07	1.45	144	145° east

CZ 3C upper stage 2019-027B 44232						in space
Launched Beidou-3 G-2.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 May 23, 14:24	23736	0.7223	212	34503	606.56	19.36	183

2019-F04 - failed to reach orbit CZ 4C Taiyuan Space Centre						2019 May 19, 22:49
Yaogan
Radar Earth imaging satellite aimed at sun-synchronous orbit with LTDN 06:00. Lost when the launch vehicle third stage malunctioned. Referred to as Yaogan 33 in Chinese launch announcement in what may have been a bureaucratic error as the name was subsequently re-used in a later launch of a different design of satellite.

2019-030 Soyuz-2 1B + Fregat Plesetsk Cosmodrome						2019 May 27, 06:23
Cosmos 2534 (Uragan-M № 758) 2019-030A 44299						in space
GLONASS-M navigation satellite to fill a space in the constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 May 29, 17:40	25520	0.0005	19128	19156	676.21	64.79	259
2019 Jun 04, 12:20	25551	0.0007	19155	19190	677.42	64.79	50
2019 Jun 15, 22:00	25508	0.0012	19099	19161	675.73	64.79	287

Fregat rocket stage 2019-030B 44300						in space
Mission information in preparation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )

2019-032 CZ 11H Towed barge 'Tai Rui', Yellow Sea - 34°.9 N, 121.2 E						2019 Jun 5, 04:06
Jilin-1 High Resolution 03A (Jilin-1 GF03A) 2019-032A 44310						in space
Chinese high resolution, multi-spectral imaging satellite. Catalogue Number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 07, 08:19	6945	0.0014	557	576	96.00	44.99	308
2022 May 01, 03:03	6945	0.0011	560	575	96.01	44.98	74

Tianqi 3 2019-032B 44311						in space
6U Cubesat? - comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 07, 11:31	6944	0.0014	556	576	95.98	44.98	315
2022 May 01, 03:46	6940	0.0013	553	571	95.89	44.98	73

Xiaoxiang-1 04 2019-032C 44312						in space
Full-color miniature remote sensing camera. Remote sensing imaging technology verification based on industrial lens + commercial high performance detector. 7.2m resolution RGB remote sensing camera
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 07, 09:55	6944	0.0014	556	576	95.98	44.99	317
2022 May 01, 03:11	6939	0.0012	553	570	95.88	44.99	72

Tianxiang 1 2019-032D 44313						in space
Test satellite to demonstrate Ka-band communications in space. Catalogue Number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 07, 09:54	6944	0.0015	555	576	95.97	45.00	315
2022 May 01, 04:28	6938	0.0014	551	569	95.86	45.00	69

Tianxiang 2 2019-032E 44314						in space
Test satellite to demonstrate Ka-band communications in space. Catalogue Number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 07, 11:30	6943	0.0016	554	576	95.97	44.99	314
2022 May 01, 03:04	6939	0.0014	551	571	95.88	44.99	72

Bufeng 1A (Wind Catcher 1A) 2019-032F 44315						in space
Small satellite to monitor ocean wind fields and wave heights/patterns to improve typhoon monitoring. Its detectors use reflected MEO navsat transmissions to measure wave height and speed. Catalogue Number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 07, 08:17	6942	0.0017	552	576	95.93	44.98	317
2022 May 01, 03:09	6937	0.0016	548	569	95.83	44.98	82

Bufeng 1B (Wind Catcher 1C) 2019-032G 44316						in space
Small satellite to monitor ocean wind fields and wave heights/patterns to improve typhoon monitoring. Its detectors use reflected MEO navsat transmissions to measure wave height and speed. Catalogue Number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 07, 11:31	6945	0.0013	557	576	96.00	44.99	307
2022 May 01, 02:41	6945	0.0016	556	578	96.01	44.98	62

CZ 11 fourth stage 2019-032H 44317						Re-entered - 2021 Mar 12 Life 646 days
Launched Jilin-1 HR 03A and six other satellites. An eighth satellite remained attached to the upper stage because of fault detected shortly before launch. A decision was made not to release it.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 07, 14:49	6830	0.0266	270	634	93.62	44.92	314

2019-035 CZ 3B Xichang Space Centre						2019 Jun 24, 18:09
Beidou 46 (Beidou-3 IGEO-2) 2019-035A 44337						in space
Phase 2 operational satellite in China's navigation satellite system. It also provides time and messaging services for the Asia-Pacific region from inclined geosynchronous orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Jun 25, 04:49	24380	0.7305	193	35812	631.42	28.58	180
2019 Jul 05, 14:00	42159	0.0012	35730	35831	1435.80	55.05	186	106° east
2019 Aug 31, 18:34	42163	0.0012	35735	35835	1436.01	55.05	183	108° east
2023 Feb 12, 20:01	42161	0.0030	35658	35908	1435.92	55.14	194	119° east

CZ 3B fourth stage 2019-035B 44338						Re-entered - 2019 Oct 22 Life 120 days
Mission information in preparation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )

2019-037 Electron (Make It Rain) Rocket Lab Launch Complex, New Zealand						2019 Jun 29, 04:30
Painani 1 2019-037A 44365						Re-entered - 2023 Jan 14 Life 1295 days
3U Cubesat owned by Mexico's Ministry of National Defense (Sedena). It is equipped with infrared sensors capable of imaging the Earth's surface and measuring its temperature.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 30, 02:55	6834	0.0007	451	461	93.71	45.01	290

Prometheus 2-9 2019-037B 44366						Re-entered - 2022 Jun 6 Life 1073 days
1.5U Cubesat in the Prometheus programme, launched as one of a pair. Prometheus Block 2 satellites act as a host for separately-produced payloads. This is one of two similar satellites on the same launch, carrying an unspecified payload for the US Special Operations Command (SOCOM) to demonstrate satellites working together. May actually be a 3U Cubesat with the hosted SOCOM equipment carried in a 1.5U compartment.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 30, 09:09	6832	0.0010	448	461	93.67	45.01	279

BlackSky 3 (Global 3) 2019-037C 44367						Re-entered - 2023 May 16 Life 1417 days
Commercial multi-spectral Earth imaging satellite from BlackSky Global inc.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 30, 10:42	6832	0.0011	446	461	93.66	45.01	278

ACRUX 1 2019-037E 44369						Re-entered - 2022 Jun 17 Life 1084 days
1U Cubesat - built by the University of Melbourne, Australia as an educational project under the Melbourne Space Program.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 30, 10:40	6827	0.0016	438	460	93.57	45.01	270

SpaceBEE 9 2019-037F 44370						Re-entered - 2021 Dec 16 Life 901 days
0.25U Cubesat from Swarm Technologies for two-way communications system in LEO. Swarm intends to operate a 150 satellite constellation. It also carries a GPS receiver to help determine its location.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 30, 07:33	6827	0.0017	437	460	93.56	45.01	267

SpaceBEE 8 2019-037G 44371						Re-entered - 2021 Apr 26 Life 667 days
0.25U Cubesat from Swarm Technologies for two-way communications system in LEO. Swarm intends to operate a 150 satellite constellation. It also carries a GPS receiver to help determine its location.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 30, 12:14	6827	0.0017	437	460	93.56	45.01	271

Prometheus 2-7 2019-037K 44374						Re-entered - 2022 May 20 Life 1056 days
1.5U Cubesat in the Prometheus programme, launched as one of a pair. Prometheus Block 2 satellites act as a host for separately-produced payloads. This is one of two similar satellites on the same launch, carrying an unspecified payload for the US Special Operations Command (SOCOM) to demonstrate satellites working together. May actually be a 3U Cubesat with the hosted SOCOM equipment carried in a 1.5U compartment.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 01, 10:06	6832	0.0010	448	461	93.67	45.01	285

Electron third stage (kick stage) 2019-037D 44368						Re-entered - 2022 Apr 14 Life 1020 days
Launched cluster of satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 30, 06:00	6828	0.0016	439	461	93.58	45.01	276

Electron second stage 2019-037H 44372						Re-entered - 2020 Mar 16 Life 261 days
Launched cluster of satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 30, 05:36	6755	0.0120	295	458	92.08	45.01	248

2019-I08 Nanoracks Cubesat Deployer International Space Station						2019 Jul 3, 10:15
GEMS (Global Environmental Monitoring System) 1998-067QK 44385						Re-entered - 2021 Apr 3 Life 640 days
3U Cubesat equipped with microwave radiometer i to capture 3D temperature and moisture atmospheric profiles. IOD (In Orbit Demonstration System) launch from Orbital Micro Systems.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 09, 18:42	6790	0.0004	409	414	92.80	51.64	119

2019-I09 Nanoracks Cubesat Deployer International Space Station						2019 Jul 3, 11:50
KRAKsat 1998-067QL 44426						Re-entered - 2021 Mar 14 Life 620 days
1U Cubesat - produced students at the AGH University of Science and Technology, Kraków, carrying an experiment to investigate the use of ferrofluid (powdered metal) as a flywheel. Its storage batteries failed to hold a charge from the the solar cells.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 14, 06:55	6790	0.0006	408	416	92.80	51.65	114

Światowid 1998-067QM 44427						Re-entered - 2020 Jan 18 Life 199 days
2U Cubesat from Poland, carrying a high resolution Earth imaging system.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 13, 20:06	6790	0.0005	409	415	92.81	51.64	126

2019-I10 Nanoracks Cubesat Deployer International Space Station						2019 Jul 3, 14:50
VCC A (Virginia Cubesat Constellation A) 1998-067QN 44428						Re-entered - 2021 Oct 18 Life 838 days
1U Cubesat - One of a set of three launched simultaneously to provide measurements of orbit decay. Each was equipped with a drag device to cause re-entry at the end of mission. Built by a consortium of universities in the state of Virginia, USA. All three reportedly failed to activate on release into orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 14, 17:42	6790	0.0003	409	414	92.79	51.64	140

VCC C (Virginia Cubesat Constellation C) 1998-067QQ 44430						Re-entered - 2021 May 15 Life 682 days
1U Cubesat - One of a set of three launched simultaneously to provide measurements of orbit decay. Each was equipped with a drag device to cause re-entry at the end of mission. Built by a consortium of universities in the state of Virginia, USA. All three reportedly failed to activate on release into orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 13, 21:37	6790	0.0003	409	414	92.79	51.64	140

VCC B (Virginia Cubesat Constellation B) 1998-067QR 44431						Re-entered - 2021 Oct 13 Life 833 days
1U Cubesat - One of a set of three launched simultaneously to provide measurements of orbit decay. Each was equipped with a drag device to cause re-entry at the end of mission. Built by a consortium of universities in the state of Virginia, USA. All three reportedly failed to activate on release into orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 14, 13:05	6790	0.0004	409	414	92.80	51.64	148

2019-I11 Nanoracks Cubesat Deployer International Space Station						2019 Jul 3, 16:25
Entrysat 1998-067QP 44429						Re-entered - 2021 Aug 10 Life 769 days
3U Cubesat from ISAE-SUPAERO and funded by CNES, France - designed to study the behaviour of a piece of space debris in orbit and in the first minutes of re-entry. Communication with ground stations was never established after. release from ISS.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 14, 16:10	6789	0.0003	409	414	92.79	51.64	137

2019-038 Soyuz-2 1B + Fregat Vostochny Cosmodrome						2019 Jul 5, 05:41
Meteor M2-2 2019-038A 44387						in space
Meteorological satellite providing global observations of the Earth's surface and its atmosphere. The data acquired by the satellite is used for weather analysis and forecasting, climate change monitoring, sea water monitoring and forecasting, and space weather analysis and prediction.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Jul 05, 21:02	7192	0.0003	812	816	101.17	98.57	85	03:05
2019 Dec 17, 20:21	7192	0.0001	813	815	101.17	98.59	5	02:58
2019 Dec 18, 11:32	7191	0.0002	811	815	101.15	98.59	62	02:58
2023 Feb 13, 11:40	7191	0.0001	812	813	101.14	98.76	355	03:02

2019-039 Soyuz-2 1V +Volga Plesetsk Cosmodrome						2019 Jul 10, 17:14
Cosmos 2535 2019-039A 44421						in space
Military satellite, one of four carried on the launch. Used to test an on-orbit satellite servicing system, making close approaches to, and possibly attaching itself to, Cosmos 2538
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Jul 12, 09:52	6995	0.0008	611	622	97.03	97.88	298	09:01
2019 Jul 18, 20:46	6995	0.0008	611	622	97.03	97.88	275	09:01
2019 Jul 19, 21:03	6995	0.0008	611	622	97.03	97.88	272	09:01
2019 Jul 20, 16:27	6994	0.0008	611	622	97.02	97.88	259	09:01
2019 Jul 21, 02:10	6994	0.0007	611	621	97.02	97.88	262	09:01
2019 Jul 21, 21:35	6994	0.0007	611	621	97.03	97.88	259	09:01
2019 Jul 23, 10:48	6996	0.0008	612	623	97.05	97.88	285	09:01
2019 Jul 24, 11:37	6994	0.0010	609	623	97.02	97.88	282	09:01
2019 Aug 02, 19:58	6994	0.0011	608	623	97.01	97.88	240	09:01
2019 Sep 30, 17:57	6992	0.0012	606	623	96.98	97.87	51	09:02
2019 Oct 09, 18:40	6989	0.0009	605	617	96.91	97.86	357	09:02

Cosmos 2536 2019-039B 44422						Re-entered - 2024 Jun 21 Life 1808 days
Military satellite, one of four carried on the launch. Purpose unknown.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Jul 12, 09:51	6995	0.0008	611	622	97.03	97.87	310	09:01

Cosmos 2537 2019-039C 44423						Re-entered - 2023 Oct 7 Life 1550 days
Military satellite, one of four carried on the launch. Purpose unknown.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Jul 12, 10:19	6996	0.0009	612	624	97.06	97.89	300	09:01

