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

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

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

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

Users can go straight to specific launches by pointing to the page URL followed by the three digit launch number, eg - https://www.OrbitalFocus/Diaries/Launches/Launches.php?year=2022#001

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

2022-001 Falcon 9 Block 5 (Starlink Group 04-05) Kennedy Space Center						2022 Jan 6, 21:49
Starlink 3321 2022-001A 50803						Re-entered - 2025 Feb 3 Life 1124 days
One member of a simultaneously-launched cluster of forty nine LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 22:04 UTC. All satellites were injected initially into similar orbits at 200-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 11, 20:00	6668	0.0054	254	326	90.31	53.22	180
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jan 6 Life <1 day
Launched forty nine Starlink satellites. Caused to re-enter above the south Atlantic/south western Indian Ocean about 00:59 UTC, 1.3 circuits after lift-off.
Not Catalogued - orbit parameters unavailable

2022-002 Falcon 9 Block 5 (Transporter 3) Cape Canaveral Space Force Station						2022 Jan 13, 15:25
FossaSat-2E1 (WISeSAT 1) 2022-002B 50985						Re-entered - 2023 Jun 23 Life 526 days
2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from EXOport 6 at 16:31 UTC. One of six similar satellites carried on the Transporter 3 launch. All are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 17:00	6903	0.0014	515	535	95.14	97.51	211
Umbra 02 2022-002C 50986						Re-entered - 2024 Nov 8 Life 1030 days
Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Released from launch vehicle at 16:47 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 21:51	6907	0.0010	522	536	95.21	97.51	213
ION SCV-004 (Elysian Eleonora) 2022-002K 50993						in space
Satellite Carrier Vehicle built by D-Orbit - released from launch vehicle at 16:49 UTC carrying a small group of satellites for release 2022 Jan-Feb after departure from Falcon 9: Dodona - Jan 24? Labsat - Jan 28 Stork 1 - Jan 31 Stork 2 - Feb 3 SW1FT - Feb 4 VZLUSat 2 - Jan 26 Also hosts a payload not designed to be released as a separate satellite: Unibap - on-orbit cloud computing demonstrator.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 23:26	6907	0.0010	522	536	95.21	97.51	215
MDASat-1a (Maritime Domain Awareness Satellite) 2022-002M 50995						in space
2U Cubesat from the French South African Institute of Technology. Equipped with an AIS receiver to relay short messages and navigational information from ships at sea. Released from launch vehicle at 16:36 UTC. One of three similar satellites carried on the Transporter 3 launch. All are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 23:27	6907	0.0009	523	535	95.22	97.50	210
Tevel-1 2022-002AF 51013						Re-entered - 2024 Aug 4 Life 934 days
1U Cubesat from the Herzliya Science Center in Israel, carring an amateur radio payload for education purposes. Released from launch vehicle at 16:33 UTC. Identification based on amateur radio observations. One of eight similar satellites carried on the Transporter 3 launch. Contacts reported with all of the amateur radio payloads.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 23:27	6907	0.0009	523	535	95.21	97.50	211
SATLLA-2B 2022-002AG 51014						Re-entered - 2023 Nov 1 Life 657 days
2p PocketQube from Ariel University, Israel. Equipped with an imaging system and an amateur radio payload. Released from EXOport 6 at 16:27 UTC. One of two similar satellites carried on the Transporter 3 launch. SATLLA-2A is reported by its owners as having failed to activate after release from the launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 23:23	6905	0.0013	518	536	95.17	97.52	215
Flock 4X-1 2022-002AK 51017						Re-entered - 2024 Nov 6 Life 1028 days
3U Cubesat - part of Planet's Flock 4X cluster of second generation imaging satellites. Released from the launch vehicle in a fifteen minute sequence commencing at 16:31 UTC. One of forty four similar satellites carried on the Transporter 3 launch. All are in similar orbits and are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 23:23	6905	0.0012	519	536	95.18	97.51	215
Lemur-2 (Ramonamae) 2022-002AP 51021						Re-entered - 2024 May 29 Life 867 days
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. Lemur-2 satellites are named after development and support team members. Released from launch vehicle at 16:32 UTC. One of four similar satellites carried on the Tranporter 3 launch. All are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 17:07	6908	0.0009	524	536	95.23	97.51	224
Grizu-263A 2022-002AT 51025						Re-entered - 2023 Oct 3 Life 628 days
1p PocketQube, Mission details to follow. Released from EXOport 6 at 16:25 UTC. Initial identification by Nico Janssen - based on radio tracking.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 17:02	6905	0.0013	518	536	95.17	97.52	216
Sich 2-1 (Sich 2-30) 2022-002AY 51030						in space
Small satellite from Ukraine's Pivdenne (Yuzhnoye) State Design Office, to monitor the use of land, vegetation, forest, water resources and to reduce the consequences of natural disasters. Released from launch vehicle at 16:48 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 23:26	6907	0.0010	522	536	95.21	97.51	216
SanoSat 1 2022-002AZ 51031						Re-entered - 2024 Feb 7 Life 755 days
1p PocketQube built by Nepalese university students and engineers, carries a gamma radiation sensor to be used as an aid in teaching. Also carries an amateur radio payload. Released from EXOport 6 at 16:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 17:02	6905	0.0013	518	536	95.17	97.51	216
Unicorn-2D 2022-002BA 51032						Re-entered - 2023 Apr 13 Life 455 days
3p PocketQube satellite as a demonstrator of a future constellation of night-time imaging satellites to study global light pollution.. Released from EXOport 6 at 16:25 UTC. One of three similar satellites carried on the Transporter 3 launch. Only one is accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 17:01	6904	0.0011	518	534	95.16	97.50	201
Lemur-2 + OroraTech 1 (Rohovithsa) 2022-002BE 51036						Re-entered - 2024 Aug 3 Life 933 days
6U Cubesat from Spire Global carrying the standard Lemur-2 payload but in a 6U chassis. The other half of the satellite carries a payload from German company Ororatech consisting of a thermal infrared imager to detect, record and analyse the incidence of wildfires on the Earth's surface. Released from launch vehicle at 16:32 UTC. One of three similar satellites carried on the Transporter 3 launch. All are accounted for but the supplementary payloads of the other two are unknown.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 17:07	6908	0.0009	524	536	95.23	97.51	225
IRIS-A (Intelligent Remote Sensing and Internet Satellite) 2022-002BN 51044						in space
2U Cubesat from the Nationa Cheng Kung University of Taiwan. Equipped with an imaging system and a comms package for relaying data from the ground via the Internet. Released from launch vehicle at 16:36 UTC. Initial identification by Nico Janssen - based on radio tracking.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 17:06	6908	0.0009	524	535	95.23	97.50	213
HYPSO-1 (Hyperspectral Satellite for Ocean Observation) 2022-002BX 51053						in space
6U Cubesat from the Norwegian University of Science and Technology to study biological activity near the ocean surface. Released from EXOport 6 at 16:28 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 15:32	6908	0.0008	525	536	95.24	97.50	223
Kepler 16 (Astraeus) 2022-002CB 51057						in space
6U Cubesat - Kepler Gen 1 satellite, part of a planned 140 satellite constellation from Kepler Aerospace carrying a high capacity communications system to provide links between other satellites and the ground, and a prototype of the company's Internet communications system. Released from launch vehicle at 16:36 UTC. One of four similar satellites carried on the Transporter 3 launch. All are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 15:32	6908	0.0008	525	536	95.24	97.51	217
ETV-A1 2022-002CE 51060						in space
16U Cubesat (4x4) from UK company Sen. First in a constellation of video distribution satellites. Released from EXOport 6 at 16:27 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 15:32	6909	0.0009	524	536	95.24	97.51	232
BRO 5 (Breizh Reconnaissance Orbiter 5) 2022-002CF 51061						in space
6U Cubesat (3x2) from Unseen Labs of France for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic. Released from EXOport 6 at 16:29 UTC. Initial identification by Nico Janssen - based on radio tracking.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jan 18, 15:32	6909	0.0009	524	536	95.25	97.51	233	10:00
DEWA-Sat 1 2022-002CM 51067						Re-entered - 2024 Oct 30 Life 1021 days
3U Cubesat from the Dubai Electricity and Water Authority, UAE to demonstrate internet connection of remote station in the area's electricity and water networks. Released from EXOport 6 at 16:28 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 15:33	6909	0.0007	526	536	95.26	97.50	232
ICEYE X14 2022-002CQ 51070						in space
Small satellite fitted with a sythetic aperture radar for Earth surface imaging. Ultimately intended to be part of an eighteen satellite constellation. Released from EXOport 7 at 16:47 UTC. One of two similar satellites carried on the Transporter 3 launch. Both are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jan 18, 23:25	6906	0.0011	520	536	95.19	97.51	216	10:00
Capella 7 (Whitney 5) 2022-002CS 51072						Re-entered - 2023 Aug 26 Life 590 days
Second generation satellite from Capella Space carrying Synthetic Aperture Radar for Earth imaging. Member of a planned thirty satellite constellation. Released from launch vehicle at 16:48 UTC. One of two similar satellites carried on the Transporter 3 launch. Both are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jan 18, 23:25	6906	0.0010	521	535	95.20	97.51	219	10:00
NuX-1 2022-002CT 51073						Re-entered - 2023 Apr 4 Life 446 days
3U Cubesat from Singapore companies NuSpace and Aliena. Equipped with an electronic thruster and a comms package for relaying data from the ground via the Internet. Released from EXOport 6 at 16:28 UTC. Tentative identification from amateur observations using radio - Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 15:20	6901	0.0013	513	532	95.08	97.52	253
Delfi-PQ 2022-002CU 51074						Re-entered - 2024 Jan 9 Life 726 days
3p PocketQube satellite from the Technical University of Delft, Netherlands launched to demonstrate/verify the satellite design. Released from EXOport 6 at 16:24 UTC. Initial identification by Nico Janssen - based on radio tracking.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 18, 15:21	6901	0.0013	514	532	95.09	97.53	251
USA 320 (Starshield 0001) 2022-002CV 51075						Re-entered - 2024 Nov 28 Life 1050 days
US government NRO imaging reconnaissance satellite, probable demonstrator. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Presence on launch vehicle undeclared prior to lift-off. Intentionally caused to re-enter.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jan 18, 15:21	6901	0.0014	514	533	95.10	97.51	249	10:00
2022 Jan 22, 17:45	6906	0.0011	521	536	95.20	97.51	260	10:00
2023 Jan 31, 14:50	6906	0.0003	526	530	95.19	97.47	143	09:53
2024 Mar 23, 14:43	6890	0.0003	509	514	94.86	97.42	255	09:36
2024 Oct 5, 15:48	6811	0.0002	431	435	93.24	97.39	172	09:59
USA 321 (Starshield 0002) 2022-002CX 51077						Re-entered - 2023 Apr 1 Life 443 days
US government NRO imaging reconnaissance satellite, probable demonstrator. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Presence on launch vehicle undeclared prior to lift-off. Intentionally caused to re-enter.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jan 18, 15:22	6902	0.0014	514	533	95.11	97.51	247	10:00
2022 Jan 24, 18:56	6906	0.0011	521	535	95.19	97.51	255	10:00
2023 Jan 31, 14:48	6906	0.0004	526	530	95.19	97.47	195	09:55
2023 Feb 6, 11:56	6889	0.0002	509	512	94.83	97.48	54	09:55
2023 Feb 16, 04:47	6841	0.0003	461	465	93.86	97.47	102	09:55
2023 Feb 20, 10:18	6821	0.0001	442	444	93.44	97.47	82	09:56
2023 Feb 27, 11:41	6792	0.0002	413	415	92.84	97.47	90	09:57
2023 Mar 6, 11:50	6759	0.0001	380	381	92.16	97.47	83	09:59
USA 322 (Starshield 0003) 2022-002CY 51078						Re-entered - 2023 Apr 2 Life 444 days
US government NRO imaging reconnaissance satellite, probable demonstrator. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Presence on launch vehicle undeclared prior to lift-off. Intentionally caused to re-enter.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jan 18, 15:22	6902	0.0014	514	533	95.11	97.51	246	10:00
2022 Jan 21, 11:36	6906	0.0012	520	536	95.19	97.51	262	10:00
2023 Jan 31, 03:44	6906	0.0004	525	531	95.19	97.47	185	09:55
2023 Feb 7, 03:47	6885	0.0002	505	509	94.76	97.47	98	09:55
2023 Feb 16, 03:15	6841	0.0002	462	465	93.86	97.47	40	09:55
2023 Feb 20, 17:05	6821	0.0002	442	444	93.45	97.47	87	09:56
2023 Feb 27, 13:10	6789	0.0002	410	412	92.78	97.47	64	09:57
2023 Mar 6, 11:41	6757	0.0003	376	381	92.12	97.46	116	09:59
USA 323 (Starshield 0004) 2022-002CZ 51079						Re-entered - 2023 Apr 2 Life 444 days
US government NRO imaging reconnaissance satellite, probable demonstrator. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Presence on launch vehicle undeclared prior to lift-off. Intentionally caused to re-enter.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jan 18, 15:22	6902	0.0014	514	533	95.11	97.51	246	10:00
2022 Jan 25, 10:47	6906	0.0011	520	536	95.19	97.51	245	10:00
2023 Jan 31, 03:40	6906	0.0004	525	531	95.19	97.47	174	09:54
2023 Feb 6, 18:13	6887	0.0002	508	511	94.80	97.47	111	09:53
2023 Feb 13, 15:37	6853	0.0002	474	476	94.10	97.46	82	09:54
2023 Feb 20, 10:15	6821	0.0002	442	444	93.44	97.46	82	09:54
2023 Feb 27, 11:30	6788	0.0002	409	411	92.76	97.46	94	09:56
2023 Mar 6, 11:30	6755	0.0001	376	378	92.09	97.46	68	09:57
HADES 2022-002DA 51080						Re-entered - 2024 May 27 Life 865 days
1.5p PocketQube satellite built by AMSAT Spain equipped with a SSTV camera module for Earth observation and an amateur radio package. Weak transmissions detected, indicating the radio aerials did not deploy properly. Released from EXOport 6 at 16:24 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 8, 21:57	6900	0.0014	512	532	95.08	97.52	173
EASAT-2 2022-002DB 51081						Re-entered - 2024 May 23 Life 861 days
1.5p PocketQube satellite built jointly by AMSAT Spain and a group of European University students. Carries a sample of rock from Lanzarote and an amateur radio payload. Weak transmissions detected, indicating the radio aerials did not deploy properly. Released from EXOport 6 at 16:24 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 8, 21:58	6900	0.0015	512	533	95.08	97.52	173
Dodona 2022-002DE 51084						Re-entered - 2024 May 23 Life 861 days
3U Cubesat from the Space Engineering Research Centre of the University of Southern California. Demonstrator mission for a range of satellite systems. Relesed from ION SCV probably Jan 24 around 06:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 4, 17:01	6904	0.0008	520	532	95.16	97.50	148
VZLUSat 2 (Výzkumný a Zkušební Letecký Ústav Satellite) 2022-002DF 51085						in space
3U Cubesat from the Czech Aerospace Research Centre carrying an Earth imaging system and a range of sensors to study x-rays and gamma radiation. Released from ION SCV-04 2022 Jan 26 at 15:02:31 UTC. Initial identification by Nico Janssen - based on radio tracking.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 4, 17:19	6910	0.0015	521	542	95.27	97.50	167
Labsat 2022-002DG 51086						Re-entered - 2024 Sep 10 Life 971 days
3U Cubesat from SatRevolution of Poland testing the performance of space systems in microgravity. Released from ION SCV-04 2022 Jan 28 at about 07:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 4, 17:04	6904	0.0008	520	532	95.15	97.50	145
Stork 1 2022-002DH 51087						Re-entered - 2024 Apr 29 Life 837 days
3U Cubesat from SatRevolution of Poland. Part of a planned fourteen satellite constellation of Earth imaging satellites. Released from ION SCV-04 2022 Jan 31.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 4, 17:13	6909	0.0014	521	541	95.26	97.51	164
Stork 2 2022-002DJ 51088						Re-entered - 2024 May 4 Life 842 days
3U Cubesat from SatRevolution of Poland. Part of a planned fourteen satellite constellation of Earth imaging satellites. Released from ION SCV-04 2022 Feb 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 4, 17:09	6905	0.0011	520	535	95.18	97.50	145
SW1FT 2022-002DK 51089						Re-entered - 2024 May 2 Life 840 days
3U Cubesat from SatRevolution of Poland. Carries an imaging system and an experimental computer system to process and analyse images onboard the satellite. Released from ION SCV-04 2022 Feb 4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 10, 19:16	6907	0.0011	521	537	95.22	97.50	139
Challenger 2022-002xx						in space
3p PocketQube satellite from US company Mini-Cubes. Carries an internet comms package. Released from EXOport 6 at 16:30 UTC. Status unknown. Probably either failed to release from the Falcon 9 or failed to activate.
Orbit parameters awaited
Gossamer Piccolomini 2022-002xx						in space
1U Cubesat from US company Lunasonde for geological studies from orbit. Demonstrator for an eventual constellation. Released from EXOport 6 at 16:28 UTC.
Orbit parameters awaited
MDQubeSat-1 2022-002xx						in space
2p PocketQube from Innova Space of Argentina as a demonstrator of the a satellite to provide internet connection. Released from EXOport 6 at 16:27 UTC. Status unknown. Probably either failed to release from the Falcon 9 or failed to activate.
Orbit parameters awaited
PION-BR1 2022-002xx						in space
1p PocketQube from PION Labs of Brazil, to demonstrate the satellite design. Carries a receiver transmitter to provide internet connectiona and an amateur radio payload. Released from EXOport 6 at 16:27 UTC.
Orbit parameters awaited
Unicorn 1 2022-002xx						in space
2p PocketQube satellite. Mission details to follow. Released from EXOport 6 at 16:24 UTC.
Orbit parameters awaited
Unicorn 2TA-1 (Tartan Artibeus 1) 2022-002xx						in space
1p PocketQube satellite from the Department of Electrical and Computer Engineering at Carnegie Mellon University. Demonstrator for a PocketQube powered by solar cells and testing onboard processing of sensor data. Released from EXOport 6 at 16:24 UTC.
Orbit parameters awaited
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jan 13 Life <1 day
Launched Transporter 3 cluster of 105 satellites. Caused to re-enter above the western part of the Indian Ocean at about 18:00 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-003 LauncherOne (ST-27VPB) Boeing 747, Pacific Ocean off California						2022 Jan 13, 22:52
PAN A (Pathfinder for Autonomous Navigation) 2022-003A 51094						Re-entered - 2024 Jan 30 Life 747 days
3U Cubesat from Cornell University to undertake rendezvous and docking with a companion satellite carried on the same launch vehicle. Part of NASA ELaNa-29 Cubesat cluster. Released from launch vehicle at 23:46 UTC. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 14, 22:32	6879	0.0006	497	505	94.63	44.98	295
TechEdSat 13 2022-003B 51095						Re-entered - 2024 Jul 13 Life 912 days
3U Cubesat from NASA Ames carrying an artificial intelligence/machine learning (AI/ML) module featuring a neuromorphic processor. Also carries a deployable aerobrake to hasten orbit decay at the end of its operational life. Released from launch vehicle at 23:46 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 14, 22:32	6878	0.0005	496	503	94.61	44.98	285
PAN B (Pathfinder for Autonomous Navigation) 2022-003C 51096						Re-entered - 2024 Aug 16 Life 946 days
3U Cubesat from Cornell University to undertake rendezvous and docking with a companion satellite carried on the same launch vehicle. Part of NASA ELaNa-29 Cubesat cluster. Released from launch vehicle at 23:46 UTC. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 14, 22:32	6877	0.0005	496	502	94.59	44.98	253
GEARRS 3 (Globalstar Risk Reduction Satellite) 2022-003D 51097						Re-entered - 2024 Aug 7 Life 937 days
3U Cubesat from Taylor University, investigating the feasibility of using the Globalstar satellite comms network for command and control of cubesats and other small satellite systems. Released from launch vehicle at 23:46 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 14, 18:47	6877	0.0004	496	501	94.59	44.98	274
Stork 3 2022-003E 51098						Re-entered - 2023 Aug 29 Life 593 days
3U Cubesat from SatRevolution of Poland. Part of a planned fourteen satellite constellation of Earth imaging satellites. Released from launch vehicle at 23:46 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 15, 16:49	6875	0.0004	494	499	94.55	44.98	233
Lemur-2 + Adler 1 (Krywe) 2022-003F 51099						Re-entered - 2023 Sep 26 Life 621 days
6U Cubesat carrying the Austrian Particle Impact Detector (APID) to detect very small items of debris in LEO and a radar system with a 100m range. Design is based on the 3U Lemur-2 satellite from Spire but with specialised instrumentation alongside the standard Lemur-2 equipment. The satellite is named after Tom Krywe, current Chief Financial Officer of Spire. Released from launch vehicle at 23:46 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 14, 12:58	6875	0.0005	493	500	94.54	44.98	217
Steamsat 2 2022-003G 51100						Re-entered - 2023 Jun 10 Life 513 days
3U Cubesat - equipped with a water powered thruster from SteamJet Systems. Released from launch vehicle at 23:46 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 14, 22:34	6874	0.0004	493	499	94.54	44.99	222
LauncherOne upper stage 2022-003H 51101						Re-entered - 2023 Oct 4 Life 629 days
Launched seven smalll satellites. Perigee lowered after releasing satellites in order to accelerate orbit decay.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 14, 14:06	6838	0.0054	423	497	93.80	45.03	210