Cosmos 2538 2019-039D 44424						in space
Military satellite, one of four carried on the launch. Used to test an on-orbit satellite servicing system, making close approaches to, and possibly attaching itself to, Cosmos 2535. Work appeared to be completed by 2022 Sep 14 when orbit was lowered, taking it away from Cosmos 2535.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Jul 12, 09:45	6998	0.0005	616	623	97.10	97.88	287	09:01
2019 Jul 16, 18:43	6999	0.0006	616	625	97.12	97.89	252	09:01
2019 Jul 17, 02:49	6999	0.0006	617	625	97.12	97.88	262	09:01
2019 Jul 17, 12:32	6999	0.0005	617	625	97.12	97.88	260	09:01
2019 Jul 26, 10:19	6987	0.0021	594	624	96.88	97.88	253	09:01
2019 Jul 26, 18:48	6976	0.0006	593	602	96.64	97.88	287	09:01
2019 Jul 29, 16:14	6985	0.0012	599	615	96.83	97.87	178	09:01
2019 Jul 30, 09:45	6994	0.0010	609	623	97.02	97.88	255	09:01
2019 Aug 14, 13:28	6992	0.0008	608	619	96.97	97.87	200	09:01
2019 Aug 15, 02:33	6998	0.0018	607	632	97.09	97.89	202	09:01
2019 Aug 15, 10:56	6994	0.0012	607	624	97.01	97.88	198	09:01
2019 Sep 11, 19:54	6995	0.0011	609	625	97.04	97.89	108	09:02
2019 Sep 15, 17:10	6994	0.0013	607	625	97.02	97.87	102	09:02
2019 Sep 19, 22:17	6991	0.0012	605	621	96.96	97.88	99	09:02
2019 Sep 20, 20:07	6994	0.0013	606	625	97.02	97.87	83	09:02
2019 Oct 02, 12:00	6992	0.0010	607	621	96.98	97.87	52	09:02
2019 Nov 28, 15:34	6983	0.0020	591	619	96.78	97.86	185	09:02
2019 Dec 05, 22:47	6989	0.0010	604	618	96.91	97.86	154	09:03
2019 Dec 13, 18:16	6989	0.0010	604	618	96.91	97.86	130	09:03
2019 Dec 18, 19:28	6989	0.0010	603	618	96.91	97.86	116	09:03
2019 Dec 20, 16:43	6989	0.0010	603	618	96.91	97.86	111	09:03
2021 Sep 14, 16:38	6974	0.0036	571	621	96.60	97.93	179	09:07
2021 Sep 15, 14:23	6950	0.0062	528	614	96.09	97.81	200	09:08
2023 Mar 26, 03:52	6942	0.0057	524	604	95.94	97.73	125	09:38

Volga rocket body 2019-039E 44425						in space
Launched Cosmos 2535 - Cosmos 2538.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 12, 18:34	6871	0.0026	475	511	94.46	97.61	71

2019-040 Proton-M + Blok DM3 Baikonur Cosmodrome						2019 Jul 12, 12:30
Spektr RG (Spektr Roentgen-Gamma) 2019-040A 44432						Re-entered - 2019 Jul 13 Life 1 day
Joint Russian and German high-energy astrophysics observatory carrying a German x-ray telescope to map galaxy clusters, and a Russian x-ray telescope to search for supermassive black holes. Arrived L-2 2019 Oct 21.
Halo orbit around the Sun-Earth L-2 Lagrange Point

Blok DM-03 rocket stage 2019-040B 44433						Re-entered - 2019 Jul 13 Life 1 day
Launched Spektr RG.
Heliocentric orbit

2019-041 Soyuz FG Baikonur Cosmodrome						2019 Jul 20, 16:28
Soyuz MS-13 (Soyuz 11F732A48 № 743) 2019-041A 44437						Re-entered - 2020 Feb 6 Life 201 days Returned to Earth
Carrying crew to ISS - Alexandr Skortsov (Roscosmos), Luca Parmatiano (ESA) and Andrew Morgan (NASA). Precise launch time 16:28:21 UTC. Docked with the aft port of Zvezda Jul 20 at 22:47:50 UTC. Undocked, carrying its original crew, Aug 26 at 03:35 UTC and re-docked under manual control with the Poisk module at 03:59 UTC in order to allow Soyuz MS-14 to use Zvezda after its aborted docking with Poisk. Undocked 2020 Feb 6, 08:50 UTC carrying Skortsov, Parmatiano and Christina Koch (NASA). Retro-fire at 08:18 OTC led to landing shortly before 09:13 UTC approx 150 km SE of Dzhezkazgan in Kazakhstan.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 20, 18:31	6641	0.0009	257	269	89.77	51.60	72
2019 Jul 20, 21:04	6792	0.0007	409	418	92.84	51.64	161

Soyuz upper stage 2019-041B 44438						Re-entered - 2019 Jul 24 Life 4 days
Launched Soyuz MS-13.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 20, 20:41	6577	0.0005	196	202	88.47	51.61	87

2019-042 GSLV Mk III M1 Satish Dhawan Space Centre						2019 Jul 22, 09:13
Chandrayaan 2 2019-042A 44441						Re-entered - 2019 Sep 6 Life 46 days
Indian lunar orbiter, carried 'Vikram' lunar lander. Used five engine firing starting Jul 24 to raise its orbit before entering Barycentric orbit Aug 13. Retro-fire Aug 20 at 03:32 UTC placed it into lunar orbit. Four further firings lowered the orbit to operational height for release of Vikram on Sep 2. Chandrayaan then began its own lunar exploration mission from orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 24, 05:28	29046	0.7758	133	45203	821.08	21.43	179
2019 Jul 26, 15:10	33860	0.8057	202	54762	1033.47	21.42	181
2019 Aug 01, 20:31	42280	0.8409	348	71456	1442.00	21.06	183
2019 Aug 06, 09:36	51042	0.8699	264	89064	1912.72	21.56	185
2019 Aug 13, 21:07	78528	0.9148	313	143986	3650.00	21.67	186
2019 Aug 18, 00:00	208216	0.9751	-1201	404877	15759.08	21.81	184
2019 Aug 18, 00:00	208216	0.9751	-1201	404877	15759.08	21.81	184

Vikram Lunar Lander						in space
Indian lunar landing vehicle carrying 'Pragyan' lunar rover. Separated from Chandrayaan 2 Sep 2 at 0745 UTC. Three retro-firings Sep 3 at 03:20 UTC and 22:12 UTC, and Sep 6 at 20:08 UTC set it on course for landing but it crashed on the lunar surface at 20:23 UTC.
Impacted on the Moon

GSLV third stage 2019-042B 44442						Re-entered - 2019 Oct 16 Life 86 days
Launched Chandrayaan 2.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 24, 23:02	29034	0.7753	145	45167	820.57	21.41	180

2019-043 Hyperbola 1 (Y1) Jiuquan Space Centre						2019 Jul 25, 05:00
CAS 7B + BP-1B (China Amateur radio Satellite) 2019-043A 44443						Re-entered - 2019 Aug 6 Life 12 days
1.5U Cubesat - combined payload consisting of an amateur radio transponder package and telemetry transmitter (CAS-7B) and a balloon experiment to increase air drag and accelerate orbit decay (BP-1B).
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 25, 15:38	6668	0.0014	280	299	90.31	42.72	279

Hyperbola 1 fourth stage uncatalogued						Re-entered - 2019 Jul 25 Life <1 day
Launched CAS-7. Also carried three experimental payloads that remained attached to it alongside two ballast items carrying commercial advertisements. Re-entered soon after releasing satellite and not catalogued.
Not Catalogued - orbit parameters unavailable

2019-044 Falcon 9 Block 5 Cape Canaveral Air Force Station						2019 Jul 25, 22:01
SpaceX Dragon CRS-18 2019-044A 44446						Re-entered - 2019 Aug 27 Life 33 days Returned to Earth
Carrying a cargo to the ISS under NASA's Commercial Resupply Services (CRS) contract. Captured by the ISS Remote Manipulator System July 27 at 13:11 UTC and attached to the lower port of the Harmony module at 16:01 UTC. Undocked using the RMS Aug 27 at 12:25 UTC. Released 14:59 UTC. Retro-fire led to splashdown at 20:20 UTC in the Pacific Ocean, about 300 km SW of Baja, California.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 26, 00:59	6673	0.0138	203	387	90.41	51.63	49
2019 Jul 26, 23:34	6666	0.0127	203	373	90.28	51.64	53
2019 Jul 27, 05:34	6664	0.0126	203	370	90.24	51.65	54
2019 Jul 27, 13:31	6792	0.0006	409	418	92.84	51.64	184
2019 Aug 27, 12:22	6794	0.0008	410	421	92.88	51.64	333
2019 Aug 27, 17:12	6784	0.0013	397	414	92.67	51.65	283

Falcon 9 upper stage uncatalogued						Re-entered - 2019 Jul 25 Life <1 day
Launched Dragon CRS-18. Caused to re-enter soon after releasing payload, not catalogued.
Not Catalogued - orbit parameters unavailable

2019-045 CZ 2C Xichang Space Centre						2019 Jul 26, 03:57
Yaogan 30-05A 2019-045A 44449						in space
One of a triplet of simultaneously-launched satellites described as being for "electromagnetic environment detection and related technological tests”. That may indicate they are electronic intelligence gathering satellites. The three satellites are spaced at 120º intervals around the orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 26, 15:38	6975	0.0012	588	605	96.62	35.00	304
2019 Jul 31, 12:13	6985	0.0007	602	611	96.82	35.00	328
2019 Aug 15, 03:15	6977	0.0004	596	602	96.67	35.00	318
2023 Feb 13, 13:15	6972	0.0004	591	596	96.55	35.00	145

Yaogan 30-05B 2019-045B 44450						in space
One of a triplet of simultaneously-launched satellites described as being for "electromagnetic environment detection and related technological tests”. That may indicate they are electronic intelligence gathering satellites. The three satellites are spaced at 120º intervals around the orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 26, 17:56	6975	0.0011	589	605	96.62	35.00	302
2019 Jul 29, 18:55	6976	0.0010	591	605	96.64	35.00	325
2019 Aug 12, 00:43	6977	0.0010	592	606	96.66	34.99	84
2023 Feb 13, 04:38	6972	0.0010	586	601	96.55	34.99	286

Yaogan 30-05C 2019-045C 44451						in space
One of a triplet of simultaneously-launched satellites described as being for "electromagnetic environment detection and related technological tests”. That may indicate they are electronic intelligence gathering satellites. The three satellites are spaced at 120º intervals around the orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 26, 17:56	6975	0.0011	589	604	96.61	35.00	302
2019 Jul 30, 16:45	6967	0.0009	583	595	96.45	35.00	336
2019 Aug 14, 08:29	6977	0.0001	598	600	96.67	35.00	145
2023 Feb 13, 10:34	6972	0.0002	592	595	96.55	35.00	305

CZ 2C second stage 2019-045D 44452						in space
Launched cluster of three Yaogan-30 satellites. Perigee lowered after satellite release.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 28, 18:49	6903	0.0103	454	597	95.14	34.98	65

2019-I07 Dextre Arm + Kaber Micro Satellite Deployer International Space Station						2019 Jul 27, 20:05
RedEye 1 (Pinot) 1998-067QJ 44364						Re-entered - 2022 Jul 24 Life 1093 days
Small satellite from DARPA, possibly for testing inter-satellite communication links.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 28, 09:21	6791	0.0008	407	418	92.82	51.64	85

2019-046 Soyuz-2 1A + Fregat Plesetsk Cosmodrome						2019 Jul 30, 05:57
Meridian 8 (Meridian № 18L) 2019-046A 44453						in space
HEO military/government comsat to support Russian forces, commercial shipping and communication ground stations at northern latitudes across Russia. First mission for the Meridian-M version. Meridian also supports the clandestine short messaging system formerly provided by the Parus satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 01, 14:38	26738	0.7246	985	39734	725.19	62.81	270
2019 Aug 19, 14:00	26555	0.7225	990	39364	717.76	62.79	270

Fregat rocket stage 2019-046B 44454						in space
Launched Meridian 8.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 09, 05:05	26575	0.7297	805	39588	718.56	62.75	270

Soyuz upper stage uncatalogued						Re-entered - 2019 Jul 30 Life <1 day
Launched Meridian 8. Re-entered naturally over southern Indian Ocean about 1 hr after launch before completing first orbit.
Not Catalogued - orbit parameters unavailable

2019-047 Soyuz-2 1A Baikonur Cosmodrome						2019 Jul 31, 12:10
Progress MS-12 (Progress 7K-MS №442) 2019-047A 44455						Re-entered - 2019 Nov 29 Life 121 days
Supplies to ISS. Precise launch time 12:10:46 UTC. Docked with the port on Pirs 2019 Jul 31 at 15:29 UTC. Undocked 2019 Nov 28 at 10:25 UTC. Retro-fire at 13:39 UTC led to destructive re-entry above the southern Pacific Ocean at 14:11 UTC. Any surviving fragments hit the ocean surface about eight minutes later.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 31, 07:53	6792	0.0006	409	418	92.84	51.64	199

Soyuz upper stage 2019-047B 44456						Re-entered - 2019 Aug 4 Life 4 days
Launched Progress MS-12.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 31, 22:19	6578	0.0022	185	215	88.50	51.61	69

2019-048 Proton-M + Briz-M Baikonur Cosmodrome						2019 Aug 5, 21:56
Cosmos 2539 (Blagovest, 14F149 № 14L) 2019-048A 44457						in space
Russian military and civilian communications satellite providing high-speed internet, data communications, television and radio broadcasting, telephony and videoconferencing services.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 13, 23:08	42102	0.0027	35610	35837	1432.87	0.04	306	63° east
2019 Aug 15, 18:13	42143	0.0021	35676	35854	1435.01	0.03	309	64° east
2019 Aug 16, 13:10	42158	0.0017	35707	35853	1435.74	0.03	303	64° east
2019 Aug 21, 07:12	42281	0.0008	35867	35938	1442.02	0.01	121	60° east
2019 Aug 30, 11:19	42197	0.0006	35793	35846	1437.76	0.01	326	45° east
2019 Aug 30, 22:25	42179	0.0004	35785	35816	1436.81	0.01	290	45° east
2019 Aug 31, 04:30	42177	0.0004	35780	35818	1436.73	0.02	294	45° east
2023 Feb 13, 08:28	42164	0.0001	35782	35789	1436.05	0.05	306	12° east