2022-004 CZ 2D Taiyuan Space Centre						2022 Jan 17, 02:35
Shiyan 13 (Test 13) 2022-004A 51102						in space
Purpose unknown - described as "mainly used for space environment exploration and related technical tests". Orbit decayed naturally until mid January 2023 then perigee raised by 135 km followed by a further manoeuvre 2023 March.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jan 17, 17:14	7206	0.0653	357	1298	101.45	98.68	144	09:40
2023 Jan 12, 14:19	7190	0.0658	339	1285	101.12	98.62	174	09:44
2023 Jan 12, 19:50	7241	0.0587	437	1287	102.19	98.62	173	09:44
2023 Jan 13, 11:23	7256	0.0564	469	1287	102.52	98.62	170	09:44
2023 Jan 14, 14:53	7264	0.0566	474	1297	102.68	98.62	166	09:44
2023 Feb 21, 21:37	7263	0.0566	474	1296	102.67	98.60	58	09:39
2023 Feb 22, 13:07	7310	0.0514	556	1308	103.67	98.60	52	09:39
2023 Feb 23, 12:14	7323	0.0501	578	1312	103.95	98.61	48	09:38
2023 Feb 23, 16:49	7328	0.0502	582	1318	104.05	98.60	47	09:38
CZ 2D second stage 2022-004B 51103						in space
Launched Shiyan 13.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 17, 12:09	7204	0.0652	356	1295	101.42	98.68	145

2022-005 Falcon 9 Block 5 (Starlink Group 04-06) Kennedy Space Center						2022 Jan 19, 02:02
Starlink 3366 2022-005A 51104						in space
One member of a simultaneously-launched cluster of forty nine LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 02:17 UTC. All satellites were injected initially into similar orbits at 200-300 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 24, 16:00	6669	0.0054	254	327	90.33	53.22	184
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jan 19 Life <1 day
Launched forty nine Starlink satellites. Caused to re-enter above the south Atlantic/south western Indian Ocean about 04:10 UTC, 1.3 circuits after lift-off.
Not Catalogued - orbit parameters unavailable

2022-006 Atlas V 511 Cape Canaveral Space Force Station						2022 Jan 21, 19:00
USA 324 (GSSAP 5) 2022-006A 51280						in space
One of a pair of simultaneously-launched Geosynchronous Space Situational Awareness Program satellites to act as a sensor in the US Space Surveillance Network (SSN). It carries an experimental sensor look at objects in geosynchronous orbit with a view to identifying satellites and differentiating between payloads, rocket bodies and debris. Separated from launch vehicle Jan 22 at 01:35 UTC. Initial orbit based on ULA pre-launch data, others on amateur observations. 'USA' number is out of sequence.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Jan 22, 01:36	42514	0.0007	36106	36165	1453.97	0.00	351
USA 325 (GSSAP 6) 2022-006B 51281						in space
One of a pair of simultaneously-launched Geosynchronous Space Situational Awareness Program satellites to act as a sensor in the US Space Surveillance Network (SSN). It carries an experimental sensor look at objects in geosynchronous orbit with a view to identifying satellites and differentiating between payloads, rocket bodies and debris. Separated from launch vehicle Jan 22 at 01:45 UTC. Initial orbit based on ULA pre-launch data, others on amateur observations. 'USA' number is out of sequence.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Jan 22, 01:46	42499	0.0011	36075	36168	1453.22	0.00	341
Atlas V upper stage (Centaur) 2022-006C 51282						in space
Launched GSSAP 5 & GSSAP 6. Orbit based on ULA data for the Geosynchronous Transfer Orbit. Currently in an orbit similar to the satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 21, 20:14	24658	0.7320	231	36329	642.25	25.97	0

2022-007 CZ 4C Jiuquan Space Centre						2022 Jan 25, 23:44
Ludi Tance 01-01 (L-SAR 01-01, Land Exploration 01-02) 2022-007A 51284						in space
Earth surface studies satellite equipped with a large, high resolution, Synthetic Aperture Radar operating at L-band frequencies. Will work in conjunction with the L-SAR 01-02 satellite, launched 2022 Feb 26.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jan 26, 09:33	6976	0.0006	594	602	96.65	97.81	242	06:00
2022 Feb 8, 03:07	6982	0.0003	602	606	96.76	97.81	95	06:00
2022 Feb 12, 03:56	6981	0.0002	601	604	96.75	97.81	85	06:00
CZ-4C upper stage 2022-007B 51285						in space
Launched L-SAR 01A. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 26, 07:08	6897	0.0126	432	606	95.01	97.84	31

2022-I01 Nanoracks Cubesat Deployer International Space Station						2022 Jan 26, 12:00
GASPACS (Get Away Special Passive Attitude Control Satellite) 1998-067TB 51439						Re-entered - 2022 May 22 Life 116 days
1U Cubesat from Utah State University - one of four satellites in NASA's ELaNa 38 cluster, it will extend a 1m long inflatable boom to evaluate its use for supporting equipment and in satellite stabilisation. Allocation of Catalogue Number and Designation based on radio observations by amateur observers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 28, 18:28	6794	0.0009	410	422	92.88	51.64	79
FEES 2 (Flexible Experimental Embedded Satellite) 1998-067TD 51441						Re-entered - 2022 Nov 16 Life 294 days
0.3U Cubesat - from Italian company GP Advanced Projects, carrying an imaging system, a message relay system and an amateur radio payload. Will test use of Iridium satellite system for data relay. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 28, 18:28	6794	0.0009	409	422	92.88	51.64	81
PATCOOL (Passive Thermal Coating Observatory Operating in Low-Earth Orbit) 1998-067TE 51442						Re-entered - 2022 Nov 18 Life 296 days
3U Cubesat - one of four satellites in NASA's ELaNa 38 cluster and sponsored by NASA, from the University of Florida to assess feasibility of using cryogenic surface coatings as a method of passive cooling. Actual release was 12:10 UTC, ten minutes behind FEES 2 and GASPACS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 28, 18:28	6793	0.0009	409	421	92.87	51.64	91

2022-I02 Nanoracks Cubesat Deployer International Space Station						2022 Jan 26, 13:30
TARGIT (Tethering and Ranging mission of the Georgia Institute of Technology) 1998-067TC 51440						Re-entered - 2022 May 3 Life 97 days
3U Cubesat - one of four satellites in NASA's ELaNa 38 cluster, sponsored by NASA’s Undergraduate Student Instrument Program. It deployed a small inflatable target on a tether and used a miniaturised LiDAR imaging camera to create a 3D image of it. The target will later be released into independent orbit to allow imaging at longer distances. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 28, 18:28	6794	0.0009	409	422	92.88	51.64	78
2022 Mar 29, 03:53	6754	0.0005	373	380	92.07	51.64	206
DAILI (Daily Atmospheric Ionospheric Limb Imager) 1998-067TF 51443						Re-entered - 2022 Jun 26 Life 151 days
6U Cubesat (6x1) - one of four satellites in NASA's ELaNa 38 cluster, to determine the daytime density of oxygen of the upper atmosphere, between 140 and 300 km, by analysing the spectrum of its dayglow. Actual release was 13:40 UTC, ten minutes behind TARGIT.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jan 28, 18:28	6793	0.0011	408	422	92.86	51.64	75