Briz-M rocket stage 2019-049B 44458						in space
Launched Cosmos 2539. Orbit raised after releasing the satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 17:56	45223	0.0712	35625	42066	1595.16	0.16	157

Briz-M propellant tank 2019-049C 44459						in space
Auxilliary propellant tank discarded by Briz-M that launched Cosmos 2539.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 17, 17:29	24429	0.7229	390	35711	633.30	48.71	3

2019-049 Ariane 5ECA (VA-249) Centre Spatiale Guyanaise						2019 Aug 6, 19:30
EDRS-C (European Data Relay Satellite) 2019-049A 44475						in space
Second satellite in EDRS to provide point to point communications including to/from other satellites including the ISS. Brought into service 2020 Jan 23.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 08, 08:02	24400	0.7291	232	35812	632.19	4.47	179
2019 Aug 13, 09:32	39141	0.0775	29730	35797	1284.44	0.16	194
2019 Aug 14, 07:39	40657	0.0371	32770	35787	1359.75	0.13	180
2019 Aug 16, 04:20	42154	0.0003	35765	35787	1435.54	0.07	353	18° east
2019 Aug 19, 00:57	42073	0.0008	35661	35729	1431.42	0.08	195	19° east
2019 Aug 23, 05:11	42141	0.0006	35738	35787	1434.89	0.10	358	22° east
2019 Aug 25, 20:57	42165	0.0001	35784	35789	1436.09	0.09	222	21° east
2019 Nov 26, 20:02	42164	0.0001	35782	35788	1436.03	0.04	324	21° east
2019 Nov 27, 05:58	42069	0.0001	35688	35694	1431.21	0.04	71	22° east
2019 Dec 06, 21:59	42165	0.0001	35783	35791	1436.12	0.01	250	31° east
2023 Feb 12, 12:26	42165	0.0000	35785	35789	1436.13	0.08	24	31° east

HYLAS 3 (Highly Adaptable Satellite 3) 2019-049A						in space
Comsat to provide high speed links to Europe, Africa and the Middle East. Expected location 31° east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )

Intelsat 39 2019-049B 44476						in space
Commercial comsat providing video distribution and broadband connections to customers across Africa, Asia, Europe, the Middle East and Asia. Expected location - 29° east to replace Intelsat 902.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 08, 10:58	26530	0.5889	4527	35776	716.73	2.86	178
2019 Aug 10, 02:44	30590	0.3781	12647	35776	887.41	1.55	177
2019 Aug 11, 23:48	41078	0.0257	33645	35754	1380.92	0.38	172
2019 Aug 19, 18:14	41266	0.0234	33923	35853	1390.43	0.38	171
2019 Aug 27, 00:46	42199	0.0006	35794	35848	1437.86	0.11	297	78° east
2019 Aug 29, 14:24	42177	0.0006	35775	35822	1436.71	0.05	29	55° east
2019 Sep 26, 05:05	42165	0.0001	35783	35791	1436.12	0.03	49	55° east
2019 Sep 30, 19:19	42095	0.0001	35713	35721	1432.53	0.04	30	59° east
2019 Oct 04, 20:16	42113	0.0004	35719	35752	1433.48	0.03	242	62° east
2019 Oct 07, 20:24	42163	0.0001	35781	35790	1436.03	0.03	105	62° east
2023 Feb 12, 18:27	42165	0.0002	35780	35794	1436.11	0.02	33	62° east

Ariane 5 upper stage 2019-049C 44477						in space
Launched Intelsat 39 and EDRS-C
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 08, 18:39	24251	0.7280	217	35528	626.40	4.55	181

2019-050 Falcon 9 Block 5 Cape Canaveral Air Force Station						2019 Aug 6, 23:23
Amos 17 2019-050A 44479						in space
Israeli comsat covering Africa, Europe and the Middle East. Expected location - 17° east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 08, 05:56	24354	0.7292	217	35734	630.39	26.01	178
2019 Aug 10, 14:40	25907	0.6266	3295	35763	691.65	16.69	179
2019 Aug 12, 11:58	33372	0.2631	18214	35774	1011.20	4.02	178
2019 Aug 12, 20:22	38964	0.0818	29399	35773	1275.71	0.95	173
2019 Aug 15, 04:11	41705	0.0112	34861	35793	1412.68	0.09	94	12° east
2019 Aug 15, 17:58	42273	0.0020	35809	35979	1441.61	0.17	305	14° east
2019 Aug 19, 15:00	42166	0.0002	35781	35794	1436.15	0.17	292	14° east
2023 Feb 12, 19:57	42164	0.0002	35778	35795	1436.07	0.02	220	17° east

Falcon 9 upper stage 2019-060B 44480						in space
Launched Amos 17.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 08, 02:22	24342	0.7292	214	35714	629.95	26.03	178

2019-051 Atlas V 551 Cape Canaveral Air Force Station						2019 Aug 8, 10:13
USA 292 (AEHF 5) 2019-051A 44481						in space
Advanced Extremely High Frequency US military and government communications satellite. Lift-off was 29 minutes into the launch window after a short delay. Separated from the launch vehicle at 15:53 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 09, 15:38	31204	0.3352	14366	35287	914.29	9.99	180
2019 Aug 11, 16:08	33218	0.2749	17709	35971	1004.22	9.48	180
2019 Aug 16, 23:19	36458	0.1430	24865	35295	1154.65	8.15	181
2019 Aug 28, 15:15	36812	0.1280	25723	35146	1171.52	7.91	180
2019 Sep 09, 18:00	37412	0.1052	27098	34970	1200.27	7.71	179
2019 Oct 22, 20:51	40258	0.0492	31900	35859	1339.78	6.97	182
2019 Nov 04, 03:15	41441	0.0365	33549	36577	1399.28	6.76	186
2019 Nov 07, 13:09	41741	0.0322	34017	36708	1414.49	6.70	185	119° west
2019 Nov 11, 23:43	41997	0.0226	34670	36569	1427.55	6.59	185	99° west
2019 Nov 22, 22:27	42167	0.0004	35773	35804	1436.19	6.40	293	94° west
2023 Feb 13, 04:44	42165	0.0050	35575	35999	1436.13	3.79	358	55° east

TDO 1 (Technology Demonstration Orbiter) 2019-051B 44482						Re-entered - 2022 Dec 30 Life 1240 days
12U Cubesat (4x3) - possibly equipped with laser reflectors for visual tracking. Purpose is for calibration of laser-based tracking equipment on the ground.. Separated from launch vehicle at 10:42 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 28, 12:00	24124	0.7268	213	35278	621.49	26.26	193

Atlas V upper stage (Centaur) 2019-051C 44483						in space
Launched AEHF 5 and TDO 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 23, 02:03	30961	0.3466	13853	35313	903.62	9.66	182

2019-052 Jielong 1 (Smart Dragon 1) Jiuquan Space Centre						2019 Aug 17, 04:11
Qiancheng 1(?) 2019-052A 44486						in space
Small imaging satellite for remote sensing, particularly for soil moisture monitoring from Qiansheng Exploration Technology Co. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Aug 18, 21:28	6924	0.0020	532	559	95.56	97.61	245	10:29

Tianqi 2 2019-052B 44487						in space
6U Cubesat? - comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 18, 21:04	6922	0.0021	529	559	95.53	97.61	251

Xingshidai 5 (Star Times 5) 2019-052C 44488						Re-entered - 2024 Nov 19 Life 1921 days
Small Earth observation satellite equipped with visible light and infrared imagers and owned by Chengdu Guoxing Aerospace Technology Co. Includes artificial intelligence software to help pinpoint unusual events on the Earth's surface such as fires. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 18, 21:04	6923	0.0023	529	560	95.54	97.61	248

Jielong 1 upper stage uncatalogued						Re-entered - 2019 Aug 17 Life <1 day
Launched group of three satellites. De-orbited
Not Catalogued - orbit parameters unavailable

2019-053 CZ 3B Xichang Space Centre						2019 Aug 19, 12:03
Chinasat 18 2019-053A 44493						in space
Comsat intended for geosynchronous orbit. Problems detected soon after separation from the launch vehicle left it stranded in transfer orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 20, 19:12	24383	0.7292	224	35785	631.50	28.40	180

CZ 3B fourth stage 2019-053B 44494						Re-entered - 2023 May 27 Life 1377 days
Launched Chinasat 18.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 20, 03:38	23659	0.7230	176	34387	603.62	28.41	179

2019-054 Electron (Look Ma, No Hands) Rocket Lab Launch Complex, New Zealand						2019 Aug 19, 12:12
BRO 1 (Breizh Reconnaissance Orbiter 1) 2019-054A 44495						in space
6U Cubesat (3x2) from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 26, 18:33	6919	0.0013	532	550	95.47	45.02	307

Pearl White 1 2019-054C 44497						in space
6U Cubesat (3x2) - one of a simultaneousl-launched pair on a demonstration mission for USAF Space Command to test new concepts for power, propulsion, communications and controlling air drag. Aimed at one year lifetime, built by Tiger Innovations, Inc.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 20:25	6920	0.0012	534	550	95.48	45.01	283

Pearl White 2 2019-054D 44498						in space
6U Cubesat (3x2) - one of a simultaneousl-launched pair on a demonstration mission for USAF Space Command to test new concepts for power, propulsion, communications and controlling air drag. Aimed at one year lifetime, built by Tiger Innovations, Inc.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 20:25	6919	0.0013	533	550	95.47	45.01	281

BlackSky 4 (Global 4) 2019-054E 44499						in space
Commercial multi-spectral Earth imaging satellite from BlackSky Global inc.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 20:26	6922	0.0010	537	550	95.51	45.01	285

Electron third stage (kick stage) 2019-054B 44496						in space
Launched group of four satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 20:27	6923	0.0009	539	550	95.54	45.01	285

Electron second stage 2019-054F 44500						Re-entered - 2020 Nov 5 Life 444 days
Launched group of four satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 26, 20:20	6799	0.0185	295	547	92.99	45.01	282

2019-055 Soyuz-2 1A Baikonur Cosmodrome						2019 Aug 22, 03:38
Soyuz MS-14 (Soyuz 11F732A48 № 744) 2019-055A 44504						Re-entered - 2019 Sep 6 Life 15 days Returned to Earth
Visit to ISS - carried no crew in a test flight with the Soyuz-2 1a launch vehicle. Precise launch time 06:38:31 UTC. Scheduled automatic docking Aug 24 at 05:32 UT with the Pirs module of ISS was called off when a fault was detected in the Kurs rendezvous system aboard Pirs during the approach. Soyuz MS-14 stood off from the ISS while Aleksandr Skvortsov, Luca Parmitano and Andrew Morgan boarded Soyuz MS-13 and relocated the craft from Zvezda to Pirs using manual control. Soyuz MS-14 docked automatically with the rear port of Zvezda Aug 27 at 03:12 UTC. Undocked 2019 Sep 7 at 18:14 UTC. Retro-fire at 20:37 UTC led to landing in Kazakhstan at 21:32 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 22, 05:39	6588	0.0024	194	226	88.70	51.65	75
2019 Aug 23, 12:49	6670	0.0009	286	297	90.35	51.64	324
2019 Aug 24, 03:29	6667	0.0006	285	293	90.29	51.63	332
2019 Aug 24, 09:53	6795	0.0006	413	420	92.90	51.64	319
2019 Aug 26, 11:39	6794	0.0004	414	418	92.89	51.64	320
2019 Aug 28, 09:57	6794	0.0008	410	421	92.88	51.65	337

Soyuz upper stage 2019-055B 44505						Re-entered - 2019 Aug 26 Life 4 days
Launched Soyuz-MS-14.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 22, 04:09	6584	0.0015	195	216	88.61	51.65	65

2019-056 Delta 4 Medium+ 5,2 Vandenberg Air Force Base						2019 Aug 22, 13:06
USA 293 (GPS IIIA SV02, Magellan) 2019-056A 44506						in space
Block 3 GPS Navsat.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 23, 03:04	17063	0.5561	1195	20174	369.69	55.01	270
2019 Aug 29, 16:33	25325	0.0488	17712	20181	668.47	55.02	270
2019 Sep 03, 21:36	26567	0.0002	20183	20195	718.24	55.02	130

Delta 4 upper stage uncatalogued						Re-entered - 2019 Aug 22 Life <1 day
Launched USA 296. De-orbited soon after releasing satellite, not catalogued.
Not Catalogued - orbit parameters unavailable

2019-057 Rokot + Briz-KM Baikonur Cosmodrome						2019 Aug 30, 14:00
Cosmos 2540 (Geo-IK-2 № 13/Musson 2-3) 2019-057A 44517						in space
Geodetic satellite, based on the GLONASS-M chassis with equipment including radar altimeter, laser retro reflectors and GLONASS receivers. Final use of Rockot launch vehicle.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Aug 31, 03:31	7330	0.0009	945	959	104.10	99.27	316	06:01
2019 Sep 20, 12:36	7321	0.0001	943	943	103.90	99.27	111	06:01
2023 Feb 13, 12:24	7321	0.0000	943	943	103.90	99.25	129	06:18

Briz-KM rocket stage 2019-057B 44518						in space
Launched Cosmos 2540
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 30, 19:18	7188	0.0202	665	955	101.08	99.23	257

2019-058 Kuaizhou 1A Jiuquan Space Centre						2019 Aug 30, 23:41
Xiaoxiang-1 07 2019-058A 44519						in space
6U Cubesat fromTianyi Research Institute - testbed for technology involved in air traffic control from orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 31, 21:42	6979	0.0012	593	609	96.70	97.79	287
2023 Feb 13, 09:59	6958	0.0014	570	590	96.27	97.79	73

Taizhi 1 (KX-09) 2019-058B 44520						in space
Small satellite from the Innovation Academy for Microsatellites of the Chinese Academy of Sciences, conducting microgravity research aimed at detecting gravity waves.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 31, 21:41	6978	0.0011	592	607	96.68	97.79	291
2023 Feb 13, 09:35	6975	0.0013	587	606	96.62	97.79	81