2022-008 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Jan 31, 23:11
CSG-2 (COSMO-SkyMed Second Generation) 2022-008A 51444						in space
Italian Space Agency second generation, follow-on, Earth imaging satellite equipped with synthetic aperture radar. Precise launch time 23:11:50 UTC, separated from launch vehicle upper stage Feb 1 at 00:11 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Feb 1, 07:22	7001	0.0004	620	626	97.16	97.90	128	17:45
2022 Feb 12, 05:07	6998	0.0002	619	621	97.10	97.89	89	17:45
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Feb 1 Life 1 day
Launched CSG 2. Caused to re-enter above the south eastern Pacific Ocean Feb 1 about 01:05 UTC, 1.3 circuits after lift-off.
Not Catalogued - orbit parameters unavailable

2022-009 Falcon 9 Block 5 Vandenberg Space Force Base						2022 Feb 2, 20:27
USA 326 2022-009A 51445						in space
Government/military imaging reconnaissance satellite. Orbit details are based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6900	0.0010	515	529	95.07	97.40	160	12:17
2022 Apr 9, 02:12	6885	0.0023	491	522	94.75	97.40	33	12:07
2022 Aug 1, 01:49	6881	0.0021	489	518	94.68	97.40	12	12:05
2022 Sep 1, 23:37	6881	0.0020	489	516	94.67	97.41	268	12:05
2023 Mar 12, 23:03	6875	0.0012	489	505	94.55	97.41	90	12:05
2023 Aug 15, 02:21	6875	0.0003	495	499	94.56	97.41	68	12:04
2024 May 15, 01:18	6882	0.0010	497	510	94.69	97.43	166	12:02
2024 Sep 2, 23:32	6878	0.0004	498	503	94.62	97.41	314	12:00
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Feb 2 Life <1 day
Launched USA 326. Caused to re-enter with any surviving fragments hitting the Pacific Ocean near 42° north, 142° west at about 22:05 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-I03 JEM Small Satellite Orbital Deployer International Space Station						2022 Feb 3, 08:55
Light 1 1998-067TG 51509						Re-entered - 2023 Jan 16 Life 347 days
3U Cubesat - a collaboration between the UAE Space Agency and Bahrain’s National Space Science Agency to monitor and study terrestrial gamma ray flashes from thunderstorms and cumulus clouds.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 4, 20:43	6792	0.0011	407	421	92.85	51.65	108

2022-I04 JEM Small Satellite Orbital Deployer International Space Station						2022 Feb 3, 10:30
GT-1 1998-067TH 51510						Re-entered - 2022 Jun 19 Life 136 days
1U Cubesat - from the Georgia Institute of Technology (USA). Demonstrator of the life-cycle of a university-built satellite from initial design to re-entry.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 4, 17:37	6794	0.0009	410	421	92.88	51.64	102

2022-010 Falcon 9 Block 5 (Starlink Group 04-07) Kennedy Space Center						2022 Feb 3, 18:13
Starlink 3181 2022-010F 51461						in space
One member of a simultaneously-launched cluster of forty nine LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 02:17 UTC. All satellites were injected initially into similar orbits at 200-300 km altitude. A solar storm shortly after launch caused higher than expected drag on the satellites, preventing them making orbit-raising manoeures. Many of them re-entered within a couple of weeks.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 8, 22:00	6663	0.0047	254	316	90.22	53.22	182
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Feb 3 Life <1 day
Launched forty nine Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 20:30 UTC, 1.3 circuits after lift-off.
Not Catalogued - orbit parameters unavailable

2022-011 Soyuz-2.1a + Fregat Plesetsk Cosmodrome						2022 Feb 5, 07:00
Cosmos 2553 2022-011A 51511						in space
Military satellite described as a "technological spacecraft… equipped with newly developed on-board devices and systems for their development under radiation and heavy charged particles".
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 5, 14:51	8369	0.0005	1987	1995	126.98	67.09	272
2022 Feb 6, 09:55	8374	0.0004	1993	1999	127.11	67.09	268
Fregat rocket stage uncatalogued						Re-entered - 2022 Feb 5 Life <1 day
Launched Cosmos 2553. Caused to re-enter - probably near 60° south, 170° east at about 09:50 UTC, about 1.4 circuits after launch.
Not Catalogued - orbit parameters unavailable

2022-012 Soyuz ST-B + Fregat-M (VS-27) Centre Spatiale Guyanaise						2022 Feb 10, 18:09
OneWeb 0410 2022-012A 51622						in space
Broadband distribution satellite for the UK company OneWeb. One of 34 similar satellites carried on this launch, released from the Fregat stage of the launch vehicle in nine batches of four over a period of three hours.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 14, 16:00	6851	0.0015	463	484	94.07	87.40	235
Fregat rocket stage uncatalogued						Re-entered - 2022 Feb 10 Life <1 day
Launched cluster of 34 OneWeb satellites. Directed to destructive re-entry above the Indian Ocean at about 23:50 UTC.
Not Catalogued - orbit parameters unavailable

2022-F01 - failed to reach orbit Rocket 3.3 (Astra LV0008) Cape Canaveral Space Force Station						2022 Feb 10, 20:00
BAMA 1
3U Cubesat from the University of Alabama to demonstrate a drag sail to accelerate orbit decay. Part of NASA's ELaNa 41 cluster, lost when the launch vehicle shroud failed to detach and second stage thrust vectoring failed to perform properly.
INCA (Ionosphere Neutron Content Analyzer)
3U Cubesat from New Mexico State University to study the spectrum of Neutron flux in LEO. Part of NASA's ELaNa 41 cluster, lost when the launch vehicle shroud failed to detach and second stage thrust vectoring failed to perform properly.
QubeSat
2U Cubesat from University of California Berkeley to test and characterise the effects of orbital conditions on quantum gyroscopes built around nitrogen vacancy centres in the mineral diamond. Part of NASA's ELaNa 41 cluster, lost when the launch vehicle shroud failed to detach and second stage thrust vectoring failed to perform properly.
R5-S1
3U Cubesat from NASA Johnson Space Centre to demonstrate a fast, cost effective method to build a Cubesat - precise payload unknown. Part of NASA's ELaNa 41 cluster, lost when the launch vehicle shroud failed to detach and second stage thrust vectoring failed to perform properly.

2022-013 PSLV-XL (PSLV C-52) Satish Dhawan Space Centre						2022 Feb 14, 00:29
EOS 04 (Earth Observation Satellite 4) 2022-013A 51656						in space
Indian remote sensing satellite equipped with Earth imaging radar. Separated from launch vehicle at 00:47 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Feb 14, 07:47	6906	0.0010	521	535	95.20	97.55	249	06:00
Ispiresat 1 2022-013B 51657						in space
Student satellite from the Indian Institute of Space Technolgy and the University of Colorado. Carries an Earth imaging thermal camera. Separated from launch vehicle at 00:47 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 14, 07:51	6905	0.0010	520	533	95.17	97.56	253
INS 2D 2022-013C 51658						Re-entered - 2024 Nov 13 Life 1003 days
Satellite from ISRO acting as a demonstrator for equipment designed for the planned India-Bhutan Joint Satellite (INS-2B). Separated from launch vehicle at 00:47 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 14, 06:28	6905	0.0009	520	533	95.16	97.56	259
PSLV upper stage 2022-013D 51659						in space
Launched EOS 04 and two small satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 14, 07:59	6897	0.0033	496	542	95.01	97.57	339

2022-014 Soyuz-2.1a Baikonur Cosmodrome						2022 Feb 15, 04:25
Progress MS-19 (Progress 7K-MS №449) 2022-014A 51660						Re-entered - 2022 Oct 24 Life 251 days
Supplies and equipment to ISS. Docked with the Poisk module Feb 17 at 07:03 UTC, about three minutes earlier than scheduled. Undocked Oct 23 at 22:45:34 UTC. Retro-fire for four minutes Oct 24 at 01:51 UTC led to destructive re-entry above the southern Pacific Ocean at 02:24 UTC with any surviving fragments hitting the surface a few minutes later.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 15, 04:56	6589	0.0023	195	226	88.71	51.64	98
2022 Feb 15, 11:57	6674	0.0028	278	315	90.44	51.64	329
2022 Feb 16, 16:46	6677	0.0027	281	317	90.49	51.64	325
2022 Feb 17, 12:32	6795	0.0006	413	421	92.91	51.64	139
2022 Oct 23, 14:44	6796	0.0005	414	421	92.92	51.64	8
Soyuz upper stage 2022-014B 51661						Re-entered - 2022 Feb 17 Life 2 days
Launched Progress MS-19.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 15, 08:59	6583	0.0028	186	223	88.58	51.66	66

2022-015 Antares 230+ Wallops Flight Facility						2022 Feb 19, 17:40
Cygnus NG-17 (SS Piers Sellers) 2022-015A 51712						Re-entered - 2022 Jun 29 Life 130 days
Northrop Grumman vehicle carrying supplies to ISS under CRS-2 contract with NASA. First Cygnus Enhanced version capable of boosting the ISS orbit. Capured by ISS Remote Manipulator Feb 21 at 09:44 UTC, about 9 min behind schedule. Docked with downward-facing port of the Unity module at 12:02 UTC. Undocked using Canadarm under ground control 2022 Jun 28, then released into independent orbit at 12:07 UTC. A thruster firing Jun 29 led to re-entry at about 06:55 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 19, 19:20	6662	0.0045	254	313	90.19	51.64	148
2022 Feb 20, 05:07	6669	0.0054	254	327	90.32	51.64	148
2022 Feb 20, 11:18	6716	0.0114	261	414	91.28	51.64	122
2022 Feb 20, 16:27	6790	0.0006	408	416	92.80	51.64	168
2022 Feb 21, 14:01	6795	0.0005	414	420	92.91	51.64	151
2022 Jun 28, 11:40	6795	0.0005	413	420	92.90	51.64	282
2022 Jun 28, 14:54	6798	0.0007	415	424	92.96	51.65	338
2022 Jun 29, 06:05	6659	0.0174	165	397	90.13	51.64	306
NACHOS 1 (Nano-satellite Atmospheric Chemistry Hyperspectral Observation System) 2022-015D 52917						Re-entered - 2023 Feb 3 Life 349 days
3U Cubesat from the US Los Alamos National Laboratory using a new design of heat detector by measuring, mapping and quantifying trace gasses in support of volcanology and climate change research. Released from Cygnus NG-17 2022 Jun 28 at 20:20 UTC after leaving ISS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 29, 19:39	6783	0.0008	399	410	92.65	51.64	318
Antares second stage 2022-015B 51713						Re-entered - 2022 Feb 25 Life 6 days
Launched SS Piers Sellers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 20, 06:36	6621	0.0090	183	303	89.36	51.62	143

2022-016 Falcon 9 Block 5 (Starlink Group 04-08) Cape Canaveral Space Force Station						2022 Feb 21, 14:44
Starlink 3528 2022-016A 51714						in space
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 15:47 UTC. All satellites were injected initially into similar orbits at about 350 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 25, 16:00	6718	0.0001	339	340	91.32	53.22	58
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Feb 21 Life <1 day
Launched forty six Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 17:00 UTC, 1.3 circuits after lift-off.
Not Catalogued - orbit parameters unavailable

2022-017 Falcon 9 Block 5 (Starlink Group 04-11) Vandenberg Space Force Base						2022 Feb 25, 16:12
Starlink 3622 2022-017A 51768						in space
One member of a simultaneously-launched cluster of fifty LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 17:14 UTC. All satellites were injected initially into similar orbits at about 350 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 2, 16:00	6706	0.0001	327	329	91.09	53.22	48
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Feb 25 Life <1 day
Launched fifty Starlinks. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-018 CZ 4C Jiuquan Space Centre						2022 Feb 26, 23:44
Ludi Tance 01-02 (L-SAR 01-02, Land Exploration 01-02) 2022-018A 51822						in space
Earth surface studies satellite equipped with a large, high resolution, Synthetic Aperture Radar operating at L-band frequencies. Will work in conjunction with the L-SAR 01-01, launched 2022 Jan 25.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Feb 27, 04:38	6976	0.0004	595	601	96.65	97.81	267	06:00
2022 Mar 3, 12:48	6981	0.0001	602	604	96.75	97.80	128	06:00
2022 May 25, 02:07	6981	0.0002	602	604	96.75	97.81	90	06:00
2022 May 25, 11:48	6978	0.0003	598	602	96.69	97.81	62	06:00
2022 Jun 7, 02:56	6979	0.0002	599	602	96.70	97.81	104	06:00
2022 Jun 10, 22:54	6981	0.0002	602	604	96.75	97.81	103	06:00
2022 Jun 11, 20:25	6981	0.0002	601	604	96.75	97.81	103	06:00
2022 Dec 7, 10:47	6981	0.0002	601	604	96.75	97.81	63	06:00
2022 Dec 12, 05:49	6986	0.0013	599	616	96.85	97.76	146	06:00
2022 Dec 14, 07:55	6990	0.0002	610	613	96.93	97.81	92	06:00
2022 Dec 30, 11:55	6981	0.0001	602	604	96.75	97.81	116	06:00
CZ-4C upper stage 2022-018B 51823						in space
Launched L-SAR 01B. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 27, 05:36	6885	0.0134	414	599	94.75	97.87	39

2022-019 CZ 8 core alone (Y2) Wenchang Space Centre						2022 Feb 27, 03:06
Chaohu 1 2022-019xx						in space
Small radar imaging satellite produced by the Spacety company.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Chuangxin (Shiyan?) 2022-019xx						in space
Probably a small store-dump communications satellite developed by the Chinese Academy of Sciences, to be used to collect and relay water conservancy, hydrological and meteorological data from remote monitoring stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Hainan 1-01 2022-019xx						in space
Maritime surveillance satellite produced by the Shenzhen Aerospace Dongfanghong Satellite company.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Hainan 1-02 2022-019xx						in space
Maritime surveillance satellite produced by the Shenzhen Aerospace Dongfanghong Satellite company.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Jilin-1 High Resolution 02A 01 (Jilin-1 GF02A 01) 2022-019xx						in space
Chinese high resolution, multi-spectral imaging satellite. Demonstrator for new onboard systems.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Jilin-1 High Resolution 03D 10 (Jilin-1 GF3D 10) 2022-019xx						in space
High resolution, multi-spectral imaging satellite. One of nine similar satellites carried on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Qixing 1 2022-019xx						in space
Mission details to follow.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Taijing-3 01 2022-019xx						in space
Commercial satellite for high-resolution remote sensing using an optical imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Taijing-4 01 2022-019xx						in space
Commercial remote sensing satellite equipped with a radar imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Tianqi 19 2022-019xx						in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Wenchang 1-01 2022-019xx						in space
Small satellite equipped with an Earth imaging system, and produced by the Minospace company.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Wenchang 1-02 2022-019xx						in space
Small satellite equipped with an Earth imaging system, and produced by the Minospace company.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Xidian 1 2022-019xx						in space
Small satellite equipped with an Earth imaging system, and produced by the Minospace company.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
Xingshidai 17 (Daiyun, Star Times 17) 2022-019xx						in space
Remote sensing - equipped with a multispectral Earth imaging system, from ADA Space (Chengdu Guoxing Aerospace Technology company) of China. Also carries a laser communication system and uses an artificial intelligence system to control the creation and processing of images. Part of a planned 100 satellite constellation. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6913	0.0023	519	551	95.34	97.51	267	10:31
CZ 8 upper stage 2022-019U 51842						Re-entered - 2024 Jul 28 Life 882 days
Launched cluster of 22 small satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Feb 27, 09:09	6878	0.0070	451	548	94.61	97.57	212

2022-020 Electron (The Owl's Night Continues) Rocket Lab Launch Complex, New Zealand						2022 Feb 28, 20:37
StriX β 2022-020A 51847						in space
Imaging satellite equipped with a synthetic aperture radar - produced by the University of Tokyo, the Tokyo Institute of Technology, Keio University, Japan Space Systems, and a private company - Synspective Inc of Tokyo. Demonstrator for a future constellation of 25 - 30 satellites to monitor ground movement and ground changes in urban areas. The name derives from the scientific name for the owl and its sensitivity to low levels of light.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Mar 1, 05:18	6942	0.0013	555	573	95.94	97.78	291	09:00
Electron third stage (kick stage) 2022-020B 51848						Re-entered - 2024 May 21 Life 813 days
Launched StriX β. Perigee lowered after releasing satelite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 1, 05:14	6894	0.0061	474	558	94.94	97.09	30
Electron second stage 2022-020C 51849						Re-entered - 2022 Mar 15 Life 15 days
Launched StriX β.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 1, 06:33	6772	0.0313	182	606	92.44	97.73	222

2022-021 Atlas V 541 Cape Canaveral Space Force Station						2022 Mar 1, 21:38
GOES 18 (Geostationary Operational Environmental Satellite) 2022-021A 51850						in space
Imaging meteorological satellite from the North American Atmospheric Administration (NOAA). Also carries a search and rescue radio transponder. Separated from launch vehicle Mar 2 at 01:11 UTC. Reached GEO Drift Orbit Mar 15. Expected location - 136°.8 west. Test location 89°.5 west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Mar 2, 02:48	28462	0.4635	8893	35275	796.45	9.45	180
2022 Mar 8, 04:55	32400	0.2856	16769	35275	967.33	4.69	181
2022 Mar 10, 15:01	34969	0.1911	21909	35272	1084.62	2.66	180
2022 Mar 13, 09:48	38051	0.0949	28063	35283	1231.16	1.34	181
2022 Mar 18, 12:15	42024	0.0016	35579	35713	1428.91	0.06	54	91°.0 W
2022 Mar 21, 10:34	42164	0.0001	35783	35789	1436.08	0.06	286	89°.5 W
2022 May 19, 20:45	42344	0.0002	35960	35973	1445.27	0.04	77
2022 Jun 7, 06:24	42178	0.0005	35781	35819	1436.78	0.05	70	136°.8 W
Atlas V upper stage 2022-021B 51851						in space
Launched GOES-T. Perigee lowered after releasing satellite at orbital apogee.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 8, 06:06	27973	0.4767	8260	34931	776.03	9.66	179

2022-022 Falcon 9 Block 5 (Starlink Group 04-09) Kennedy Space Center						2022 Mar 3, 14:25
Starlink 3542 2022-022A 51852						in space
One member of a simultaneously-launched cluster of forty seven LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 9, 22:00	6715	0.0001	336	338	91.28	53.22	53
Falcon 9 upper stage uncatalogued						in space
Launched forty seven Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 16:40 UTC, 1.3 circuits after lift-off
Not Catalogued - orbit parameters unavailable

2022-023 CZ 2C Xichang Space Centre						2022 Mar 5, 06:01
Xuanming 1 2022-023G 51952						Re-entered - 2024 Jun 8 Life 826 days
(6?)U Cubesat - commercial remote sensing satellite from Xinguan Aerospace. Technology verification vehicle for a future constellation. Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 6, 05:22	6869	0.0016	480	502	94.43	63.44	298
Yinhe 2-01 (Galaxy 2-01) 2022-023xx						in space
One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6869	0.0015	480	501	94.42	63.44	302
Yinhe 2-02 (Galaxy 2-02) 2022-023xx						in space
One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6869	0.0015	480	501	94.42	63.44	302
Yinhe 2-03 (Galaxy 2-03) 2022-023xx						in space
One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6869	0.0015	480	501	94.42	63.44	302
Yinhe 2-04 (Galaxy 2-04) 2022-023xx						in space
One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6869	0.0015	480	501	94.42	63.44	302
Yinhe 2-05 (Galaxy 2-05) 2022-023xx						in space
One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6869	0.0015	480	501	94.42	63.44	302
Yinhe 2-06 (Galaxy 2-06) 2022-023xx						in space
One of a batch of six broadband communication satellites from chinese company Galaxy Aerospace.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6869	0.0015	480	501	94.42	63.44	302
CZ 2C second stage 2022-023H 51953						in space
Launched cluster of seven small satellites. Seems to have raised apogee after releasing satellites, reason unknown but possibly to support instrumentation remaining attached after satellites' deployment. Orbit, Catalogue Number, Designation and orbit subject to confirmation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 6, 05:25	6942	0.0117	483	645	95.95	63.64	247

2022-024 Qased (Messenger) Shahroud Test Centre, Dasht-e Kavir, Iran						2022 Mar 8, 05:05
Nour 2 (Light 2) 2022-024A 51954						Re-entered - 2024 May 17 Life 801 days
6U Cubesat - military satellite launched by the Iranian Revolutionary Guard Corps, probably for low resolution Earth imaging - purpose was announced as "reconnaissance".
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 8, 15:36	6882	0.0013	495	513	94.70	58.30	238
2023 Sep 27, 09:16	6822	0.0018	431	456	93.45	58.28	31
Qased upper stage 2022-024B 51955						in space
Launched Nour 2.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 8, 15:36	6881	0.0010	496	509	94.67	58.30	248

2022-025 Falcon 9 Block 5 (Starlink Group 04-10) Cape Canaveral Space Force Station						2022 Mar 9, 13:45
Starlink 3700 2022-025A 51956						in space
One member of a simultaneously-launched cluster of forty eight LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 16, 14:00	6702	0.0001	323	325	91.01	53.22	88
Falcon 9 upper stage uncatalogued						in space
Launched forty eight Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 16:00 UTC, 1.3 circuits after lift-off
Not Catalogued - orbit parameters unavailable

2022-026 Rocket 3.3 (Astra LV0009) Kodiak Launch Centre, Alaska						2022 Mar 15, 16:22
OreSat0 (Oregon Satellite 0) 2022-026K 52017						Re-entered - 2024 Sep 29 Life 929 days
1U Cubesat from Portland State University. Carries a colour imaging system and an amateur radio payload. Released from launch vehicle at 16:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Mar 17, 17:05	6903	0.0026	507	543	95.14	97.50	229	05:30
SpaceBEE 112 2022-026T 52025						Re-entered - 2024 Jan 12 Life 668 days
0.25U Cubesat from Swarm Technologies to provide a two-way communications system from LEO as part of a 150 satellite constellation. To aid tracking,the satellite carries a radar retro-reflector. It also carries a GPS receiver to help determine its location. One of twenty SpaceBEE satellites carried on the launch. All were aimed at similar orbits and all have been confirmed as active.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Mar 18, 15:17	6903	0.0026	507	543	95.13	97.50	225	05:30
Astra upper stage 2022-026A 52008						Re-entered - 2024 Jan 2 Life 658 days
Launched multiple satellites. A further payload, S4 Crossover, remains intentionally attached to it. S4 Crossover is a Cubesat (6U) from Near Space Launch inc as a demonstrator for a possible future satellite design. It carries an Iridium satellite telephone, a Globalstar transmitter and sensors to monitor radiation and space plasma density.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 15, 18:02	6882	0.0048	470	537	94.69	97.49	274

2022-027 CZ 4C Jiuquan Space Centre						2022 Mar 17, 07:09
Yaogan 34-02 2022-027A 52084						in space
Imaging satellite - orbit is similar to the Yaogan 31 electronic surveillance satellites,and the Initial orbit plane has RAAN about three degrees to the east of that of the third Yaogan 31 triplet (launch no 2021-014). Settled into formation with Yaogan 31 Group 3, sitting 34° of orbit arc behind it and following a near-identical ground track.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 17, 12:23	7472	0.0003	1092	1096	107.14	63.40	262
2022 Mar 18, 11:28	7462	0.0014	1074	1094	106.92	63.39	263
2023 Feb 13, 08:16	7468	0.0026	1070	1109	107.04	63.40	345
CZ 4C third stage 2022-027B 52085						in space
Launched Yaogan 34-02. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 17, 08:43	7396	0.0105	940	1095	105.50	63.40	44

2022-028 Soyuz-2.1a Baikonur Cosmodrome						2022 Mar 18, 15:55
Soyuz MS-21 (Soyuz 11F732A48 № 750) 2022-028A 52086						Re-entered - 2022 Sep 29 Life 195 days Returned to Earth
Carrying crew to ISS - Oleg Artemyev (commander), Denis Matveev and Sergey Korsakov (all Roscosmos). Docked, under manual control by its crew, with the Prichal module of ISS at 19:12 UTC on day of launch - due to an unspecified problem with the 'Kurs' automatic system at 180m from the ISS. Undocked, carrying its original crew 2022 Sep 29, 07:34 UTC. Following retrofire, the descent module landed near Dzhezkazgan, Russia at 10:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 18, 16:26	6590	0.0019	200	224	88.73	51.68	84
2022 Mar 18, 17:55	6796	0.0004	416	421	92.94	51.64	283
2022 Sep 28, 07:10	6794	0.0002	414	417	92.88	51.64	303
Soyuz upper stage 2022-028B 52087						Re-entered - 2022 Mar 21 Life 3 days
Launched Soyuz MS-21.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 18, 16:24	6588	0.0023	195	226	88.70	51.66	76

2022-029 Falcon 9 Block 5 (Starlink Group 04-12) Cape Canaveral Space Force Station						2022 Mar 19, 04:42
Starlink 3537 2022-029A 52088						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 05:41 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 22, 16:00	6686	0.0010	301	315	90.69	53.22	295
Falcon 9 upper stage uncatalogued						in space
Launched fifty three Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 06:55 UTC, 1.3 circuits after lift-off
Not Catalogued - orbit parameters unavailable

2022-030 Soyuz-2.1a + Fregat Plesetsk Cosmodrome						2022 Mar 22, 12:48
Meridian 10 (Meridian-M № 20L) 2022-030A 52145						in space
HEO military/government comsat to support Russian forces, commercial shipping and communication ground stations at northern latitudes across Russia. Third mission for the Meridian-M version. Meridian also supports the clandestine short messaging system formerly provided by the Parus satellites. Moved to stable, operational orbit on or after Apr 18 but orbit data not published until May 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 23, 02:12	26748	0.7252	974	39767	725.61	62.83	270
2022 Apr 2, 02:18	26757	0.7236	1018	39740	725.96	62.79	270
2022 May 18, 15:21	26555	0.7209	1035	39320	717.77	62.75	270
Fregat rocket stage 2022-030B 52146						in space
Launched Meridian 10. Separated from Soyuz launch vehicle together with attached Meridian-M at 12:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 23, 14:04	26589	0.7297	810	39612	719.14	62.80	270

2022-I05 JEM Small Satellite Orbital Deployer International Space Station						2022 Mar 24, 09:00
IHI-Sat 1998-067TJ 52147						Re-entered - 2022 Nov 18 Life 239 days
3U Cubesat from IHI Corporation and the Space Robotics Laboratory of Tohoku University, Japan. Demonstrator of a tracking system for AIS, the identification and short messaging system for use by ships at sea.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 28, 20:08	6793	0.0004	412	418	92.87	51.64	14

2022-I06 JEM Small Satellite Orbital Deployer International Space Station						2022 Mar 24, 12:10
KITSUNE (Kyutech standardized bus Imaging Technology System Utilizing Networking and Electron content measurements) 1998-067TK 52148						Re-entered - 2023 Mar 14 Life 355 days
6U Cubesat from Kyushu Institute of Technology, Japan. Carries a high resolution Earth imaging system and a radio system to collect data from remote ground stations and sensors.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 28, 20:10	6794	0.0003	414	418	92.89	51.64	353

2022-031 CZ 6A (Y-1) Taiyuan Space Centre						2022 Mar 29, 09:50
Tiankun 2 2022-031A 52150						in space
Technology demonstration satellite for satellite bus including an attitude control system, thermal cladding and an onboard processing system for optical imaging. Released from launch vehicle at 10:04 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Mar 29, 15:45	6975	0.0012	588	605	96.61	97.80	262	17:00
Puijang 2 2022-031B 52151						in space
Small technology demonstration satellite, includes an Earth imaging system. Released from launch vehicle at 10:06 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Mar 29, 17:22	6974	0.0011	588	604	96.60	97.78	267	17:00
CZ 6A third stage 2022-031C 52152						in space
Launched Puijang 2 and Taikun 2. Orbit lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 29, 16:05	6952	0.0028	554	592	96.13	97.78	2