Kuaizhou 1A fourth stage 2019-058C 44521						Re-entered - 2023 Aug 20 Life 1451 days
Launched Xiaoxiang-1 07 and KX-09.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 31, 17:08	6898	0.0244	351	688	95.02	97.80	41

2019-059 CZ 4B Taiyuan Space Centre						2019 Sep 12, 03:26
Ziyuan-1 02D 2019-059A 44528						in space
Remote sensing satellite equipped with a full-color high-resolution multi-spectral camera and a panchromatic camera. Its main tasks include production of images at 1:50,000 scale for use in land resource surveys to monitor disaster prevention measures, disaster mitigation, agriculture, forestry, water conservancy and the environment.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Sep 12, 20:07	7121	0.0012	735	752	99.68	98.58	264	10:30
2019 Sep 13, 17:39	7124	0.0009	739	752	99.73	98.58	267	10:30
2019 Sep 15, 05:47	7146	0.0008	762	774	100.19	98.58	162	10:30
2019 Sep 16, 16:54	7152	0.0001	773	775	100.33	98.58	111	10:30
2023 Feb 13, 10:08	7152	0.0002	773	775	100.32	98.46	110	10:38

Ice Pathfinder (BNU-1) 2019-059B 44529						in space
Small satellite mainly tasked with observing the environmental changes of the Antarctic and Arctic. Carries a multispectral camera; a high-resolution visible-light camera; and an Automatic Identification System AIS) receiver for relaying messages from ships at sea.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 13, 03:48	7120	0.0012	733	750	99.65	98.58	269
2023 Feb 13, 12:56	7118	0.0015	729	751	99.61	98.52	104

Jinniuzuo 1 (Taurus 1) 2019-059C 44530						in space
3U Cubesat from Aerospace System Engineering Research Institute of Shanghai for youth education and amateur radio. Carries an amateur radio payload and is equipped with an experimental solar sail to be deployed later in the mission to accelerate orbit decay.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 13, 12:07	7119	0.0013	732	751	99.64	98.59	271
2023 Feb 13, 10:30	7109	0.0014	720	740	99.41	98.55	112

CZ-4B rocket stage 2019-059D 44531						in space
Launched Ziyun-1 2D and others.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 13, 12:45	6974	0.0204	453	738	96.60	98.68	22

2019-060 CZ 11 Jiuquan Space Centre						2019 Sep 19, 06:42
Zhuhai-1 OVS-03 2019-060A 44534						in space
Commercial Chinese Earth observation satellite using high definition video. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Sep 20, 06:05	6882	0.0013	495	513	94.69	97.40	277	13:00
2019 Oct 20, 04:22	6891	0.0015	502	523	94.88	97.40	197	12:59
2023 Feb 13, 14:01	6861	0.0014	473	492	94.26	97.47	284	13:00

Zhuhai-1 OHS-05 2019-060C 44536						in space
Commercial Chinese Earth observation satellite equipped with high definition, multispectral cameras. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Sep 20, 06:05	6882	0.0012	495	512	94.69	97.40	280	13:00
2019 Oct 20, 10:26	6891	0.0011	505	520	94.88	97.41	193	12:59
2023 Feb 13, 15:06	6861	0.0010	476	490	94.26	97.47	281	13:01

Zhuhai-1 OHS-06 2019-060D 44537						in space
Commercial Chinese Earth observation satellite equipped with high definition, multispectral cameras. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Sep 20, 06:05	6881	0.0013	494	511	94.67	97.40	283	13:00
2019 Oct 20, 10:02	6891	0.0010	506	520	94.88	97.40	212	12:59
2023 Feb 13, 11:43	6861	0.0009	477	489	94.26	97.46	305	12:57

Zhuhai-1 OHS-07 2019-060E 44538						in space
Commercial Chinese Earth observation satellite equipped with high definition, multispectral cameras. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Sep 20, 06:04	6881	0.0014	493	512	94.67	97.40	282	13:00
2019 Oct 20, 09:55	6891	0.0010	506	519	94.88	97.40	197	12:59
2023 Feb 13, 11:39	6861	0.0008	477	489	94.26	97.46	298	12:55

Zhuhai-1 OHS-08 2019-060F 44539						in space
Commercial Chinese Earth observation satellite equipped with high definition, multispectral cameras. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Sep 20, 13:41	6880	0.0015	492	512	94.65	97.40	286	13:00
2019 Oct 20, 01:50	6891	0.0008	507	518	94.88	97.41	219	12:59
2023 Feb 13, 14:28	6861	0.0008	477	488	94.26	97.47	319	13:02

CZ 11 fourth stage 2019-060B 44535						Re-entered - 2019 Sep 19 Life <1 day
Launched cluster of Zuhai-1 satellites. Orbit was lowered soon after releasing the satellites in order to precipitate re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 19, 08:03	6702	0.0345	93	555	91.02	97.37	311
2019 Sep 19, 15:37	6606	0.0191	102	353	89.05	97.38	310

2019-061 CZ 3B + YZ-1 Xichang Space Centre						2019 Sep 22, 21:10
Beidou 47 (Beidou-3 M-23) 2019-061A 44542						in space
Phase 2 operational satellite in MEO for China's navigation satellite system. Launch was brought forward by 24 hrs to avoid forecast bad weather at the launch site.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 24, 18:57	28248	0.0115	21546	22194	787.47	55.03	177
2019 Oct 01, 20:30	28205	0.0100	21547	22108	785.71	55.02	176
2019 Oct 26, 10:46	27909	0.0008	21508	21554	773.35	55.01	312
2023 Feb 12, 05:05	27906	0.0008	21505	21551	773.23	54.53	4

Beidou 48 (Beidou-3 M-24) 2019-061B 44543						in space
Phase 2 operational satellite in MEO for China's navigation satellite system. Launch was brought forward by 24 hrs to avoid forecast bad weather at the launch site.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 24, 18:53	28242	0.0116	21535	22192	787.22	55.02	177
2019 Sep 28, 18:54	28154	0.0085	21535	22016	783.54	55.02	178
2019 Oct 04, 10:38	27906	0.0007	21507	21549	773.23	55.01	288
2023 Feb 12, 21:50	27906	0.0005	21513	21543	773.23	54.52	3

YZ-1 rocket stage 2019-061C 44544						in space
Launched pair of Beidou-3 satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 23, 14:12	28501	0.0032	22033	22213	798.08	55.14	234

CZ 3B fourth stage 2019-061D 44545						Re-entered - 2020 Sep 22 Life 366 days
Launched pair of Beidou-3 satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 23, 22:23	15765	0.5825	204	18569	328.32	55.02	171

2019-062 H-IIB (F-8) Tanegashima Space Centre						2019 Sep 24, 16:05
Kounotori 8 (HTV-8) 2019-062A 44546						Re-entered - 2019 Nov 3 Life 40 days
Carrying supplies and equipment to ISS. Precise launch time 16:05:05 UTC. Separated from launch vehicle at 16:20:07 UTC. Captured with ISS RMS Sep 28 at 11:13 UTC and docked with the downward-facing port of the ISS Harmony module at 15:08 UTC. Postponed from Sep 10 after a fire broke out on the launch pad. Undocked from Harmony Nov 1 at 1345 UTC by ISS RMS under ground control. Released into independent orbit at 17:21 UTC. Final retro-fire Nov 3 at 01:41 led to destructive re-entry at about 02:09 UTC. Any surviving fragments impacted the southern Pacific Ocean some 4500 km east of New Zealand at around 02:30 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 24, 18:55	6620	0.0112	167	316	89.33	51.67	321
2019 Sep 24, 20:25	6623	0.0085	188	301	89.40	51.66	313
2019 Sep 25, 19:12	6736	0.0010	351	365	91.70	51.66	278
2019 Sep 27, 18:42	6754	0.0016	365	386	92.06	51.65	191
2019 Sep 28, 03:52	6782	0.0006	400	408	92.65	51.64	88
2019 Sep 28, 07:16	6793	0.0006	411	420	92.87	51.64	94
2019 Sep 28, 12:46	6795	0.0007	411	421	92.90	51.64	93
2019 Oct 31, 13:30	6794	0.0006	412	420	92.89	51.65	210
2019 Nov 02, 22:52	6693	0.0087	256	373	90.82	51.97	286
2019 Nov 03, 00:26	6650	0.0191	145	399	89.94	51.64	296

H-IIB upper stage uncatalogued						Re-entered - 2019 Sep 24 Life <1 day
Launched Kounotori 8. De-orbited shortly after releasing its payload so not catalogued.
Not Catalogued - orbit parameters unavailable

2019-063 CZ 2D Jiuquan Space Centre						2019 Sep 25, 00:54
Yunhai-1 02 (largest fragment) 2019-063A 44547						in space
Meteorological satellite developed by the Shanghai Academy of Spaceflight Technology (SAST) to be used for observation of atmospheric, marine and space environments, disaster prevention and scientific experiments. Broke into 30+ fragments 2021 Mar 18, probably after colliding with an item of orbital debris.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Sep 25, 05:57	7152	0.0009	767	780	100.32	98.58	269	07:10
2019 Sep 30, 10:57	7161	0.0001	782	784	100.52	98.59	278	07:10
2023 Feb 13, 01:50	7160	0.0002	781	784	100.50	98.48	156	07:06

CZ 3B fourth stage 2019-063B 44548						in space
Launched Yunhai 1 2.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 26, 08:03	7139	0.0008	755	767	100.05	98.15	16

2019-064 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2019 Sep 25, 13:57
Soyuz MS-15 (Soyuz 11F732A48 № 745) 2019-064A 44550						Re-entered - 2020 Apr 17 Life 205 days Returned to Earth
Carrying crew to ISS - Oleg Skripochka (Roscosmos), Jessica Meir (NASA), Hazza Al Mansouri (UAE spaceflight participant). Precise launch time 13:57:43 UTC. Docked with rear port of Zvezda at 19:42 UTC. Undocked 2020 Apr 17 at 01:53 UTC carrying Skripochka, Meir and Andrew Morgan (NASA). Retrofire at 04:22 UTC led to landing at 05:16:43 UTC, 147 km south east of Dzhezkazgan, Kazakhstan.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 25, 14:26	6583	0.0015	195	215	88.59	51.64	68
2019 Sep 25, 17:01	6736	0.0028	339	377	91.70	51.66	206
2019 Sep 25, 17:01	6795	0.0007	411	421	92.90	51.64	84
2020 Apr 16, 12:06	6799	0.0004	418	423	92.98	51.64	121

Soyuz upper stage 2019-064B 44551						Re-entered - 2019 Sep 28 Life 3 days
Launched Soyuz MS-15.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 25, 19:40	6578	0.0008	195	205	88.49	51.65	40

2019-065 Soyuz-2 1B + Fregat Plesetsk Cosmodrome						2019 Sep 26, 07:46
Cosmos 2541 (EKS 3/Tundra 13L) 2019-065A 44552						in space
Missile early warning satellite capable of tracking missiles and other heat sources in the Earth's atmosphere and in space. May also carry a strategic communications system for use by the Russian Military.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 26, 15:51	26469	0.6969	1646	38537	714.29	63.83	270
2019 Oct 08, 07:33	26551	0.6983	1633	38712	717.59	63.84	270

Fregat-M stage 2019-065B 44553						in space
Launched Cosmos 2541.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 02, 08:13	26475	0.6968	1648	38545	714.51	63.82	270

2019-066 CZ 4C Taiyuan Space Centre						2019 Oct 4, 18:51
Gaofen 10 2019-066A 44622						in space
Remote sensing satellite to be used for land use surveys, urban planning, road network design, crop estimation and disaster prevention/mitigation, part of a remote sensing programme based on LEO and GEO satellites. Replaces the original Gaofen 10 that was lost in a launch failure 2016 Aug 31. An unspecified issue on Oct 2 caused 24 hr launch postponement from Oct 3.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Oct 05, 04:01	6995	0.0007	612	622	97.04	97.78	252	01:59
2019 Oct 11, 23:54	7003	0.0004	622	628	97.21	97.77	16	01:59
2019 Oct 13, 03:03	7006	0.0000	628	628	97.27	97.78	262	01:59
2023 Feb 13, 10:05	7004	0.0002	624	627	97.22	97.92	331	01:28

CZ 4C third stage 2019-066B 44623						in space
Launched Gaofen 10.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 04, 21:30	6902	0.0129	434	613	95.10	97.75	39

2019-067 Proton-M + Briz-M Baikonur Cosmodrome						2019 Oct 9, 10:17
Eutelsat 5 West B 2019-067A 44624						in space
Comsat to join Eutelsat 5 West A and eventually take over its functions. Coverage is aimed at France, Italy and Algeria. Satellite includes GEO 3, an EGNOS (European Geostationary Navigation Overlay Service) to improve the precision of ESA's Galileo navigation system for users needing very accurate position information. Precise launch time 10:17:56 UTC. Released from the launch vehicle Oct 10 at 01:53 UTC. Oct 24, Eutelsat revealed an unspecified problem with one of the solar arrays (probably not having deployed fully, if at all). 2020 Jan 17, Eutelsat confirmed the south solar array did not deploy and the satellite is working at 45% capacity. Expected location - 5° west.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Oct 10, 15:21	44913	0.5910	11989	65080	1578.75	13.36	179
2019 Oct 14, 10:25	53994	0.3193	30374	64857	2081.00	3.36	179
2019 Oct 18, 15:00	56748	0.2552	35888	64852	2242.28	1.99	179
2019 Oct 19, 23:13	47728	0.1151	35855	46846	1729.52	0.97	178
2019 Oct 21, 13:56	43726	0.0345	35842	38855	1516.61	0.28	174
2019 Oct 22, 09:42	42234	0.0005	35834	35878	1439.63	0.03	102	4° east
2019 Oct 28, 14:44	42164	0.0001	35781	35792	1436.07	0.01	232	2° east
2020 Jan 10, 23:07	42165	0.0002	35779	35794	1436.11	0.06	52	2° east
2020 Jan 13, 15:20	42271	0.0002	35885	35901	1441.54	0.05	333	2° west
2020 Jan 17, 07:40	42167	0.0002	35782	35797	1436.24	0.05	111	5° west
2023 Feb 12, 07:48	42165	0.0002	35780	35793	1436.09	0.08	114	5° west