2022-032 CZ 11 Jiuquan Space Centre						2022 Mar 30, 02:29
Tianping 2A 2022-032A 52153						in space
Small satellite, one of a simultaneously-launched group of three. Precise purpose unknown but reportedly for space environment studies in LEO and acting as calibration targets for ground-based visual and radar tracking equipment. Probably equipped with an Earth imaging system. Catalogue Number, Designation and orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Mar 30, 08:21	6972	0.0013	585	603	96.56	97.80	283	08:47
Tianping 2B 2022-032C 52155						in space
Small satellite, one of a simultaneously-launched group of three. Precise purpose unknown but reportedly for space environment studies in LEO and acting as calibration targets for ground-based visual and radar tracking equipment. Probably equipped with an Earth imaging system. Catalogue Number, Designation and orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Mar 30, 12:14	6971	0.0015	582	603	96.53	97.80	292	08:47
Tianping 2C 2022-032D 52156						in space
Small satellite, one of a simultaneously-launched group of three. Precise purpose unknown but reportedly for space environment studies in LEO and acting as calibration targets for ground-based visual and radar tracking equipment. Probably equipped with an Earth imaging system. Catalogue Number, Designation and orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Mar 30, 12:04	6971	0.0015	582	603	96.53	97.79	292	08:47
CZ 11 fourth stage 2022-032B 52154						Re-entered - 2022 Apr 7 Life 8 days
Launched Tianping 2A, 2B & 2C.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Mar 30, 06:33	6777	0.0387	137	662	92.54	97.63	322

2022-033 Falcon 9 Block 5 (Transporter 4) Cape Canaveral Space Force Station						2022 Apr 1, 16:24
Spark 1 (LEO 1) 2022-033A 52157						in space
Small satellite from Omnispace, demonstrator for a future LEO comsat constellation to include internet connectivity.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 13:06	7026	0.0012	639	656	97.68	97.95	238
GNOMES 3 (GNSS Navigation and Occultation Measurement Satellite) 2022-033B 52158						in space
Small satellite from PlanetiQ, equipped with radio receivers to observe occultations of MEO navsat signals in order to study the Earth's upper atmosphere and contribute to weather forecasting.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 17:57	7024	0.0012	638	654	97.64	97.95	249
EnMAP (Environmental Mapping and Analysis Program) 2022-033C 52159						in space
German hyperspectral imaging satellite mission to monitor and characterise the Earth’s environment.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Apr 6, 13:01	7023	0.0009	638	651	97.62	97.95	265	10:59
Alfa Crux 2022-033D 52160						Re-entered - 2024 Apr 5 Life 735 days
3U Cubesat from a consortium of Brazilian and UK universities to demonstrate point-to-point and store/forward messaging communications from remote areas.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 12:46	6883	0.0009	499	511	94.72	97.39	282
ARCSAT (Arctic Regional Communications small SATellite) 2022-033E 52161						in space
6U Cubesat from Norway's Defence Research Establishment to to demonstrate the use and relevance of a satellite relay for UHF communication at high latitudes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 15:55	6883	0.0009	499	511	94.72	97.39	278
Lynk Tower 1 2022-033F 52162						in space
Small satellite from Lynk Global providing two-way connectivity for broadband, voice, and text messaging globally.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 12:43	6882	0.0009	497	510	94.69	97.39	260
ION SCV-005 (Almighty Alexius) 2022-033G 52163						Re-entered - 2024 Aug 6 Life 858 days
Satellite Carrier Vehicle built by D-Orbit - released from launch vehicle at 17:50 UTC carrying a small group of satellites for later deployment: Plantsat - released Apr 9, KLEOS, KSM 2c - Released Apr 11, KLEOS, KSM 2d - Released Apr 11, SUCHAI 2 - released Apr 13, SUCHAI 3 - released Apr 14, KLEOS, KSM 2a - released May 9, KLEOS, KSM 2b - released May 9. Also carries a hosted payload from Upmosphere consisting of a wooden box containing personal items for clients wishing to deposit something on-orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 12:44	6882	0.0009	497	510	94.69	97.39	261
2022 Apr 14, 11:48	6881	0.0010	496	510	94.68	97.39	226
2022 Apr 18, 12:07	6882	0.0011	496	511	94.69	97.44	208
2022 Apr 19, 11:48	6882	0.0011	496	512	94.70	97.47	201
2022 Apr 24, 11:51	6883	0.0013	496	514	94.72	97.59	181
2022 Apr 25, 11:32	6883	0.0014	496	515	94.73	97.62	177
Hawk 4B (Cluster 4 #2) 2022-033J 52165						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
Hawk 4A (Cluster 4 #1) 2022-033L 52167						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. One of three similar satellites carried on this launch. All were aimed at similar orbits and are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 17:28	6882	0.0009	498	510	94.69	97.39	263
ÑuSat 23 (Annie Maunder) 2022-033M 52168						Re-entered - 2024 Nov 1 Life 945 days
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. One of five similar satellites carried on this launch. All were aimed at similar orbits and are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Apr 6, 12:44	6882	0.0008	498	510	94.70	97.39	267	10:58
MP42 2022-033N 52169						Re-entered - 2024 Oct 20 Life 933 days
Small satellite to built by Nanoavionics of Lithuania to prove the MP42 platform and carring a number of technology tests and technical customer payloads including a 'cell tower in space' for mobile telephony.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 17:26	6880	0.0011	495	510	94.66	97.39	263
Hawk 4C (Cluster 4 #3) 2022-033P 52170						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
Shakuntala 2022-033S 52173						Re-entered - 2024 Jan 13 Life 652 days
Demonstrator satellite from Indian company Pixxel for a hyperspectral Earth imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Apr 6, 11:05	6879	0.0012	492	510	94.64	97.39	256	10:58
BRO 7 (Breizh Reconnaissance Orbiter 7) 2022-033T 52174						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 12:39	6879	0.0012	492	509	94.63	97.39	250
BDSat 2022-033U 52175						Re-entered - 2024 Apr 18 Life 748 days
1U Cubesat from the Czech Republic testing space environment sensors and carrying an amateur radio system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 11:04	6879	0.0013	492	509	94.63	97.39	252
SpaceBEE 128 2022-033AB 52182						Re-entered - 2023 Oct 11 Life 558 days
0.25U Cubesat from Swarm Technologies to provide a two-way communications system from LEO as part of a 150 satellite constellation. To aid tracking,the satellite carries a radar retro-reflector. It also carries a GPS receiver to help determine its location. One of twelve SpaceBEE satellites carried on the launch. All were aimed at similar orbits and are accounted for.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 6, 17:29	6882	0.0008	498	509	94.70	97.38	266
PlantSat 2022-033AH 52188						Re-entered - 2024 Mar 4 Life 703 days
3U Cubesat from the University of Chile and the University of Santiago de Chile to study the development of a plant in a simulated Martian environment. Released from ION SCV-005 2022 Apr 9 at 14:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 14, 14:52	6878	0.0005	496	503	94.61	97.39	248
Kleos Scouting Mission 2c (KSM-2c) 2022-033AJ 52189						Re-entered - 2024 Aug 16 Life 868 days
6U Cubesat - one of two satellites orbiting together, designed to observe maritime activity, particularly of shipping in strategic areas not using AIS. Carries radio receivers to monitor nautical radio bands. Satellite built by GomSpace in Denmark for Luxemburg company Kleos Space. Released from ION SCV-005 on Apr 11 at 07:13 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 15, 16:13	6881	0.0010	496	510	94.68	97.38	221
Kleos Scouting Mission 2d (KSM-2d) 2022-033AK 52190						Re-entered - 2023 Dec 7 Life 615 days
6U Cubesat - one of two satellites orbiting together, designed to observe maritime activity, particularly of shipping in strategic areas not using AIS. Carries radio receivers to monitor nautical radio bands. Satellite built by GomSpace in Denmark for Luxemburg company Kleos Space. Released from ION SCV-005 on Apr 11 at 18:16 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 15, 16:13	6881	0.0010	496	510	94.68	97.38	221
Suchai 3 2022-033AL 52191						Re-entered - 2024 May 25 Life 785 days
1U Cubesat from the University of Chile and the University of Santiago de Chile studying the ionosphere, Released from ION SCV-005 on Apr 13 at 08:03:04 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 15, 17:50	6884	0.0011	498	513	94.73	97.40	203
Suchai 2 2022-033AM 52192						Re-entered - 2024 Oct 6 Life 919 days
1U Cubesat from the University of Chile and the University of Santiago de Chile studying the ionosphere, Released from ION SCV-005 on Apr 14 at 07:45:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 26, 09:28	6879	0.0010	494	508	94.63	97.38	196
Kleos Scouting Mission 2a (KSM-2a) 2022-033AN 52193						Re-entered - 2024 Feb 14 Life 684 days
6U Cubesat - one of two satellites orbiting together, designed to observe maritime activity, particularly of shipping in strategic areas not using AIS. Carries radio receivers to monitor nautical radio bands. Satellite built by GomSpace in Denmark for Luxemburg company Kleos Space. Released from ION SCV-005 on May 9 at 15:49:19 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 16, 12:47	6880	0.0014	493	511	94.66	97.40	131
Kleos Scouting Mission 2b (KSM-2b) 2022-033AP 52194						Re-entered - 2024 Aug 13 Life 865 days
6U Cubesat - one of two satellites orbiting together, designed to observe maritime activity, particularly of shipping in strategic areas not using AIS. Carries radio receivers to monitor nautical radio bands. Satellite built by GomSpace in Denmark for Luxemburg company Kleos Space. Released from ION SCV-005 on May 9 at 18:58:48 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 16, 20:41	6880	0.0014	493	512	94.66	97.40	131
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Apr 1 Life <1 day
Launched Transporter 4 satellite cluster. Caused to re-enter above the Indian Ocean at about 18:45 UTC on day of launch.
Not Catalogued - orbit parameters unavailable

2022-034 Electron (Without Mission a Beat) Rocket Lab Launch Complex, New Zealand						2022 Apr 2, 12:41
BlackSky 18 (Global 18) 2022-034B 52196						in space
Second Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc. Released from kick stage at about 13:41 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 3, 01:44	6813	0.0009	429	440	93.27	53.01	293
BlackSky 20 (Global 20) 2022-034C 52197						in space
Second Generation commercial multi-spectral Earth imaging satellite from BlackSky Global inc. Released from kick stage at about 13:41 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 3, 18:49	6811	0.0010	426	440	93.23	53.00	285
Electron third stage (kick stage) 2022-034D 52198						Re-entered - 2022 Apr 6 Life 4 days
Launched pair of BlackSky Global Gen 2 satellites. Perigee lowered after releasing satelites. Space-Track has this object labelled incorrectly as the Electron second stage.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 2, 20:53	6677	0.0182	177	421	90.50	52.98	54
Electron second stage 2022-034E 52199						Re-entered - 2022 Apr 11 Life 9 days
Launched pair of BlackSky Global Gen 2 satellites. Space-Track has this object labelled incorrectly as the Electron kick stage.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 2, 18:24	6698	0.0208	181	459	90.92	53.03	243

2022-035 CZ 4C Jiuquan Space Centre						2022 Apr 6, 23:47
Gaofen 3-03 2022-035A 52200						in space
Earth imaging satellite equipped with a Synthetic Aperture Radar with resolution of 1m. Sun-synchronous orbit plane matched to its predecessors. The satellites will work together observing targets mainly on the Earth's sea/ocean surface.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Apr 7, 04:13	7120	0.0005	738	745	99.64	98.40	271	06:02
2022 Apr 19, 12:51	7127	0.0005	746	753	99.80	98.42	76	06:02
2022 Apr 21, 19:01	7129	0.0002	750	752	99.85	98.42	100	06:02
2023 Feb 13, 10:11	7129	0.0001	751	752	99.85	98.42	91	06:03
CZ 4C third stage 2022-035C 52201						in space
Launched Gaofen 3-03. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 7, 04:09	7038	0.0113	580	739	97.92	98.40	51

2022-036 Soyuz-2.1b Plesetsk Cosmodrome						2022 Apr 7, 11:20
Cosmos 2554 (Lotos-S1 № 5) 2022-036A 52202						in space
Electronic intelligence gathering - signals intelligence (SIGINT) satellite. Vehicle is based on the design of the Yantar satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 7, 17:58	6948	0.0476	239	900	96.06	67.14	92
2022 Apr 8, 16:12	6950	0.0472	244	900	96.11	67.13	91
2022 Apr 12, 00:15	7281	0.0008	897	909	103.05	67.15	318
2022 Apr 12, 13:37	7285	0.0005	904	911	103.14	67.14	280
2022 Apr 13, 06:28	7283	0.0006	901	910	103.10	67.14	280
Soyuz upper stage 2022-036B 52203						Re-entered - 2022 Nov 30 Life 237 days
Launched Cosmos 2554.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 7, 16:04	6933	0.0457	238	871	95.75	67.14	93

2022-037 Falcon 9 Block 5 (Axiom 1) Kennedy Space Center						2022 Apr 8, 15:17
SpaceX Axiom 1 (Dragon Endeavour flight #3) 2022-037A 52204						Re-entered - 2022 Apr 25 Life 17 days Returned to Earth
Privately funded (Axiom Space) science mission to ISS using SpaceX Crew Dragon. Crew consisting of Michael Lopez Allegria (Commander), Larry Conor (Pilot), Eytan Stibbe (Mission Specialist - Israel) and Mark Pathy (Mission Specialist). Separated from launch vehicle at 15:29 UTC. Docked with forward facing port of ISS Harmony module April 9 at 12:29 UTC, about 16 min earlier than planned. Undocked, carrying original crew, 2022 April 25, 01:10 UTC. Retro-fire at 16:18 UTC was followed by splashdown at 17:06 UTC in the Atlantic Ocean off Florida.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 8, 18:35	6608	0.0034	207	252	89.09	51.64	228
2022 Apr 9, 08:24	6795	0.0005	414	420	92.91	51.64	3
2022 Apr 24, 13:16	6796	0.0006	414	422	92.92	51.64	30
2022 Apr 25, 01:58	6800	0.0005	419	425	93.01	51.64	57
2022 Apr 25, 04:37	6694	0.0134	226	405	90.84	51.65	163
2022 Apr 25, 06:12	6692	0.0133	225	403	90.80	51.64	164
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Apr 8 Life <1 day
Launched Crew Dragon Axiom 1. Caused to re- enter above the Indian Ocean about 45 mins after lift-off.
Not Catalogued - orbit parameters unavailable
Crew Dragon trunk module 2022-037B 52319						Re-entered - 2022 May 14 Life 36 days
Separated from Dragon Endeavour 2022 April 25 at 16:16 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 27, 16:45	6684	0.0123	223	388	90.64	51.89	173