MEV-1 (Mission Extension Vehicle 1) 2019-067B 44625						in space
Northrop Grumman spacecraft - launched to rendezvous and attach itself to the Intelsat 901 GEO comsat (28624/2001-024A) then take over its pointing and station-keeping functions in order to extend its on-orbit life by five years. May then move to another satellite. Precise launch time 10:17:56 UTC. Released from the launch vehicle Oct 10 at 02:11 UTC into super-synchronous orbit then pushed towards Intelsat rendezvous by onboard electric thruster system, arriving 2020 Jan 31. Intelsat 901 had departed its station at 27°.5 east 2019 Dec 11 and moved to GEO graveyard orbit. MEV-1 then docked with Intelsat 901 on 2020 Feb 25 at 07:15 UTC so all subsequent listed orbits are for the combined objects. Arrived at Intelsat 901 new location of 27°.5 west 2020 Mar 29.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Oct 10, 15:18	44842	0.5906	11979	64948	1575.01	13.39	179
2019 Oct 14, 11:02	46021	0.5479	14429	64857	1637.57	9.81	179
2019 Nov 22, 20:00	45425	0.3862	21505	56589	1605.84	5.20	188
2019 Nov 26, 11:14	45439	0.3863	21510	56613	1606.60	5.21	189
2019 Dec 29, 03:25	44186	0.2172	28209	47407	1540.59	2.74	207
2020 Jan 03, 05:00	44190	0.2173	28212	47413	1540.81	2.75	207
2020 Jan 23, 03:30	42982	0.0542	34272	38935	1478.03	1.63	251
2020 Jan 29, 00:22	42667	0.0208	35401	37175	1461.81	1.57	266	118° west
2020 Jan 31, 17:34	42485	0.0035	35956	36258	1452.50	1.56	294	132° west
2020 Feb 25, 13:28	42467	0.0002	36081	36098	1451.59	1.64	351	132° east
2020 Mar 03, 13:33	42616	0.0002	36228	36247	1459.22	1.42	340	97° east
2020 Mar 12, 14:01	42616	0.0003	36227	36250	1459.22	0.86	358	45° east
2020 Mar 17, 16:11	42619	0.0003	36227	36255	1459.38	0.56	353	16° east
2020 Mar 22, 07:05	42622	0.0003	36229	36258	1459.50	0.22	342	11° west
2020 Mar 26, 04:48	42230	0.0001	35848	35857	1439.45	0.17	55	25° west
2020 Mar 29, 07:39	42231	0.0001	35849	35857	1439.49	0.06	43	27° west
2020 Mar 30, 11:16	42165	0.0001	35781	35793	1436.11	0.06	113	27° west
2023 Feb 11, 09:19	42165	0.0001	35782	35791	1436.09	0.05	81	27° west

Briz-M rocket stage 2019-067C 44626						in space
Launched Eutelsat 5 West B and MEV-1. Performed a separation manoeuvre after releasing MEV-1. Orbits shown are estimates based on data from Khrunichev, the launch vehicle operator, covering the stages of flight leading up to satellite separation. Catalogue Number and Designation to be confirmed. Space-Track orbit data awaited.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 09, 10:33	6567	0.0012	181	197	88.27	51.55	80
2019 Oct 09, 12:28	9531	0.2995	298	6007	154.33	50.40	179
2019 Oct 09, 15:02	39119	0.8251	465	65016	1283.32	50.10	180
2019 Oct 10, 01:53	45073	0.5831	12412	64977	1587.18	13.40	180
2019 Oct 10, 04:12	43935	0.6119	10675	64438	1527.45	13.30	180

Briz-M APT 2019-067D 44627						in space
Discarded propellant tank from Briz-M rocket stage.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 09, 18:03	16228	0.5846	363	19336	342.88	50.35	173

2019-068 Pegasus XL Lockheed L-1011 over Atlantic Ocean near Cape Canaveral AFS						2019 Oct 11, 01:59
ICON (Ionospheric Connection Explorer) 2019-068A 44628						in space
NASA satellite to study the influences of terrestrial weather and space weather on the ionosphere. The L-1011 took off from Cape Canaveral AIr Force Station at 00:31 UTC and climbed to about 12,500 metres. The Pegaus rocket was released thirty four minutes into a ninety minute launch window that opened at 01:25 UTC. The originally planned release at 01:30 UTC was abandoned because of communications dificulties between the aircraft and the ground. Delayed one day from Oct 10 due to weather.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 14, 22:43	6971	0.0019	580	606	96.54	26.99	169

Pegasus upper stage 2019-068B 44629						in space
Launched ICON.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 14, 22:40	6968	0.0016	579	602	96.49	27.00	166

2019-069 Electron (As the Crow Flies) Rocket Lab Launch Complex, New Zealand						2019 Oct 17, 01:22
Palisade 2019-069A 44634						in space
Imaging satellite owned by Aquila Systems, built to test systems for upcoming satellites based on its 16U (4x4, non-standard Cubesat) Corvus platform. Released from Electron kick stage at 02:33 UTC. Launch delayed from Oct 14 due to thunderstorms in the launch area.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 17, 20:21	7594	0.0011	1208	1224	109.77	87.90	117

Electron second stage 2019-069B 44635						Re-entered - 2023 Sep 14 Life 1428 days
Launched Palisade satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 17, 18:44	7136	0.0629	309	1206	99.98	87.89	272

Electron third stage (kick stage) 2019-069C 44636						in space
Launched Palisade satellite. Performed a perigee-lowering engine firing after releasing the satellite into circular orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 18, 13:50	7229	0.0503	487	1215	101.95	87.90	24

2019-070 CZ 3B Xichang Space Centre						2019 Oct 17, 15:21
TJS 4 (Communication Technology Test Satellite 4) 2019-070A 44637						in space
Described as a technology test satellite, TJS 4 is probably military in nature and intended for signals intelligence gathering (SIGINT).
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Oct 18, 03:45	24387	0.7303	200	35818	631.68	27.03	180
2019 Oct 29, 15:28	42166	0.0003	35775	35800	1436.14	0.09	276	84° east
2019 Nov 09, 02:47	42164	0.0003	35771	35800	1436.03	0.06	280	84° east
2023 Feb 12, 17:37	42166	0.0005	35767	35808	1436.14	0.04	257	83° east

CZ 3B fourth stage 2019-070B 44638						Re-entered - 2024 Nov 2 Life 1843 days
Launched TJS 4.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 18, 03:41	23963	0.7256	197	34973	615.27	27.01	179

2019-071 Antares 230+ Wallops Flight Facility						2019 Nov 2, 13:59
Cygnus NG-12 (SS Alan Bean) 2019-071A 44701						Re-entered - 2020 Mar 17 Life 136 days
Northrop Grumman vehicle carrying supplies to ISS under CRS-2 contract with NASA. Precise launch time 13:59:47 UTC at the beginning of approximately five minute window. Separated from launch vehicle 14:07:36 UTC. Arrived ISS Nov 4 and captured by ISS RMS at 09:10 UTC under control of crew. Docked with downward-facing port of Unity module using RMS under control of ground-based engineers at 11:21 UTC. Undocked 2020 Jan 31 then released from RMS at 13:36 UTC the same day. Whilst in post-undocking free flight, Cygnus released a number of Cubesats and hosted a payload for the US company, Lynk, for experimentation in using space based-mobile phone cells. Planned re-entry 2020 Mar 2 was delayed in order to extend the Lynk tests. Retro fire Mar 17 around 23:00 UTC led to re-entry above the southern Pacific Ocean around 23:40 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 02, 15:36	6637	0.0021	244	273	89.68	51.62	139
2019 Nov 03, 03:23	6726	0.0101	280	416	91.50	51.64	239
2019 Nov 03, 11:09	6775	0.0028	378	416	92.50	51.64	243
2019 Nov 04, 05:34	6790	0.0006	408	416	92.81	51.65	214
2020 Jan 31, 18:10	6799	0.0004	418	424	92.99	51.64	217
2020 Feb 01, 11:53	6843	0.0009	458	471	93.89	51.65	271
2020 Mar 17, 13:36	6841	0.0012	454	471	93.84	51.62	52

Orbital Factory 2 2019-071C 45113						Re-entered - 2023 Mar 20 Life 1234 days
1U Cubesat from the University of Texas at El Paso (UTEP). It carries a 3D printer to demostrate the concept of conducting repairs on a solar cell. Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 04, 00:09	6846	0.0013	459	476	93.94	51.64	295

Aerocube 14A 2019-071D 45114						Re-entered - 2023 Feb 4 Life 1190 days
3U Cubesat, one of a pair, equipped to demonstrate a new star-tracker technology, test a selection of new materials and test a new solar cell. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 01, 19:30	6846	0.0011	460	475	93.94	51.64	278

SwampSat II 2019-071E 45115						Re-entered - 2021 Oct 19 Life 717 days
3U Cubesat from the University of Florida to measure VLF (Very Low Frequency) waves in the ionosphere. It is equipped with a 4m x 4m deployable aerial. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 04, 07:59	6846	0.0013	459	476	93.95	51.64	297

Aerocube 14B 2019-071F 45116						Re-entered - 2023 Feb 8 Life 1194 days
3U Cubesat, one of a pair, equipped to demonstrate a new star-tracker technology, test a selection of new materials and test a new solar cell. Released from Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 02, 10:36	6845	0.0011	460	475	93.94	51.64	293

Aerocube 15B 2019-071G 45117						Re-entered - 2023 Feb 10 Life 1196 days
3U Cubesat one of a pair from Aerospace Corporation to test a low cost optical imager. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )

Aerocube 15A 2019-071H 45118						Re-entered - 2023 Feb 7 Life 1193 days
3U Cubesat one of a pair from Aerospace Corporation to test a low cost optical imager. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 10, 20:24	6845	0.0011	459	474	93.92	51.64	318

Very Low Frequency Propagation Mapper 2019-071K 45120						Re-entered - 2022 Sep 29 Life 1062 days
6U Cubesat from USAF Research Lab. Will study the progagtion of VLF radio signals within the magnetospher, using transmissions from the DSX satelli already in orbit (44344/2019-036F). Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 10, 20:24	6844	0.0011	458	474	93.92	51.64	317

CIRiS (Compact Infrared Radiometer in Space) 2019-071L 45121						Re-entered - 2023 Mar 14 Life 1228 days
6U Cubesat from Utah State University to collect, process and calibrate infrared images to measure the temparuture of the Earth’s surface below. Built by Ball Aerospace. Released from Cygnus NG-12 Slingshot Deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 10, 20:23	6844	0.0011	458	474	93.92	51.64	316

ORCA 8 2019-071R 45126						Re-entered - 2022 Aug 8 Life 1010 days
6U Cubesat from US Defense Advanced Research Projects Agency (DARPA). Onboard equipment is From Systems and Technology Research, a US company that specialises in sensors relating to image processing clandestine communications and SIGINT (among others). Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 10, 20:23	6844	0.0010	459	473	93.92	51.64	289

EdgeCube 2019-071xx						in space
1U Cubesat from Sonoma State University of California in partnership with Morehead State University in Kentucky. It will study chlorophyl by measuring seasonal and other changes in light reflection from leaves. Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
estimated orbit	6846	0.0011	460	475	93.94	51.64	278

HuskySat 1 2019-071xx						in space
3U Cubesat from the University of Washington to demonstrate plasma propulsion and high gain telemetry system for potential use in cubesats operating as far away as the Moon. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
estimated orbit	6846	0.0012	459	476	93.95	51.64	282

MiniCarb 2019-071xx						in space
6U Cubesat developed by NASA, the Lawrence Livermore National Laboratory and the USAF to detect and measure the amounts of greenhouse gases, such as methane and carbon dioxide, in the Earth's atmosphere. Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
estimated orbit	6844	0.0011	458	474	93.92	51.64	317

2019-072 CZ 4B Taiyuan Space Centre						2019 Nov 3, 03:22
Gaofen 7 2019-072A 44703						in space
Civilian high resolution stereoscopic Earth imaging satellite for mapping.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Nov 04, 23:00	6875	0.0013	488	506	94.55	97.49	266	10:31
2019 Nov 30, 19:25	6880	0.0011	495	510	94.66	97.49	155	10:32
2023 Feb 13, 09:49	6879	0.0010	495	508	94.64	97.38	32	10:42

SRSS 1 (Sudanese Remote Sensing Satellite) 2019-072B 44704						Re-entered - 2023 Nov 29 Life 1487 days
Small satellite developed for the Sudanese government by the Shenzhen Aerospace Oriental Red Sea Satellite Co. Designed for both civil and military remote sensing mainly over Sudan.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 05, 21:35	6873	0.0013	486	504	94.52	97.50	268
2023 Feb 13, 09:38	6834	0.0012	447	464	93.70	97.40	14

Huangpu 1 2019-072C 44705						Re-entered - 2023 Nov 9 Life 1467 days
Small developmental/test satellite for remote sensing built by the Shanghai Aerospace Technology Research Institute.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 04, 11:00	6873	0.0014	485	505	94.51	97.48	277
2023 Feb 13, 10:03	6827	0.0011	441	456	93.56	97.39	9

Xiaoxiang-1 08 2019-072D 44706						Re-entered - 2023 Apr 25 Life 1269 days
6U Cubesat from Tianyi Research Institute (SpaceTy) - testbed for multispectral remote sensing imaging system for agricultural crop surveys. Also carries a laser communication system and a French-supplied experimental iodine-fuelled thruster to speed up orbital decay at end of life.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 04, 11:00	6873	0.0016	484	506	94.52	97.49	268
2023 Feb 13, 09:13	6780	0.0007	397	406	92.59	97.40	338

CZ-4B upper stage 2019-072E 44707						Re-entered - 2020 Apr 8 Life 157 days
Launched Gaofen 7. Performed an orbit-lowering engine firing after releasing its satellites in order to accelerate re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 03, 09:00	6738	0.0196	228	492	91.75	97.59	28