2022-038 CZ 3B Xichang Space Centre						2022 Apr 15, 12:00
Zhongxing 6D (Chinasat 6D) 2022-038A 52255						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. Probably moved to Geosynchronous Drift Orbit Apr 16. Expected location - 125° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Apr 16, 04:12	24378	0.7289	232	35769	631.34	28.46	180
2022 Apr 27, 15:02	42165	0.0002	35777	35797	1436.12	0.07	334	130°.0 E
2022 May 3, 19:18	42222	0.0003	35831	35857	1439.01	0.05	324	126°.3 E
2022 May 7, 16:49	42165	0.0002	35780	35793	1436.08	0.02	357	125°.1 E
CZ 3B fourth stage 2022-038B 52256						in space
Launched Zhongxing 6D. Orbit lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 15, 15:51	23652	0.7225	186	34362	603.34	28.47	179

2022-039 CZ 4C Taiyuan Space Centre						2022 Apr 15, 18:16
Daqi 1 (Atmosphere Environment Monitoring Satellite) 2022-039A 52257						in space
Environment Monitoring satellite equipped with a cluster of active instrumentation, including a LIDAR, to monitor the build-up of aerosols, dust and polluting gases relating to climate change, such as carbon dioxide, in the Earth's atmosphere. An observation from Mauna Kea, Hawaii 2023 Jan 28 showed it is equipped with a downward-pointing green laser to measure pollution.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Apr 15, 21:24	7064	0.0007	681	690	98.47	98.13	233	01:35
2022 Apr 18, 13:30	7071	0.0005	690	697	98.63	98.14	28	01:34
2022 Apr 20, 12:48	7079	0.0000	700	701	98.79	98.13	282	01:34
2023 Jan 28, 07:58	7078	0.0003	698	702	98.78	98.16	93	01:27
2023 Aug 14, 10:09	7079	0.0003	699	703	98.79	98.18	184	01:24
CZ 4C third stage 2022-039B 52258						Re-entered - 2022 May 12 Life 27 days
Launched AEMS. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 15, 21:20	6974	0.0137	500	691	96.59	98.16	63

2022-040 Falcon 9 Block 5 Vandenberg Space Force Base						2022 Apr 17, 13:13
USA 327 (NOSS 3-9 p/l 1?, Intruder?) 2022-040A 52259						in space
Navy Ocean Surveillance Satellite (NOSS)? An expected companion satellite to create a twin satellite formation did not materialise - unclear whether this was by design or error. Orbits based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 23, 02:14	7486	0.0134	1008	1208	107.43	63.45	179
2022 Aug 16, 22:57	7486	0.0128	1012	1204	107.43	63.44	178
2022 Aug 21, 22:54	7484	0.0123	1015	1198	107.40	63.44	178
Falcon 9 upper stage uncatalogued						in space
Launched USA 327. Directed to a destructive re-entry above the eastern Pacific Ocean about 140 minutes after lift-off.
Not Catalogued - orbit parameters unavailable

2022-041 Falcon 9 Block 5 (Starlink Group 04-14) Cape Canaveral Space Force Station						2022 Apr 21, 17:51
Starlink 3810 2022-041A 52262						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 18:50 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 25, 18:00	6705	0.0001	326	328	91.06	53.22	67

2022-042 Falcon 9 Block 5 Kennedy Space Center						2022 Apr 27, 07:52
SpaceX Dragon Crew 4 (Dragon Freedom flight #1) 2022-042A 52318						Re-entered - 2022 Oct 14 Life 170 days Returned to Earth
Crew flight to ISS provided by SpaceX under contract to NASA. Crew members - Kjell Lindgren (NASA), Bob Hines (NASA), Samantha Cristoforetti (ESA) and Jessica Watkins (NASA). Docked with the downward-facing port of the Harmony module at 23:37 UTC on the day of launch. Undocked 2022 Oct 14 at 14:05 UTC carrying original crew. After detaching the trunk module and retro-fire, splashed down off Florida at 20:55 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 27, 08:17	6579	0.0015	191	211	88.51	51.65	3
2022 Apr 27, 12:30	6615	0.0040	210	263	89.23	51.65	229
2022 Apr 28, 13:13	6795	0.0006	413	422	92.92	51.64	43
2022 Oct 14, 11:21	6795	0.0003	414	419	92.90	51.64	303
2022 Oct 14, 17:39	6785	0.0003	405	409	92.71	51.64	304
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Apr 27 Life <1 day
Launched Dragon Crew 4. Caused to re-enter above the Indian Ocean about 45 mins after lift-off.
Not Catalogued - orbit parameters unavailable
Crew Dragon trunk module 2022-042B 54047						Re-entered - 2023 Apr 5 Life 343 days
Separated from Dragon Crew 4 shortly before retrofire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 14, 23:56	6784	0.0006	402	410	92.68	51.33	311

2022-043 CZ 2C Jiuquan Space Centre						2022 Apr 29, 04:11
Siwei Gaojing 1-01 (Superview Neo 1-01) 2022-043A 52320						in space
One of a simultaneously launched pair of commercial remote sensing satellites from the Siwei Surveying and Mapping Technology Co aimed at producing 3D Earth images.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Apr 29, 16:16	6873	0.0012	487	503	94.52	97.47	276	10:31
2022 May 7, 05:55	6875	0.0012	489	506	94.56	97.46	221	10:31
2022 Oct 16, 21:33	6869	0.0013	482	499	94.42	97.46	28	10:38
2022 Oct 17, 06:51	6874	0.0012	488	504	94.53	97.46	68	10:38
2025 Feb 27, 13:29	6864	0.0001	486	487	94.33	97.38	110	10:56
Siwei Gaojing 1-02 (Superview Neo 1-02) 2022-043C 52322						in space
One of a simultaneously launched pair of commercial remote sensing satellites from the Siwei Surveying and Mapping Technology Co aimed at producing 3D Earth images.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Apr 29, 16:15	6871	0.0013	484	502	94.47	97.47	290	10:31
2022 Jun 1, 18:40	6873	0.0020	481	508	94.51	97.47	160	10:32
2022 Oct 9, 21:42	6869	0.0020	477	505	94.42	97.46	68	10:38
2022 Oct 10, 05:21	6874	0.0012	488	505	94.54	97.46	65	10:38
2025 Feb 27, 14:12	6864	0.0001	485	486	94.32	97.38	78	10:56
CZ 2C second stage 2022-043D 52323						Re-entered - 2023 Jun 20 Life 417 days
Launched pair of Superview Neo 1 satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Apr 29, 07:06	6811	0.0091	371	495	93.24	97.56	25

2022-044 Angara 1.2 Plesetsk Cosmodrome						2022 Apr 29, 19:56
Cosmos 2555 2022-044A 52330						Re-entered - 2022 May 17 Life 18 days
Possible imaging reconnaissance satellite. Re-entry occurred within four weeks and there were no orbit adjustments. Separated from launch vehicle at 20:18 UTC. LTDN matches Cosmos 2551 (49127/2021-081A) that also re-entered naturally with no significant orbit changes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Apr 30, 05:08	6664	0.0011	278	293	90.22	96.45	240	11:30
2022 May 17, 22:17	6504	0.0014	117	135	87.00	96.42	229	11:29
Orbit insertion stage uncatalogued						Re-entered - 2022 Apr 29 Life <1 day
Launched Cosmos 2555. Re-entered above the central Pacific Ocean at around 23:30 UTC after 2.3 revolutions. Orbit listed was attained after releasing the satellite and is based on analysis of amateur observations over Europe of a gas cloud resulting from the engine firing that caused reentry.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6945	0.0415	279	855	96.00	96.45	240

2022-045 Falcon 9 Block 5 (Starlink Group 04-16) Cape Canaveral Space Force Station						2022 Apr 29, 21:27
Starlink 3889 2022-045A 52331						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 22:26 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 4, 18:00	6699	0.0001	320	322	90.94	53.22	55
Falcon 9 upper stage uncatalogued						in space
Launched fifty three Starlink satellites. Caused to re-enter with surviving fragments hitting the south Atlantic/south western Indian Ocean about 23:30 UTC, 1.3 circuits after lift-off
Not Catalogued - orbit parameters unavailable

2022-046 CZ 11H Towed barge 'Tai Rui', East China Sea - 32°.2 N, 123°.8 E						2022 Apr 30, 03:30
Jilin-1 High Resolution 04A 01 (Jilin-1 GF4A 01) 2022-046A 52388						in space
Chinese high resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 1, 09:25	6917	0.0012	530	547	95.41	97.53	284	11:20
Jilin-1 High Resolution 03D 07 (Jilin-1 GF3D 07) 2022-046B 52389						in space
Chinese high resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 1, 09:25	6916	0.0010	531	545	95.40	97.54	284	11:20
Jilin-1 High Resolution 03D 06 (Jilin-1 GF3D 06) 2022-046C 52390						in space
Chinese high resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 1, 09:25	6916	0.0012	529	546	95.39	97.53	284	11:20
Jilin-1 High Resolution 03D 05 (Jilin-1 GF3D 05) 2022-046D 52391						in space
Chinese high resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 1, 22:15	6915	0.0013	528	546	95.38	97.55	288	11:20
Jilin-1 High Resolution 03D 04 (Jilin-1 GF3D 04) 2022-046E 52392						in space
Chinese high resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 1, 20:52	6915	0.0014	527	546	95.38	97.54	287	11:20
CZ 11 fourth stage 2022-046F 52393						Re-entered - 2022 May 29 Life 29 days
Launched cluster of Jilin 1 satellites. Perigee lowered after after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 2, 14:58	6763	0.0305	178	591	92.25	97.27	314

2022-047 Electron (There And Back Again) Rocket Lab Launch Complex, New Zealand						2022 May 2, 22:49
SpaceBEE 140 2022-047F 52399						Re-entered - 2024 Mar 7 Life 675 days
0.25U Cubesat from Swarm Technologies to provide a two-way communications system from LEO as part of a 150 satellite constellation. To aid tracking,the satellite carries a radar retro-reflector. It also carries a GPS receiver to help determine its location. One of twenty four SpaceBEE satellites carried on this launch. All were aimed at similar orbits, confirmation of activation awaited.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 10, 15:40	6906	0.0008	522	533	95.18	97.45	307	11:12
TRSI 3 2022-047AA 52418						Re-entered - 2024 Jun 7 Life 767 days
1p PocketQube satellite conducting tests on decoding weak signals and testing a very small satellite transmit/receive aerial.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 10, 14:06	6906	0.0008	523	534	95.20	97.45	315	11:11
MyRadar 1 2022-047AB 52419						Re-entered - 2024 Aug 20 Life 841 days
1p PocketQube satellite demonstrating a weather reporting system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 10, 14:06	6906	0.0008	523	534	95.20	97.45	315	11:11
TRSI 2 2022-047AC 52420						Re-entered - 2024 May 31 Life 760 days
1p PocketQube satellite conducting tests on decoding weak signals and testing a very small satellite transmit/receive aerial.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 10, 14:06	6906	0.0008	523	534	95.20	97.45	316	11:11
Unicorn 2x 2022-047AD 52421						Re-entered - 2023 Jun 6 Life 400 days
3p PocketQube satellite from Alba Orbital carring a night time imaging sensor to monitor light pollution across the globe. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 10, 14:06	6906	0.0008	522	534	95.19	97.45	316
BRO 6 (Breizh Reconnaissance Orbiter 6) 2022-047AE 52422						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 10, 14:09	6908	0.0007	525	534	95.23	97.45	328
Aurorasat 1 2022-047xx						in space
1.5U Cubesat from Aurora Technologies to demonstrate a water powered thruster and a de-orbit system using 'plasma drag' greated by an electrically charged ribbon.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6906	0.0008	523	534	95.20	97.45	316	11:11
E-Space Demo 1 2022-047xx						in space
Small satellite to demonstrate satellite systems and payload for a future constellation for Internet communications.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6906	0.0008	523	534	95.20	97.45	316	11:11
E-Space Demo 2 2022-047xx						in space
Small satellite to demonstrate satellite systems and payload for a future constellation for Internet communications.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6906	0.0008	523	534	95.20	97.45	316	11:11
E-Space Demo 3 2022-047xx						in space
Small satellite to demonstrate satellite systems and payload for a future constellation for Internet communications.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6906	0.0008	523	534	95.20	97.45	316	11:11
Electron second stage 2022-047AL 52428						Re-entered - 2022 May 18 Life 16 days
Launched cluster of 34 satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 10, 06:16	6720	0.0247	176	508	91.37	97.45	226
Electron third stage (kick stage) 2022-047xx						in space
Launched cluster of 34 satellites. Copia - from Astrix Astonautics of New Zealand intentionally remains attached and aimed to demonstrate a large, inflatable solar panel for 1U Cubesats. Test inflation proved successful.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6909	0.0008	525	536	95.25	97.45	339

2022-048 CZ 2D Taiyuan Space Centre						2022 May 5, 02:38
Jilin-1 Wide Field 01C (Jilin-1 KF01C) 2022-048A 52443						in space
Imaging satellite for Earth resources and land studies, particularly in relation to mining and urban construction industries.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 6, 05:31	6916	0.0012	530	546	95.40	97.68	264	09:47
Jilin-1 High Resolution 03D 27 (Jilin-1 GF3D 27) 2022-048B 52450						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 6, 00:47	6915	0.0013	528	546	95.38	97.68	280	09:47
Jilin-1 High Resolution 03D 28 (Jilin-1 GF3D 28) 2022-048C 52449						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 6, 00:47	6915	0.0013	528	546	95.38	97.68	273	09:47
Jilin-1 High Resolution 03D 29 (Jilin-1 GF3D 29) 2022-048D 52448						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 6, 11:59	6915	0.0012	529	545	95.38	97.68	269	09:47
Jilin-1 High Resolution 03D 30 (Jilin-1 GF3D 30) 2022-048E 52447						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 6, 07:07	6915	0.0013	528	546	95.39	97.68	270	09:47
Jilin-1 High Resolution 03D 31 (Jilin-1 GF3D 31) 2022-048F 52446						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 6, 11:59	6916	0.0013	528	547	95.39	97.68	268	09:47
Jilin-1 High Resolution 03D 32 (Jilin-1 GF3D 32) 2022-048G 52445						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 6, 05:31	6916	0.0013	529	546	95.39	97.68	268	09:47
Jilin-1 High Resolution 03D 33 (Jilin-1 GF3D 33) 2022-048H 52444						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 6, 00:47	6916	0.0012	529	546	95.40	97.68	267	09:47
CZ 2D second stage uncatalogued						in space
Launched cluster of Jilin-1 satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-049 Falcon 9 Block 5 (Starlink Group 04-17) Kennedy Space Center						2022 May 6, 09:42
Starlink 3870 2022-049A 52451						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 10:36 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 13, 14:00	6710	0.0001	331	332	91.16	53.22	42
Falcon 9 upper stage uncatalogued						Re-entered - 2022 May 6 Life <1 day
Launched fifty three Starlink satellites. Caused to re-enter after releasing satellites with surviving fragments hitting the south Atlantic/south western Indian Ocean about 11:55 UTC, 1.3 circuits after lift-off
Not Catalogued - orbit parameters unavailable