2019-073 CZ 3B Xichang Space Centre						2019 Nov 4, 17:43
Beidou 49 (Beidou-3 IGEO-3) 2019-073A 44709						in space
Phase 2 operational satellite in China's navigation satellite system. It also provides time and messaging services for the Asia-Pacific region from inclined geosynchronous orbit. Probably moved into geosynchronous drift orbit some time on Nov 5 and arrived on station shortly after. Launch completes the IGEO part of the Beidou-3 constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Nov 04, 23:24	24384	0.7309	184	35828	631.57	28.51	180
2019 Nov 22, 20:40	42159	0.0025	35675	35888	1435.81	58.70	184	106° east
2023 Feb 12, 13:52	42160	0.0029	35661	35903	1435.84	56.88	179	118° east

CZ 3B fourth stage 2019-073B 44710						Re-entered - 2021 Feb 25 Life 479 days
Launched Beidou-3 IGEO-3.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 04, 20:52	23652	0.7239	152	34396	603.33	28.50	179

2019-074 Falcon 9 Block 5 Cape Canaveral Air Force Station						2019 Nov 11, 14:56
Starlink-1007 2019-074A 44713						Re-entered - 2024 Oct 2 Life 1787 days
One member of a simultaneously-launched cluster of sixty LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from the launch vehicle around 15:57 UTC. All satellites were injected initially into similar orbits at 300 km altitude.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 14, 22:00	6678	0.0001	299	300	90.51	53.01	326
2019 Nov 28, 12:00	6728	0.0001	349	351	91.53	53.01	46
2020 Jun 20, 04:00	6928	0.0001	549	550	95.64	53.00	105

Falcon 9 upper stage uncatalogued						Re-entered - 2019 Nov 11 Life <1 day
Launched cluster of Starlink satellites. Caused to re-enter about one hour after lift-off. Any surviving fragments from its destructive re-entry impacted the Southern Ocean. Not catalogued.
Not Catalogued - orbit parameters unavailable

2019-075 Kuaizhou 1A Jiuquan Space Centre						2019 Nov 13, 03:40
Jilin-1 High Resolution 02A (Jilin-1 GF02A) 2019-075A 44777						in space
Chinese high resolution, multi-spectral imaging satellite. Launch postponed from Oct 27 (weather) and Oct 29 (problem with launch vehicle guidance system).
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Nov 15, 04:43	6917	0.0011	532	546	95.42	97.54	255	10:00
2023 Feb 13, 12:15	6911	0.0005	530	537	95.30	97.65	179	09:23

Kuaizhou 1A fourth stage 2019-075B 44778						Re-entered - 2019 Nov 20 Life 7 days
Launched Jilin-1 02A. Performed a retro-fire after releasing the satellite in order to speed up re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 06:23	6765	0.0362	142	631	92.29	97.50	25

2019-076 CZ 6 (Y-4) Taiyuan Space Centre						2019 Nov 13, 06:35
Ningxia-1 1A (Zhongzi 1A) 2019-076A 44779						in space
One of a cluster of five similar satellites, probably a demonstrator or 'pathfinder' mission. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor the radio spectrum over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 14, 11:13	7271	0.0008	887	899	102.84	45.00	257
2019 Nov 24, 12:39	7271	0.0008	887	899	102.84	45.01	300
2020 Jan 12, 16:25	7266	0.0010	881	895	102.73	45.01	217

Ningxia-1 1B (Zhongzi 1B) 2019-076B 44780						in space
One of a cluster of five similar satellites, probably a demonstrator or 'pathfinder' mission. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor the radio spectrum over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 23:13	7271	0.0008	887	899	102.84	45.01	254
2019 Nov 24, 04:04	7270	0.0010	885	899	102.81	45.01	300
2020 Jan 12, 17:47	7266	0.0009	882	894	102.73	45.01	210

Ningxia-1 1C (Zhongzi 1C) 2019-076C 44781						in space
One of a cluster of five similar satellites, probably a demonstrator or 'pathfinder' mission. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor the radio spectrum over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 23:13	7270	0.0009	886	899	102.82	45.00	263
2019 Nov 24, 04:00	7269	0.0011	882	898	102.79	45.00	300
2020 Jan 12, 19:09	7266	0.0009	881	895	102.73	45.00	199

Ningxia-1 1D (Zhongzi 1D) 2019-076D 44782						in space
One of a cluster of five similar satellites, probably a demonstrator or 'pathfinder' mission. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor the radio spectrum over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 11:48	7270	0.0010	885	899	102.81	45.01	272
2019 Nov 24, 03:58	7267	0.0012	880	898	102.76	45.01	303
2020 Jan 14, 10:10	7266	0.0013	879	897	102.74	45.01	194

Ningxia-1 1E (Zhongzi 1E) 2019-076E 44783						in space
One of a cluster of five similar satellites, probably a demonstrator or 'pathfinder' mission. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor the radio spectrum over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 21:30	7269	0.0009	884	898	102.79	45.00	277
2019 Nov 17, 21:20	7266	0.0012	879	896	102.73	45.01	292
2020 Jan 13, 03:02	7266	0.0011	880	896	102.73	45.01	204

CZ 6 third stage 2019-076F 44784						in space
Launched group of five Ningxia-1 satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 14, 12:34	7212	0.0089	770	898	101.59	45.01	8

2019-077 Kuaizhou 1A Jiuquan Space Centre						2019 Nov 17, 10:00
KL-α A 2019-077A 44785						in space
One of a pair of proof-of-concept satellites for a multi-media communications system. Built by the Institute of Microsatellite Innovation of the Chinese Academy of Sciences to be operated by a German company, KLEO Connect, that has the contract to provide demonstrator satellites for the proposed "eightyLEO" constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 17, 18:11	7429	0.0009	1044	1058	106.21	88.91	275
2021 Aug 03, 11:57	7429	0.0009	1044	1058	106.21	88.91	252

KL-α B 2019-077B 44786						in space
One of a pair of proof-of-concept satellites for a multi-media communications system. Built by the Institute of Microsatellite Innovation of the Chinese Academy of Sciences to be operated by a German company, KLEO Connect, that has the contract to provide demonstrator satellites for the proposed "eightyLEO" constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 17, 18:27	7617	0.0254	1045	1432	110.26	88.91	309
2020 Feb 27, 17:39	7616	0.0256	1043	1433	110.25	88.92	36
2020 Feb 29, 08:14	7608	0.0244	1045	1416	110.07	88.92	31
2020 Feb 29, 16:00	7584	0.0216	1043	1370	109.56	88.94	31
2020 Mar 01, 15:57	7563	0.0190	1041	1329	109.10	88.92	31
2020 Mar 02, 15:21	7543	0.0165	1040	1290	108.66	88.92	28
2020 Mar 08, 03:49	7439	0.0037	1034	1089	106.43	88.90	4
2020 Mar 08, 18:29	7429	0.0026	1032	1070	106.21	88.89	352
2021 Jul 22, 19:18	7429	0.0026	1032	1071	106.21	88.90	331

Kuaizhou 1A fourth stage 2019-077C 44787						in space
Launched KL-α pair. Performed retro-fire soon after releasing satellites in order to hasten re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 17, 21:01	7097	0.0546	331	1106	99.16	88.88	185

2019-I12 JEM Small Satellite Orbital Deployer International Space Station						2019 Nov 20, 09:50
RwaSat 1998-067QV 44790						Re-entered - 2022 Apr 27 Life 889 days
3U Cubesat from Rwanda, built with assistance from Japan. It carries a store and forward messaging system and Earth observation cameras. Release time shown is as planned - actual time not confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 21, 19:53	6793	0.0009	409	420	92.86	51.64	327

2019-I13 JEM Small Satellite Orbital Deployer International Space Station						2019 Nov 20, 10:09
AqT-D (Aqua Thruster - Demonstrator) 1998-067QW 44791						Re-entered - 2022 Apr 20 Life 882 days
3U Cubesat from the University of Tokyo to demonstrate water as a propellant for satellite thrusters. Release time shown is as planned - actual time not known.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 21, 07:50	6793	0.0003	413	416	92.86	51.64	310

2019-I14 JEM Small Satellite Orbital Deployer International Space Station						2019 Nov 20, 10:10
NARSSCube 1 1998-067QX 44792						Re-entered - 2021 Dec 20 Life 761 days
1U Cubesat from Egypt's National Authority for Remote Sensing and equipped with an Earth observation camera. Release time shown is as planned - actual time not confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 21, 10:55	6793	0.0005	412	419	92.87	51.64	327

2019-078 CZ 3B + YZ-1 Xichang Space Centre						2019 Nov 23, 00:55
Beidou 50 (Beidou-3 M-21) 2019-078A 44793						in space
Phase 2 operational satellite in MEO for China's navigation satellite system.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 29, 05:24	28247	0.0115	21542	22194	787.42	54.99	178
2019 Dec 14, 01:28	28108	0.0066	21545	21916	781.65	55.00	180
2019 Dec 20, 13:59	27907	0.0006	21512	21545	773.26	55.01	332
2023 Feb 12, 07:53	27906	0.0007	21508	21548	773.23	54.87	7

Beidou 51 (Beidou-3 M-22) 2019-078B 44794						in space
Phase 2 operational satellite in MEO for China's navigation satellite system.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 25, 03:21	28243	0.0116	21537	22192	787.26	54.99	178
2019 Dec 30, 06:01	27906	0.0005	21514	21542	773.22	55.00	323
2023 Feb 12, 05:26	27906	0.0005	21513	21542	773.23	54.85	359

YZ-1 rocket stage 2019-078C 44795						in space
Launched Beidou-3 M-21 and Beidou-3 M-22.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 23, 07:12	28737	0.0058	22193	22526	808.03	55.15	359

CZ 3B fourth stage 2019-078D 44796						in space
Launched Beidou-3 M-21 and Beidou-3 M-22.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 23, 04:16	15744	0.5819	204	18527	327.65	54.96	171

2019-079 Soyuz-2 1V + Volga Plesetsk Cosmodrome						2019 Nov 25, 17:52
Cosmos 2542 2019-079A 44797						Re-entered - 2023 Oct 24 Life 1429 days
Military satellite with sensors that allow it to observe other satellites in orbit. It also carries an Earth imaging system. Orbit is very close to, and co-planar with, that of USA 245 (39232/2013-043A), a KH-11 reconsat.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Nov 26, 12:54	6991	0.0350	368	858	96.96	97.90	319	09:40
2023 Oct 24, 06:56	6531	0.0009	148	159	87.55	97.63	275	12:48

Cosmos 2543 2019-079D 44835						Re-entered - 2024 Aug 26 Life 1736 days
Small satellite detached from Cosmos 2542 on Dec 6 probably sometime between 04:00 UTC and 10:00 UTC. Purpose possibly connected with the 'observing other satellites' capability mentioned in the launch announcement for Cosmos 2542.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 06, 13:49	6991	0.0351	368	858	96.95	97.90	286	09:40
2019 Dec 09, 16:11	6993	0.0347	372	858	96.99	97.90	276	09:40
2019 Dec 14, 15:58	7034	0.0287	454	858	97.86	97.90	260	09:40
2019 Dec 16, 17:02	7103	0.0189	590	859	99.29	97.90	253	09:40
2020 Jul 16, 18:52	6989	0.0010	604	618	96.91	97.87	141	09:07

Un-named satellite 2019-079E 45915						in space
Test of kinetic energy satellite interceptor using Cosmos 2535 (44421/2019-035A) as a target. Released from Cosmos 2543 (44835/2019-079D) 2020 Jul 17 and passed close to Cosmos 2535. Possibly aimed for a near miss in order to avoid a debris-shedding event.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Jul 16, 19:07	7022	0.0198	505	784	97.61	97.87	183

Volga rocket stage 2019-079B 44798						Re-entered - 2019 Nov 26 Life 1 day
Launched Cosmos 2542. Caused to re-enter over the southern Pacific Ocean Nov 26 with retro-fire at approx 05:30 UTC and entry into the atmosphere at about 06:10 UTC on a track heading northward from Antarctica.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 26, 04:49	6992	0.0352	368	860	96.98	97.90	320

Soyuz upper stage 2019-079C 44799						Re-entered - 2020 Jul 18 Life 236 days
Launched Cosmos 2542.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 26, 05:50	6704	0.0056	289	364	91.06	97.91	67

2019-080 Ariane 5ECA (VA-250) Centre Spatiale Guyanaise						2019 Nov 26, 21:23
TIBA 1 2019-080A 44800						in space
Egyptian government and military communications satellite. Separated from launch vehicle at 21:50 UTC. Launch postponed from Nov 22 by problem with ground equipment then delayed 14 mins by weather. Expected location - 35°.5 east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Nov 27, 00:08	24392	0.7276	266	35763	631.88	5.00	178
2019 Dec 02, 03:09	36448	0.1556	24401	35740	1154.19	0.51	173
2019 Dec 07, 22:30	42154	0.0009	35737	35814	1435.54	0.07	254	36° east
2019 Dec 08, 04:19	42163	0.0003	35774	35795	1436.00	0.07	324	36° east
2023 Feb 13, 06:15	42165	0.0002	35778	35796	1436.12	0.05	325	36° east

Inmarsat 5 F5 (GX-5) 2019-080B 44801						in space
High capacity comsat proving services to the Middle East, Europe and the Indian sub-continent. Fifth satellite in Intelsat's Global Express constellation. Separated from launch vehicle at 22:07 UTC. Launch postponed from Nov 22 by problem with ground equipment then delayed 14 mins by weather. Expected location - 11° east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Nov 27, 13:40	24365	0.7277	256	35719	630.84	5.00	178
2019 Dec 03, 15:56	42059	0.0001	35677	35685	1430.70	0.08	128	80° east
2019 Dec 05, 22:36	42086	0.0004	35690	35725	1432.05	0.08	262	83° east
2019 Dec 08, 07:45	42156	0.0012	35728	35828	1435.66	0.07	104	84° east
2019 Dec 10, 16:54	42164	0.0000	35786	35786	1436.08	0.07	45	84° east
2023 Feb 13, 04:32	42164	0.0002	35779	35794	1436.08	0.04	305	11° east

Ariane 5 upper stage 2019-080C 44802						in space
Launched TIBA 1 and Eutelsat 5 F5.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 26, 23:59	24256	0.7266	252	35503	626.59	5.06	179