2022-050 CZ 7 (Y-5) Wenchang Space Centre						2022 May 9, 17:56
Tianzhou 4 2022-050A 52509						Re-entered - 2022 Nov 14 Life 189 days
Supplies and equipment to Chinese Space Station (CSS) in advance of the Shenzhou 14 crew mission. Made rendezvous with CSS and the final docking command was issued May 10 at 00:54 UTC. Docked with the rear port of Tianhe a few minutes later. Also includes a set of hosted payloads consisting of a set of space science and engineering sensors operated independently of the space station mission. Undocked 2022 Nov 9, 06:55 UTC. Retro-fire led to re-entry above the southern Pacific Ocean Nov 14, 23:21 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 9, 22:12	6748	0.0010	363	376	91.93	41.46	288
2022 May 10, 13:55	6763	0.0012	376	393	92.24	41.47	306
2022 Nov 8, 13:27	6766	0.0009	382	394	92.32	41.48	256
2022 Nov 9, 15:31	6766	0.0010	381	394	92.31	41.48	261
2022 Nov 9, 23:28	6763	0.0016	374	395	92.24	41.48	271
Zhixing 3A 2022-050E 54245						Re-entered - 2023 Feb 12 Life 279 days
6U Cubesat carrying an Earth imaging system. Released from Tianzhou 4 on Nov 13 at 22:02 UTC, after Tianzhou departed from CSS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 16, 14:26	6763	0.0015	375	395	92.25	41.48	331
CZ 7 third stage 2022-050C 52511						Re-entered - 2022 May 16 Life 7 days
Launched Tianzhou 4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 9, 23:44	6641	0.0094	201	325	89.77	41.47	174

2022-F02 - failed to reach orbit Hyperbola 1 (Y4) Jiuquan Space Centre						2022 May 13, 07:09
unidentified satellite
Details awaited - lost when the launch vehicle failed to achieve orbit.

2022-051 Falcon 9 Block 5 (Starlink Group 04-13) Vandenberg Space Force Base						2022 May 13, 22:07
Starlink 3951 2022-051A 52533						Re-entered - 2025 Jan 17 Life 980 days
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at about 23:11 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 18, 18:00	6703	0.0001	324	326	91.03	53.22	54
Falcon 9 upper stage uncatalogued						Re-entered - 2022 May 13 Life <1 day
Launched fifty three Starlink satellites. Directed to re-enter above the Pacific Ocean within a few hours of launch.
Not Catalogued - orbit parameters unavailable

2022-052 Falcon 9 Block 5 (Starlink Group 04-15) Cape Canaveral Space Force Station						2022 May 14, 20:40
Starlink 4019 2022-052A 52598						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at about 21:44 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 20, 16:00	6709	0.0001	330	331	91.14	53.22	91
Falcon 9 upper stage uncatalogued						Re-entered - 2022 May 14 Life <1 day
Launched fifty three Starlink satellites. Directed to re-enter late on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-053 Falcon 9 Block 5 (Starlink Group 04-18) Cape Canaveral Space Force Station						2022 May 18, 10:59
Starlink 4004 2022-053A 52656						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 11:58 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 24, 15:13	6709	0.0002	329	332	91.14	53.21	54
Falcon 9 upper stage uncatalogued						Re-entered - 2022 May 18 Life <1 day
Launched fifty three Starlink satellites. Directed to re-enter late on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-054 Soyuz-2.1a Plesetsk Cosmodrome						2022 May 19, 08:03
Cosmos 2556 (Bars-M №3) 2022-054A 52713						in space
Russian government optical imaging satellite for use in cartography.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 May 19, 11:28	6825	0.0160	338	556	93.52	97.69	72	23:47
2022 May 20, 20:06	6828	0.0157	343	556	93.58	97.69	69	23:47
2022 May 21, 13:28	6839	0.0140	365	557	93.81	97.70	63	23:47
2022 May 21, 17:59	6860	0.0109	407	557	94.25	97.69	62	23:47
2022 May 22, 06:47	6904	0.0050	491	560	95.14	97.70	45	23:47
2022 May 23, 01:54	6947	0.0015	559	579	96.04	97.68	282	23:47
2022 May 23, 05:06	6950	0.0010	565	579	96.10	97.70	271	23:47
2022 Jun 20, 07:47	6935	0.0019	544	570	95.79	97.69	246	23:47
2022 Jul 10, 12:45	6887	0.0005	505	512	94.80	97.69	234	23:48
2022 Sep 30, 15:43	6886	0.0006	504	512	94.78	97.69	331	23:59
2022 Oct 1, 12:33	6885	0.0006	503	511	94.77	97.55	330	23:59
2023 Mar 31, 20:15	6880	0.0009	495	507	94.65	97.55	52	00:10
2023 Nov 22, 03:14	6871	0.0005	489	496	94.47	97.55	317	00:29
2023 Dec 21, 03:29	6870	0.0006	487	496	94.44	97.56	186	00:31
2024 Oct 31, 04:18	6866	0.0014	479	498	94.37	97.57	95	00:59
Soyuz upper stage 2022-054B 52714						Re-entered - 2023 Jun 6 Life 383 days
Launched Cosmos 2556.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 19, 09:53	6824	0.0160	337	555	93.51	97.70	73

2022-055 Atlas V N22 Cape Canaveral Air Force Station						2022 May 19, 22:54
Starliner OrbitalFlight Test 2 (Starliner CST-100 #2, Flight 1) 2022-055A 52715						Re-entered - 2022 May 25 Life 6 days Returned to Earth
Second test mission of Boeing-built spacecraft to be used for ferrying crew and cargo to/from ISS. No crew carried on this mission but it included a cargo, and an instrumented anthropomorphic dummy in one of the seats. Repeat of mission profile for OFT 1 in 2019, necessitated by failure to meet the goals of the earlier mission. Docked with forward-facing port of the Unity module May 21, 00:38 UTC. Undocked May 25, 18:36 UTC. Retro-fire at 23:05 UTC led to a parachute-assisted landing on the White Sands Missile Range at 22:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 20, 05:01	6745	0.0009	361	373	91.88	51.64	274
2022 May 20, 23:38	6796	0.0005	415	421	92.93	51.64	140
2022 May 25, 21:13	6796	0.0006	414	422	92.93	51.64	107
Atlas V upper stage (Centaur) sub-orbital						Re-entered - 2022 May 19 Life <1 day
Launched Boeing Starliner OFT 2. Re-entered the atmosphere above Indian Ocean around one hour after lift off.
See individual satellites for orbit info

2022-056 CZ 2C + YZ-1S Jiuquan Space Centre						2022 May 20, 10:30
LEO Comms Test Satellite A 2022-056A 52716						in space
Demonstrator for an LEO communications system - maybe store-dump or maybe broadband internet. Launch time chosen to match the orbit plane of a similar triplet of satellites launched 2021 Aug 24 (2021-076).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 21, 18:24	7261	0.0018	870	896	102.63	86.00	303
2023 Jun 5, 04:21	7259	0.0019	868	895	102.59	86.00	203
LEO Comms Test Satellite B 2022-056B 52717						in space
Demonstrator for an LEO communications system - maybe store-dump or maybe broadband internet. Launch time chosen to match the orbit plane of a similar triplet of satellites launched 2021 Aug 24 (2021-076). Started to raise orbit at a rate of 5 km per day on May 30. Thruster firing ceased Jun 15 then resumed Jun 22.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 21, 11:32	7258	0.0013	871	890	102.57	86.00	303
2022 May 28, 19:45	7261	0.0013	873	892	102.62	86.00	272
2022 Jun 3, 12:47	7272	0.0013	885	904	102.86	86.00	271
2022 Jun 9, 11:28	7295	0.0027	897	937	103.34	86.00	273
2022 Jun 15, 11:06	7313	0.0032	911	958	103.73	86.00	267
2022 Jun 22, 00:49	7314	0.0033	912	960	103.76	86.01	248
2022 Jul 16, 06:15	7361	0.0026	964	1002	104.75	86.00	258
2023 Jun 4, 20:22	7527	0.0045	1115	1182	108.31	86.01	174
LEO Comms Test Satellite C 2022-056C 52718						in space
Demonstrator for an LEO communications system - maybe store-dump or maybe broadband internet. Launch time chosen to match the orbit plane of a similar triplet of satellites launched 2021 Aug 24 (2021-076).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 21, 18:22	7258	0.0013	870	889	102.56	86.00	298
2022 Jul 28, 18:50	7260	0.0017	870	895	102.61	86.00	85
2023 Jun 5, 04:28	7259	0.0015	871	892	102.59	86.00	193
YZ-1S rocket stage 2022-056D 52719						Re-entered - 2022 May 21 Life 1 day
Launched triplet of LEO communication test satellites. Perigee lowered with a thruster firing at about 12:10 UTC. Re-entered May 21 at 14:53 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 May 20, 17:54	6816	0.0507	92	784	93.34	85.95	299
2022 May 20, 20:59	6787	0.0467	92	726	92.74	85.95	298
2022 May 20, 22:32	6772	0.0448	91	697	92.44	85.95	298
2022 May 21, 05:11	6700	0.0348	89	555	90.97	85.95	297
2022 May 21, 06:10	6687	0.0329	89	529	90.71	85.95	296
2022 May 21, 10:55	6614	0.0219	91	380	89.21	85.95	294
2022 May 21, 12:10	6591	0.0183	92	333	88.75	85.96	293