2019-081 PSLV-XL (PSLV C-47) Satish Dhawan Space Centre						2019 Nov 27, 03:58
Cartosat 3 2019-081A 44804						in space
Indian third generation high resolution imaging cartographic and remote sensing satellite. Separated from launch vehicle at 04:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Nov 27, 11:38	6888	0.0014	500	519	94.82	97.52	232	09:29
2023 Feb 13, 08:57	6886	0.0012	500	517	94.78	97.37	93	09:29

Meshbed 2019-081C 44806						Re-entered - 2023 May 2 Life 1252 days
3U Cubesat from Analytical Space Inc, testing its FUSE experimental phased array communication antenna.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 28, 23:35	6887	0.0013	500	518	94.79	97.52	235
2023 Feb 12, 23:22	6798	0.0006	416	424	92.97	97.37	76

Flock 4P-1 2019-081L 44814						Re-entered - 2023 Apr 19 Life 1239 days
3U Cubesat, part of Planet's Flock 4P cluster of second generation imaging satellites. The satellite is one of a cluster of twelve Flock 4P satellites carried on this launch. In order to avoid clutter the others are not listed separately. All are are in similar orbits.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 29, 12:13	6885	0.0013	498	516	94.77	97.52	215
2023 Feb 13, 03:54	6800	0.0003	419	424	93.01	97.37	79

PSLV upper stage 2019-081B 44805						in space
Launched Cartosat 3 and thirteen small satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 27, 06:53	6908	0.0046	498	561	95.23	97.51	239

2019-082 CZ 4C Taiyuan Space Centre						2019 Nov 27, 23:52
Gaofen 12-01 2019-082A 44819						in space
Earth observation using radar and high resolution optical sensors for Earth imaging to "support land surveys, crop management, urban and road network planning".
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Nov 28, 04:09	6975	0.0004	594	599	96.62	97.93	252	07:00
2019 Nov 29, 13:10	6993	0.0002	613	616	96.99	97.93	172	07:00
2019 Nov 30, 13:16	7003	0.0004	623	628	97.21	97.94	349	07:00
2019 Dec 01, 19:29	7007	0.0001	628	630	97.28	97.93	74	07:00
2023 Feb 13, 09:01	7006	0.0002	627	629	97.27	97.85	90	06:46

CZ 4C third stage 2019-082B 44820						Re-entered - 2024 Nov 11 Life 1811 days
Launched Gaofen 12. Performed a separation manoeuvre and moved into a slightly lower orbit after satellite release.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 28, 04:05	6884	0.0128	418	594	94.74	97.88	44

2019-083 Falcon 9 Block 5 Cape Canaveral Air Force Station						2019 Dec 5, 17:29
SpaceX Dragon CRS-19 2019-083A 44821						Re-entered - 2020 Jan 7 Life 33 days Returned to Earth
Carrying a cargo to the ISS under NASA's Commercial Resupply Services (CRS) contract. Captured by ISS Remote Manipulator System under manual control Dec 8 at 10:05 UTC. Docked, using the RMS under ground control, with the downward-facing port of the Harmony node at 12:47 UTC. Undocked using RMS under ground control, 2020 - Jan 6 or Jan 7, released under ground control Jan 7, 10:05 UTC, two minutes later than scheduled. Retro fire Jan 7, approx14:47 UTC led to splashdown off California near 31° north, 121° west at 15:42 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 05, 23:30	6669	0.0130	204	378	90.34	51.65	49
2019 Dec 07, 04:37	6668	0.0134	201	379	90.32	51.65	54
2019 Dec 07, 21:17	6784	0.0013	397	415	92.68	51.64	13
2019 Dec 08, 14:18	6795	0.0007	411	422	92.90	51.64	12

Falcon 9 upper stage uncatalogued						Re-entered - 2019 Dec 5 Life <1 day
Launched Dragon CRS-19. Caused to re-enter shortly after releasing Dragon.
Not Catalogued - orbit parameters unavailable

2019-084 Electron (Running Out Of Fingers) Rocket Lab Launch Complex, New Zealand						2019 Dec 6, 08:18
ALE 2 (Astro Live Experiences 2) 2019-084A 44824						Re-entered - 2023 Apr 19 Life 1230 days
Satellite aimed to create 400 artificial meteors in a selection of colours (white, green, pink and orange) partly as performance art. The meteoroid release mechanism failed to operate and none were released. The satellite includes a propulsion system for manoeuvres. that operated for a short period 2019 Feb.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 11:02	6784	0.0013	397	415	92.69	97.01	307
2023 Feb 13, 01:47	6707	0.0004	326	331	91.10	96.85	261

NOOR 1A 2019-084D 44827						Re-entered - 2020 Dec 29 Life 389 days
Satellite from Stara Space to demonstrate LEO-to-LEO intersatellite link technology, including on-demand provision of communication links to ground stations.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 07, 04:56	6754	0.0041	348	403	92.06	97.00	254

NOOR 1B 2019-084E 44828						Re-entered - 2020 Apr 7 Life 123 days
Satellite from Stara Space to demonstrate LEO-to-LEO intersatellite link technology, including on-demand provision of communication links to ground stations.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 19:43	6753	0.0040	348	402	92.05	97.00	256

Fossasat 1 2019-084F 44829						Re-entered - 2020 Oct 28 Life 327 days
1p PocketQube developed by Spain's Fossa Systems - demonstrator of communications satellite that uses low power RF to provide internet connectivity.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 21:20	6753	0.0040	348	401	92.04	97.00	254

ATL 1 (Advanced Technology of Laser) 2019-084G 44830						Re-entered - 2020 Oct 9 Life 308 days
Small satellite from Advanced Technology of Laser from Hungary designed to test a new thermal isolation material in space, conduct a thermal insulator material experiment, and DVB-T band spectrum monitoring.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 21:20	6753	0.0041	347	402	92.04	97.01	255

TRSI 1 2019-084H 44831						Re-entered - 2020 Oct 11 Life 310 days
Small satellite conducting tests on decoding weak signals and testing a very small satellite transmit/receive aerial. Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 21:19	6753	0.0037	350	399	92.04	97.01	251

SMOG-P 2019-084J 44832						Re-entered - 2020 Sep 28 Life 297 days
Spectrum monitoring payload built by students at the Budapest University of Technology and Economics in Hungary. It features a radio spectrum analyzer to measure man-made electromagnetic pollution from space.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 21:19	6752	0.0039	348	401	92.03	97.00	253

Electron third stage (kick stage) 2019-084B 44825						Re-entered - 2020 Nov 8 Life 338 days
Launched cluster of satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 16:39	6755	0.0051	342	412	92.09	97.00	257

Electron second stage 2019-084C 44826						Re-entered - 2019 Dec 18 Life 12 days
Launched cluster of satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 10:52	6672	0.0172	180	409	90.40	97.01	225

2019-085 Soyuz-2 1A Baikonur Cosmodrome						2019 Dec 6, 09:34
Progress MS-13 (Progress 7K-MS №443) 2019-085A 44833						Re-entered - 2020 Jul 8 Life 215 days
Supplies to ISS. Precise launch time 09:34:11 UTC. Docked automatically with Pirs module of ISS Dec 9 at 10:35:11 UTC, about 3 min earlier than scheduled.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 17:07	6697	0.0008	313	324	90.90	51.63	25
2019 Dec 06, 21:23	6699	0.0012	312	329	90.94	51.64	17
2019 Dec 08, 12:45	6704	0.0020	312	339	91.04	51.65	21
2019 Dec 09, 13:27	6795	0.0007	411	421	92.90	51.64	17

Soyuz upper stage 2019-085B 44834						Re-entered - 2019 Dec 10 Life 4 days
Launched Progress MS-13.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 18:41	6581	0.0024	187	219	88.55	51.66	77

2019-086 Kuaizhou 1A Taiyuan Space Centre						2019 Dec 7, 02:55
Jilin-1 High Resolution 02B (Jilin-1 GF02B) 2019-086A 44836						in space
Chinese high resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 07, 04:21	6916	0.0010	531	544	95.39	97.54	267	10:01
2019 Dec 08, 23:28	6917	0.0010	532	546	95.43	97.54	263	10:01
2023 Feb 13, 15:07	6912	0.0008	528	540	95.32	97.65	260	09:25

Kuaizhou 1A fourth stage 2019-086B 44837						Re-entered - 2020 Mar 4 Life 88 days
Launched Jilin-1 02B. Orbit perigee lowered after releasing the satellite in order to speed up re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 07, 05:54	6850	0.0416	187	756	94.03	97.52	158

2019-087 Kuaizhou 1A Taiyuan Space Centre						2019 Dec 7, 08:52
Head 2B (Head 3) 2019-087A 44838						Re-entered - 2023 Nov 1 Life 1425 days
Application satellite from Head Aerospace in the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications between internet-connected devices.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 07, 11:50	6881	0.0012	495	511	94.68	97.37	268	16:00

Head 2A (Head 2) 2019-087B 44839						Re-entered - 2024 Feb 16 Life 1532 days
Application satellite from Head Aerospace in the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications between internet-connected devices.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 07, 17:47	6881	0.0011	495	511	94.68	97.37	265	16:00

Tianyi 16 2019-087C 44840						Re-entered - 2024 Mar 28 Life 1573 days
Medium resolution optical Earth-imaging satellite. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 07, 11:49	6880	0.0010	496	509	94.66	97.38	268	16:00

Tianyi 17 2019-087D 44841						Re-entered - 2022 Dec 31 Life 1120 days
Medium resolution optical Earth-imaging satellite. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 07, 17:47	6880	0.0009	496	508	94.66	97.37	260	16:00

Tianqi 4 A 2019-087E 44842						Re-entered - 2024 Apr 18 Life 1594 days
6U Cubesat? - comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 08, 15:53	6880	0.0011	495	509	94.66	97.37	267

Tianqi 4 B 2019-087F 44843						Re-entered - 2024 Aug 2 Life 1700 days
6U Cubesat? - comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 08, 15:53	6880	0.0011	494	510	94.66	97.37	272

Kuaizhou 1A fourth stage 2019-087G 44844						Re-entered - 2020 Dec 28 Life 387 days
Launched group of six satellites. Orbit perigee lowered after releasing the satellite in order to speed up re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 07, 22:57	7049	0.0657	208	1134	98.17	97.38	341

2019-088 Soyuz-2 1B + Fregat Plesetsk Cosmodrome						2019 Dec 11, 08:54
Cosmos 2544 (Uragan-M) 2019-088A 44850						in space
GLONASS-M navigation satellite to fill a space in the constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 15:17	25516	0.0005	19126	19150	676.05	64.84	264
2019 Dec 19, 12:06	25455	0.0029	19003	19150	673.62	64.83	249
2020 Jan 03, 04:54	25508	0.0010	19106	19154	675.73	64.82	265

Volga rocket stage 2019-088B 44851						in space
Launched Cosmos 2544. Separated from Soyuz third stage at 09:04 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 15:23	25708	0.0071	19147	19513	683.70	64.81	62

2019-089 PSLV-QL (PSLV C-48) Satish Dhawan Space Centre						2019 Dec 11, 09:55
NANOVA 2019-089A 44852						Re-entered - 2024 Oct 3 Life 1758 days
3U Cubesat acting as demonstrator for the on-orbit element of "Commtrails", a project to create a search and rescue system using direct satellite links for data, voice and text messaging for emergency communications from remote areas. Built by Tyvak for Israeli company Elbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 12, 02:49	6947	0.0007	564	574	96.04	36.96	348

RISat 2BR1 (Radar Imaging Satellite) 2019-089B 44853						Re-entered - 2024 Sep 24 Life 1749 days
Indian remote sensing satellite equipped with an imaging radar. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 17:18	6948	0.0007	564	574	96.05	36.97	337

Duchifat 3 2019-089C 44854						in space
3U Cubesat for remote sensing, developed by students of the Herzliya Science Centre Space Laboratory, Israel. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 17:18	6948	0.0009	564	577	96.07	36.97	326

Lemur-2 (JPGSquared) 2019-089D 44855						Re-entered - 2024 Sep 11 Life 1736 days
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Developed by Spire (formerly Nanosatisfi). One of four Lemur-2 satellites carried on this launch. In order to avoid clutter the others are not listed separately. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 17:18	6949	0.0007	566	576	96.09	36.97	314

Isanagi (QPS-SAR) 2019-089E 44856						Re-entered - 2024 Oct 3 Life 1758 days
Japanese radar-carrying Earth observation satellite from the qPS institute.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 17:18	6951	0.0007	567	578	96.12	36.96	303

Pathfinder Technology Demonstrator 1 2019-089F 44857						in space
6U Cubesat (3x2) - NASA technology demonstrator for a water-based, low thrust, propulsion system. Project led by NASA Ames Research Center in collaboration with NASA Glenn Research Center. First of five planned PTD launches. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 19:00	6951	0.0008	568	578	96.13	36.97	297

1HOPSat (First Generation High Optical Performance Satellite) 2019-089G 44858						Re-entered - 2023 Dec 24 Life 1474 days
12U (2x2x3) Cubesat carrying a commercially operated Earth imaging system. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 19:03	6952	0.0008	569	579	96.15	36.96	280

PSLV upper stage 2019-089L 44862						in space
Launched RISat 2BR1 and nine small satellites. Orbit perigee lowered after releasing final satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 18:47	6923	0.0037	519	571	95.55	36.98	98

2019-090 CZ 3B + YZ-1 Xichang Space Centre						2019 Dec 16, 07:12
Beidou 52 (Beidou-3 M-19) 2019-090A 44864						in space
Phase 2 operational satellite in China's navigation satellite system. One of the final pair needed to complete the Beidou-3, 24 satellite, MEO constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 16, 14:19	28235	0.0119	21521	22193	786.94	55.02	178
2019 Dec 20, 08:42	28077	0.0063	21522	21877	780.36	55.02	184
2019 Dec 24, 15:10	27906	0.0013	21491	21565	773.23	55.01	255
2023 Feb 12, 11:39	27906	0.0018	21478	21578	773.23	55.56	270

Beidou 53 (Beidou-3 M-20) 2019-090B 44865						in space
Phase 2 operational satellite in China's navigation satellite system. One of the final pair needed to complete the Beidou-3, 24 satellite, MEO constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 16, 13:55	28239	0.0118	21528	22193	787.09	55.01	178
2019 Dec 21, 04:01	28197	0.0102	21530	22108	785.35	55.00	179
2020 Jan 20, 23:24	27906	0.0013	21493	21563	773.23	55.04	277
2023 Feb 12, 07:08	27906	0.0016	21483	21573	773.23	55.57	284

YZ-1 rocket stage 2019-090C 44866						in space
Launched Beidou-3 M-19 and Beidou-3 M-20.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 16, 13:27	28756	0.0065	22190	22565	808.81	54.82	356

CZ 3B fourth stage 2019-090D 44867						in space
Launched Beidou-3 M-19 and Beidou-3 M-20.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 16, 10:42	15682	0.5810	192	18416	325.74	55.00	170

2019-091 Falcon 9 Block 5 Cape Canaveral Air Force Station						2019 Dec 17, 00:10
JCSat 18 (Kacific 1) 2019-091A 44868						in space
Comsat serving east Asia. Two part payload owned jointly by Sky Perfect of Japan and Kacific of Singapore. Expected location 150° east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Dec 17, 12:28	16677	0.6012	273	20324	357.21	26.91	178
2019 Dec 20, 18:00	21052	0.6825	305	29043	506.64	26.64	179
2019 Dec 31, 14:02	42168	0.0003	35779	35801	1436.26	0.08	28	150° east
2023 Feb 12, 18:52	42165	0.0000	35786	35787	1436.09	0.01	49	150° east

Falcon 9 upper stage 2019-091B 44869						in space
Launched JCSat 18/Kacific 1
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 17, 12:27	16673	0.6012	270	20319	357.08	26.91	178

2019-092 Soyuz ST-A + Fregat-M (VS-23) Centre Spatiale Guyanaise						2019 Dec 18, 08:54
CSG-1 (COSMO-SkyMed Second Generation) 2019-092A 44873						in space
Italian Space Agency second generation, follow-on, Earth imaging satellite equipped with synthetic aperture radar. Precise launch time 08:54:20 UTC. Released from Fregat at 09:17:03 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 18, 18:42	7000	0.0001	622	623	97.15	97.82	354	17:50
2023 Feb 13, 11:22	7001	0.0001	622	623	97.15	97.89	78	17:46

CHEOPS (Characterising Exoplanet Satellite) 2019-092B 44874						in space
ESA mission to search for exoplanetary transits by performing ultra-high precision photometry on bright stars already known to host planets. Precise launch time 08:54:20 UTC. Released from Fregat at 11:19:01 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 18, 18:53	7081	0.0008	698	709	98.84	98.23	304	17:49
2023 Feb 12, 23:04	7081	0.0010	695	710	98.83	98.24	315	18:02

ANGELS (Argos Néo on a Generic Economical and Light Satellite) 2019-092D 44876						in space
12U Cubesat (3x2x2) from French national space agency CNES, fitted with a miniaturized ARGOS Néo instrument, ten times smaller than previous versions. It collects and determines the position of low-power signals and messages from ground-based ARGOS beacons. Precise launch time 08:54:20 UTC. Released from Fregat at 13:07:34 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 18, 23:19	6895	0.0011	510	525	94.97	97.45	288	17:48

EyeSat 2019-092E 44877						Re-entered - 2023 Nov 19 Life 1432 days
3U Cubesat from France's CNES, equipped with a small telescope designed to study the zodiacal light and to produce images of the Milky Way. Precise launch time 08:54:20 UTC. Released from Fregat at 13:05:04 UTC along with OPS-SAT.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 18, 23:19	6895	0.0013	508	525	94.95	97.44	293	17:48

OPS-SAT 2019-092F 44878						Re-entered - 2024 May 22 Life 1617 days
3U Cubesat - ESA mission carrying a 'sandbox' computer to act as in-orbit testbed for new software, new applications and new techniques in satellite control. Precise launch time 08:54:20 UTC. Released from Fregat at 13:05:04 UTC along with EyeSat.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 19, 00:04	6899	0.0010	514	528	95.05	97.47	274	17:48
2023 Feb 12, 22:34	6864	0.0010	479	493	94.33	97.48	221	17:56

2019-093 CZ 4B Taiyuan Space Centre						2019 Dec 20, 03:22
Tianqin 1 2019-093A 44879						in space
Test satellite carrying a micro-thruster and instruments to collect global gravity field data. More advanced versions will be used in China's upcoming gravity wave studies satellites. Also carries an Amateur Radio receiver/transmitter.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:05	7003	0.0015	615	636	97.21	97.97	263

ETRSS 1 (Ethiopia Remote Sensing Satellite) 2019-093B 44880						in space
Chinese financed and built satellite operated by Ethiopia, carries high resolution imaging system for remote sensing.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 20, 08:04	7003	0.0014	615	635	97.21	97.97	264	10:31

Tianyan 01 2019-093C 44881						in space
Small satellite equipped with a remote sensing payload.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 20, 08:05	7003	0.0014	615	635	97.21	97.98	261	10:31

Tianyan 02 2019-093D 44882						in space
Small satellite equipped with a remote sensing payload.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 20, 08:05	7003	0.0015	614	636	97.20	97.98	267	10:31

CBERS 4A (Ziyuan-1 04B, China-Brazil Earth Resources Satellite) 2019-093E 44883						in space
China-Brazil Earth Resouces Satellite carrying a range of Earth observation sensors. Brazilian built using Chinese satellite bus.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2019 Dec 27, 19:37	7003	0.0002	623	626	97.20	97.98	85	10:31
2023 Feb 13, 10:50	7002	0.0002	623	626	97.19	97.87	107	10:47

Weilai 1R (Future 1R) 2019-093F 44884						in space
China Central Television (CCTV) satellite developed by Beijing MinoSpace Technology company to be used by the broadcaster for a science outreach TV series. Replaces similar satellite lost 2018 October when its launch vehicle failed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:05	7002	0.0012	615	632	97.18	97.97	248

Yuheng 2019-093G 44885						in space
One of a pair of communication satellites with a military connection carried on this launch. Testing inter-satellite network links with Shuntian.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:02	7001	0.0013	614	633	97.17	97.98	274

Shuntian 2019-093H 44886						in space
One of a pair of communication satellites with a military connection carried on this launch. Testing inter-satellite network links with Yuheng.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:05	7000	0.0014	612	632	97.15	97.97	280

FloripaSat 2019-093J 44887						in space
1U Cubesat developed by SpaceLab students at the Federal University of Santa Catarina (UFSC), Brazil as a technology demonstrator for electronic components in space. Includes an amateur radio package.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:04	7000	0.0014	612	632	97.14	97.97	280

CZ 4B third stage 2019-093K 44888						in space
Launched CBERS 4A and other payloads. Orbit perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 12:23	6912	0.0125	447	620	95.31	97.88	20

2019-094 Atlas V N22 Cape Canaveral Air Force Station						2019 Dec 20, 11:36
Starliner OrbitalFlight Test 1 (Starliner CST-100 #1, Flight 1) 2019-094A 44900						Re-entered - 2019 Dec 22 Life 2 days Returned to Earth
First test mission of Boeing-built spacecraft to be used for ferrying crew and cargo to/from ISS, no crew carried on this mission. On separation from launch vehicle, Starliner received sufficient thrust to enter very low orbit but software problem prevented major thruster firing and caused it to use up propellant on unnecessary attitude control, leaving insufficient for ISS rendezvous. Retro-fire Dec 22 at 12:01 UTC led to touchdown 12:58 UTC at White Sands Space Harbor, New Mexico, USA.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 11:59	6512	0.0088	76	191	87.16	51.63	323
2019 Dec 20, 13:30	6578	0.0031	180	221	88.50	51.59	239
2019 Dec 20, 14:52	6580	0.0029	182	221	88.52	51.59	237
2019 Dec 20, 17:58	6581	0.0028	184	221	88.54	51.59	240
2019 Dec 21, 08:38	6631	0.0018	241	265	89.57	51.58	198
2019 Dec 21, 20:54	6632	0.0011	246	261	89.57	51.59	291

2019-095 Proton-M + Blok DM3 Baikonur Cosmodrome						2019 Dec 24, 12:03
Elektro-L №3 2019-095A 44903						in space
Second generation Russian geosynchronous metsat providing a multispectral image of the complete visible hemisphere every 30 minutes with the interval increased to 15 minutes to cope with emergencies. The satellite also carries a COSPAS-SARSAT search and rescue system receiver. Expected location 165°.8 east. Departed station 165°.8 east 2020 Jun 1, arrived 76° east Jul 1 to replace Elektro L-2 (41105/2015-074A). Elektro L-2 then moved to 14°.5 west.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Dec 24, 23:24	41848	0.0023	35371	35568	1419.93	0.58	231	93° east
2020 Jan 06, 11:25	41851	0.0024	35373	35574	1420.12	0.55	230	144° east
2020 Jan 08, 04:47	42065	0.0027	35573	35801	1431.00	0.54	38	145° east
2020 Jan 23, 03:33	42066	0.0027	35573	35802	1431.03	0.51	42	164° east
2020 Jan 26, 23:37	42158	0.0005	35758	35801	1435.74	0.50	42	165° east
2020 Feb 03, 17:48	42165	0.0004	35770	35803	1436.10	0.48	40	166° east
2020 May 31, 22:25	42165	0.0000	35785	35788	1436.09	0.20	218	166° east
2020 Jun 01, 14:35	42465	0.0072	35783	36391	1451.47	0.20	227	165° east
2020 Jun 22, 03:59	42466	0.0071	35785	36392	1451.53	0.15	227	86° east
2020 Jun 23, 16:51	42236	0.0017	35786	35929	1439.72	0.15	226	84° east
2020 Jul 01, 19:47	42178	0.0004	35784	35816	1436.79	0.13	231	77° east
2020 Jul 05, 19:16	42167	0.0001	35783	35794	1436.19	0.12	228	76° east
2023 Feb 13, 10:01	42165	0.0001	35784	35790	1436.12	0.07	31	76° east

Blok DM-03 rocket stage 2019-095B 44904						in space
Launched Elektro L-3. Initial orbit shown is an estimate of the one immediately after the first engine firing.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 24, 12:21	6562	0.0010	177	191	88.18	51.56	80
2019 Dec 27, 09:45	41424	0.0084	34697	35394	1398.40	0.46	30

2019-096 Rockot + Briz-KM Plesetsk Cosmodrome						2019 Dec 26, 23:11
Gonets 24 (Gonets M-24) 2019-096A 44905						in space
Store and forward communications satellite for Russia's civil/commercial system.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 05:02	7880	0.0005	1498	1506	116.03	82.53	316

Gonets 25 (Gonets M-25) 2019-096B 44906						in space
Store and forward communications satellite for Russia's civil/commercial system.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 04:58	7881	0.0005	1499	1507	116.05	82.53	331

Gonets 26 (Gonets M-26) 2019-096C 44907						in space
Store and forward communications satellite for Russia's civil/commercial system.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 03:02	7882	0.0005	1500	1508	116.08	82.53	343

BLITS-M (Ball Lens In The Space)						in space
Spherical, 22cm cm diameter glass ball to act as laser retro reflector for use in making high precision geodetic measurements. Reportedly failed to separate from the launch vehicle.
failed to separate from rocket

RS-44 + Briz-KM rocket stage 2019-096E 44909						in space
Launched three Gonets-M satellites and BLITS-M. Also carried attached RS-44 amateur radio transponder that remained intentionally attached to the rocket. Lowered orbit after releasing the Gonets M satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 06:16	7720	0.0209	1180	1504	112.52	82.52	270

2019-097 CZ 5 (Y3) Wenchang Space Centre						2019 Dec 27, 12:45
Shijian 20 (Practice 20) 2019-097A 44910						in space
Reportedly a technology demonstration satellite tasked with conducting 84 in-orbit tests and experiments. Onboard equipment is likely related to intelligence-gathering. From 2020 Feb - 2020 Aug, it was co-located with TJS-3 (43874/2018-110A) at 88° east. Carried on the 'return to flight' mission of CZ 5 following its launch failure in 2018.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Dec 27, 18:09	40305	0.8373	179	67674	1342.12	19.40	194
2020 Jan 08, 02:48	42164	0.0005	35763	35808	1436.04	0.14	25	115° east
2020 Apr 04, 22:23	42167	0.0007	35759	35818	1436.20	0.08	248	115° east
2020 Apr 05, 21:23	41962	0.0004	35569	35598	1425.74	0.08	261	117° east
2020 Apr 10, 06:11	42164	0.0002	35777	35795	1436.08	0.10	316	125° east
2020 Aug 25, 15:11	42167	0.0009	35750	35827	1436.21	0.37	134	125° east
2020 Aug 25, 17:22	42206	0.0019	35748	35908	1438.23	0.37	144	125° east
2020 Aug 26, 12:14	42168	0.0029	35666	35914	1436.27	0.38	144	125° east
2020 Dec 30, 13:25	42166	0.0027	35675	35901	1436.17	0.57	194	124° east
2020 Dec 30, 20:07	42251	0.0007	35842	35903	1440.49	0.56	179	124° east
2021 Feb 03, 10:09	42250	0.0008	35836	35907	1440.44	0.65	211	88° east
2021 Feb 05, 08:39	42164	0.0005	35764	35808	1436.08	0.66	301	88° east
2021 Jul 18, 13:11	42163	0.0018	35711	35859	1436.01	0.62	8	88° east
2021 Jul 19, 20:55	42178	0.0014	35743	35857	1436.77	0.34	10	88° east
2021 Jul 21, 12:39	42163	0.0008	35752	35818	1436.01	0.34	11	88° east
2023 Feb 12, 14:53	42164	0.0003	35772	35801	1436.08	1.78	232	34° east

CZ 5 second stage 2019-097B 44911						Re-entered - 2022 May 4 Life 859 days
Launched Shijian 20.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 20:04	43399	0.8468	269	73772	1499.59	18.32	195