2022-057 Falcon 9 Block 5 (Transporter 5) Cape Canaveral Space Force Station						2022 May 25, 18:35
Lemur-2 (TennysonLily) 2022-057A 52732						Re-entered - 2024 Mar 14 Life 659 days
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. Lemur-2 satellites are named after development and support team members. One of FOUR similar satellites carried on the Tranporter 5 launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:38	6910	0.0008	526	538	95.28	97.52	235
Pathfinder Technology Demonstrator 3 (PTD-3) 2022-057C 52734						Re-entered - 2024 Sep 14 Life 843 days
6U Cubesat from NASA as the first in a series of missions using a new commercial spacecraft bus. Carried the TeraByte InfraRed Delivery , or TBIRD, payload developed by the Massachusetts Institute of Technology’s Lincoln Laboratory in collaboration with NASA’s Goddard Space Flight Center. It aims to demonstrate a 200 GB/s laser-based comms downlink.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:37	6909	0.0009	525	537	95.26	97.52	229
Cicero-2 2 (Community Initiative for Cellular Earth Remote Observation) 2022-057D 52735						Re-entered - 2024 Sep 9 Life 838 days
6U Cubesat equipped to perform GPS and Galileo radio occultation observations by the Earth's atmosphere and undertake surface remote sensing by reflected navigation satellite signals. One of a simultaneously pair in an upgrade to the existing CICERO constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:37	6909	0.0008	526	537	95.26	97.51	225
GHGSat C3 (Luca) 2022-057F 52737						in space
Small satellite in a constellation being built for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:36	6909	0.0008	525	537	95.26	97.51	221
Planetum 1 2022-057G 52738						Re-entered - 2024 Dec 3 Life 923 days
1U Cubesat from Czech company Spacemaniac. Built for Planetum for astronomical studies by cluster of Prague observatories and planetariums, also carrying an amateur radio payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:36	6909	0.0008	525	536	95.25	97.51	218
Connecta T1.1 2022-057H 52739						in space
3U Cubesat from Turkish company Plan-S as a demonstrator for a constellation of broadband communications satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:36	6909	0.0009	525	537	95.25	97.52	223
Lemur-2 + Hancom payload (Sejong 1) 2022-057J 52740						Re-entered - 2024 Jul 26 Life 793 days
6U Cubesat carrying a payload from the Hancom company of South Korea, equipped with a multispectral Earth imaging system. Design is based on the 3U Lemur-2 satellite from Spire but with specialised instrumentation alongside the standard Lemur-2 equipment.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jun 1, 13:35	6909	0.0010	524	538	95.25	97.53	227	13:09
Cicero-2 1 (Community Initiative for Cellular Earth Remote Observation) 2022-057K 52741						Re-entered - 2024 Sep 18 Life 847 days
6U Cubesat equipped to perform GPS and Galileo radio occultation observations by the Earth's atmosphere and undertake surface remote sensing by reflected navigation satellite signals. One of a simultaneously pair in an upgrade to the existing CICERO constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:35	6909	0.0010	524	537	95.25	97.52	224
Centauri 5 2022-057L 52742						Re-entered - 2024 Oct 1 Life 860 days
6U Cubesat from Fleet Space - one of a planned constellation of 140 satellites to provide internet connectivity for ground based sensors.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:35	6909	0.0008	525	536	95.25	97.51	216
Agile Microsatellite (AMS) 2022-057N 52745						Re-entered - 2023 Oct 17 Life 510 days
6U Cubesat from MIT Lincoln Laboratory carrying a remote sensing payload. It will also be used to demonstrate satellite operations in an extremely low orbit. Released from Sherpa AC-1 before it too was released from the Falcon 9 rocket.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:34	6908	0.0009	524	536	95.23	97.51	207
GHGSat C5 (Diako) 2022-057N 52744						in space
Small satellite in a constellation being built for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:34	6908	0.0009	524	537	95.24	97.52	219
GHGSat C4 (Penny) 2022-057Q 52746						in space
Small satellite in a constellation being built for GHGSat Inc of Montreal. It will monitor greenhouse gases emitted from sources on the ground.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:34	6908	0.0009	524	536	95.23	97.51	209
ÑuSat 28 (Alice Lee) 2022-057R 52747						in space
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video. One of four similar satellites carried on the Transporter 5 launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:33	6908	0.0010	523	536	95.23	97.52	213
Umbra 03 2022-057X 52753						Re-entered - 2024 Apr 8 Life 684 days
Small satellite from US company UMBRA, equipped with a radar imaging system for commercial Earth observation. Released from launch vehicle at 16:47 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:32	6907	0.0010	522	536	95.22	97.51	205
Hawk 5A (Alex Witko, Cluster 5 #1) 2022-057AB 52757						in space
SIGINT (signals intelligence) satellite from Hawkeye 360 to map radio transmissions worldwide. This is a private programme where SIGINT is usually a military/government activity. One of THREE similar satellites carried on the Transporter 5 launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:31	6907	0.0010	522	536	95.21	97.52	208
Vigoride 3 2022-057AE 52760						in space
Satellite carrier from US company Momentus Systems, carrying a number of hosted payloads, Cubesats and PocketQubes to be released in the weeks after launch. Planned lifetime for the hosted payloads is six months. Experienced several problems after departing the launch vehicle the major of which was the solar array failing to function at full capacity, restricting the ability to release the satellites and provide power to the hosted payloads. Satellites: Fossasat 2E 9 - 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity - not released. Fossasat 2E 10 - 2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity - not released. Fossasat-2E 11 - released May 28, Fossasat-2E 12 - released May 28, Fossasat-2E 13 - released Jul 18, Veery Hatchling (Orion/FS-1) - released Jul 18, Fossasat 2E 7 - released Jul 30, Fossasat 2E 8- released Jul 30, SelfieSat - released late-August.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:30	6906	0.0011	521	536	95.20	97.52	205
2022 Jul 18, 03:10	6906	0.0013	519	537	95.19	97.52	55
2022 Jul 30, 13:37	6906	0.0012	519	536	95.19	97.52	16
ION SCV-006 (Thrilling Thomas) 2022-057AF 52761						in space
Satellite Carrier Vehicle built by D-Orbit carrying a pair of satellites for later deployment: Guardian - released Jul 5 at 12:54 UTC, SBUDNIC - released 2022 Jun 9 at 09:31:27 UTC. Also carries two hosted payloads: Crypto 1 - protype 1U Cubesat for undertaking cryptographic transactions from an orbiting space vehicle. Gen 01 - from secretive, possibly Italian, company/organisation called Genergo, testing a novel space propulsion system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:30	6906	0.0011	520	536	95.20	97.52	206
ICEYE X17 2022-057AG 52762						in space
Small satellite fitted with a sythetic aperture radar for Earth surface imaging. One of FIVE similar satellites carried on the Transporter 5 launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jun 1, 13:30	6906	0.0011	520	536	95.19	97.52	208	13:09
Sherpa AC-1 2022-057AH 52763						in space
Satellite carrier vehicle carrying two hosted paylods: Huginn - demonstrator for a navigation system in LEO, TROOP 3 (Train Rapid on Orbit Payload) - carrying a number of payloads for paying customers and designed to operate for eight years. Also released three satellites while still attached to the Falcon 9: Agile Microsatellite - see separate entry, CNCE 4 - see separate entry, CNCE 5 - see separate entry.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:29	6906	0.0012	519	536	95.19	97.52	203
Urdaneta (ArmSat 1) 2022-057AK 52765						in space
16U-CubeSat from Spanish company Satlantis, equipped with a camera and a binocular telescope for Earth imaging.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:27	6905	0.0013	518	536	95.17	97.52	200
Varisat 1C (Celestis 21) 2022-057AL 52766						in space
6U Cubesat from US company OmniTeq to test use of satellites to carry communications from ships at sea using HF frequencies.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 2, 00:34	6905	0.0013	517	536	95.17	97.52	201
CNCE 4 (Cubesat Networked Communications Experiment) 2022-057AM 52767						Re-entered - 2024 Apr 23 Life 699 days
3U Cubesat from the US Missile Defense Agency to demonstrate networked radio communication between satellites on orbit. One of a simulaneously-launched pair released from Sherpa AC-1 before it too was released from the Falcon 9 rocket.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:27	6905	0.0013	518	535	95.16	97.51	199
CNCE 5 (Cubesat Networked Communications Experiment) 2022-057AN 52768						Re-entered - 2024 Apr 18 Life 694 days
3U Cubesat from the US Missile Defense Agency to demonstrate networked radio communication between satellites on orbit. One of a simulaneously-launched pair released from Sherpa AC-1 before it too was released from the Falcon 9 rocket.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:27	6905	0.0013	517	535	95.16	97.51	199
Platform 1 (Sharedsat 2141) 2022-057AQ 52770						in space
6U Cubesat from Endurosat carrying a number of unspecified payloads.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:26	6904	0.0013	517	535	95.16	97.51	193
Spark 2 (Omni LEO 2) 2022-057AR 52771						in space
Small satellite from Omnispace, demonstrator for a future LEO comsat constellation to include internet connectivity.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:25	6904	0.0014	516	535	95.15	97.52	196
C-POD 1 (Cubesat Proximity Operations Demonstration) 2022-057AS 52772						Re-entered - 2024 Jun 9 Life 746 days
3U Cubesat - one of two satellites launched as a joined pair, making 6U, from NASA Ames to demonstrate rendezvous, station keeping and docking of Cubesats. Separated from C-POD 2 (52780/2022-057BB) on 2022 Oct 20 around 06:30-07:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:25	6904	0.0014	516	535	95.14	97.52	194
FossaSat-2E 11 2022-057AS 52750						Re-entered - 2023 Sep 8 Life 471 days
2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride May 28.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:29	6905	0.0012	519	535	95.18	97.52	210
FossaSat-2E 12 2022-057AT 52773						Re-entered - 2023 Oct 31 Life 524 days
2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride May 28.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:29	6905	0.0012	519	536	95.18	97.52	210
SBUDNIC (Satellite by Brown University, D-Orbit, and the National Italian Council for Research) 2022-057AU 52774						Re-entered - 2023 Aug 10 Life 442 days
3U CubeSat developed by Brown University in collaboration with the Institute on Atmospheric Pollution of the National Research Council of Italy to collect and panoramic views of space. Released from ION SCV-006 Jun 9 at 09:31:27 UTC. After its mission is complete, SBUDNIC will deploy a drag sail to deorbit itself.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 21, 14:19	6902	0.0009	518	530	95.11	97.52	149
Guardian 1 2022-057AV 52775						in space
6U CubeSat from by Aistech carrying a multispectral telescope for imaging to support commercial services linked to environmental sustainability. Released from ION SCV-006 Jul 5 at 12:54 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 13, 13:41	6908	0.0012	522	538	95.24	97.52	86
Fossasat-2E 13 2022-057AW 52776						Re-entered - 2024 Feb 3 Life 619 days
2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride 2022 Jul 18 ~08:00-09:00 UTC together with Veery Hatchling (52777/2022-057AX).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 29, 13:39	6903	0.0015	514	535	95.13	97.52	10
Veery Hatchling (Veery FS-1) 2022-057AX 52777						Re-entered - 2024 Apr 11 Life 687 days
1p PocketQube from Fossasat built for Careweather carrying a wind scatterometer as a demonstrator for a future constellation of weather monitoring satellites. The satellite carries a four-panel drag device to shorten orbital lifetime. Separated from Vigoride 3 2022 Jul 18, ~08:00-09:00 UTC together with Fossasat 2E-13 (52776/2022-057AW)
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 29, 13:38	6903	0.0015	514	535	95.13	97.52	10
FossaSat-2E 7 2022-057AY 52778						Re-entered - 2023 Aug 22 Life 454 days
2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride Jul 30.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 13:11	6906	0.0013	519	537	95.19	97.52	344
FossaSat-2E 8 2022-057AZ 52779						Re-entered - 2023 Oct 31 Life 524 days
2p PocketQube developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity. Released from Vigoride Jul 30.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 11, 11:24	6906	0.0013	519	537	95.20	97.52	341
SelfieSat 2022-057BA 53951						Re-entered - 2024 Sep 6 Life 835 days
2U Cubesat - from NTNU of Norway. Equipped with external LCD-display to show pictures sent in by the public. A camera mounted on an arm will photograph the screen with the Earth in the background. Released from Vigoride 3 late-August and initially identified by amateur observers using radio techniques. Space-Track eventually published orbit data at the end of September.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 27, 13:38	6905	0.0011	519	535	95.17	97.53	166
C-POD 2 (Cubesat Proximity Operations Demonstration) 2022-057BB 52780						Re-entered - 2024 Jun 14 Life 751 days
3U Cubesat - one of two satellites launched as a joined pair, making 6U, from NASA Ames to demonstrate rendezvous, station keeping and docking of Cubesats. Separated from C-POD 1 (52772/2022-057AS) on 2022 Oct 20 around 06:30-07:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 27, 06:16	6899	0.0015	511	531	95.04	97.53	53
Broncosat 1 2022-057xx						in space
1.5U Cubesat from Bronco Space to demonstrate Artificial Intelligence and Machine Learning for analysing Earth Images produced by an onboard imaging system before transmission to Earth. Indication is that the satellite failed to activate properly after release from Falcon 9 upper stage.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:33	6908	0.0009	523	536	95.23	97.51	205
Foresail 1 2022-057xx						in space
3U Cubesat from the University of Turku, Finland equipped with a charged-particle telescope to study the near-Earth radiation environment. Also carries a plasma brake to take the satellite out of orbit at the end of its life. Indication is that the satellite failed to activate properly after release from Falcon 9 upper stage.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 1, 13:35	6909	0.0008	525	536	95.24	97.51	215
Falcon 9 upper stage						Re-entered - 2022 May 25 Life <1 day
Launched Transporter 5 cluster of satellites. Caused to re-enter above the south eastern Pacific Ocean around 20:30 UTC. Carried Nanoracks hosted payload: Mars Demo 1 - to demonstrate debris-free metal cutting in microgravity and a vacuum. The experiment was contained within a closed container and was partially successful in that one of three samples were cut by the saw.
Not Catalogued - orbit parameters unavailable

2022-058 CZ 2C Xichang Space Centre						2022 Jun 2, 04:00
GeeSat 1-01 2022-058A 52785						in space
Small satellite owned by China's Geely automotive group. Part of a system to provide supplementary navigation information to self-driving motor vehicles. One of nine similar satellites carried on this launch. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 2, 10:05	6988	0.0014	600	619	96.88	49.99	288
CZ 2C second stage 2022-058K 52794						in space
Launched cluster of nine Geesats. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 2, 09:59	6912	0.0104	462	606	95.32	50.16	41

2022-059 Soyuz-2.1a Baikonur Cosmodrome						2022 Jun 3, 09:32
Progress MS-20 (Progress 7K-MS №450) 2022-059A 52795						Re-entered - 2023 Feb 7 Life 249 days
Supplies and equipment to ISS. Docked with the Zvezda module at 16:02 UTC (time to be confirmed). Undocked 2023 Feb 7, 04:56 UTC. Retro-fire at 08:04 UTC led to destructive re-entry above the southern Pacific Ocean with any surviving fragments hitting the ocean surface at about 08:44 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 3, 10:01	6583	0.0024	189	221	88.59	51.66	71
2022 Jun 3, 11:31	6795	0.0005	414	420	92.91	51.65	190
Soyuz upper stage 2022-059B 52796						Re-entered - 2022 Jun 5 Life 2 days
Launched Progress MS-20.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 3, 10:04	6582	0.0027	186	221	88.56	51.65	70

2022-060 CZ 2F Jiuquan Space Centre						2022 Jun 5, 02:44
Shenzhou 14 2022-060A 52797						Re-entered - 2022 Dec 4 Life 182 days Returned to Earth
Crew to CSS - Chen Dong (commander), Liu Yang and Cai Xuzhe. Docked with the downward-facing port of the Tianhe module at 09:42 UTC. Initial orbit similar to rocket upper stage. Undocked, carrying original crew, 2022 Dec 4 at 03:01 UTC. Retro-fire at 11:21 UTC led to landing near Jiuquan at about 12:10:29 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 5, 16:28	6766	0.0004	385	391	92.31	41.47	221
2022 Dec 2, 14:10	6768	0.0006	386	394	92.35	41.48	0
CZ 2F third stage 2022-060B 52798						Re-entered - 2022 Jun 21 Life 16 days
Launched Shenzhou 14.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 5, 13:05	6648	0.0108	198	341	89.91	41.47	126
Shenzhou 14 Orbital Module 2022-060G 54704						Re-entered - 2023 Oct 12 Life 494 days
Released from Shenzhou 14 2022 Dec 4, at 11:20 UTC. Space-Track was tardy in issuing orbit info, initial orbit was probably about 385 x 394 km.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 12, 13:06	6765	0.0007	382	392	92.29	41.49	116

2022-061 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Jun 8, 21:04
Nilesat 301 2022-061B 52817						in space
Egyptian comsat providing communication services to the Middle East including TV broadcasting, broadband and internet connectivity. Released from launch vehicle at 21:37 UTC. Expected location - 7° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Jun 9, 13:44	29019	0.7694	312	44969	819.92	18.64	179
2022 Jun 10, 10:00	33671	0.5246	9627	44958	1024.80	7.28	179
2022 Jun 13, 20:52	41929	0.2247	26132	44971	1424.09	1.93	179
2022 Jun 14, 16:39	46815	0.0971	35889	44983	1680.08	0.60	178
2022 Jun 14, 21:36	47103	0.1005	35990	45460	1695.65	0.49	186
2022 Jun 22, 10:53	42165	0.0000	35785	35788	1436.09	0.03	272	10°.3 W
2022 Jul 4, 21:00	42133	0.0002	35748	35761	1434.47	0.02	157	7°.4 W
Falcon 9 upper stage 2022-061B 52818						in space
Launched Nilesat 301.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 10, 08:02	29000	0.7694	309	44934	819.13	18.65	180

2022-F03 - failed to reach orbit Rocket 3.3 (Astra LV0010) Cape Canaveral Space Force Station						2022 Jun 12, 17:43
TROPICS 02 (Time-Resolved Observations of Precipitation structure and storm Intensity with a Constellation of Smallsats)
3U Cubesat - one of a simultaneously-launched pair from NASA in co-operation with MIT Lincoln Laboratory. Carried on first launch of three to set up a constellation of six satellites to study thermodynamics of the troposphere and precipitation in storm centres within the tropical region of the Earth's atmosphere. Lost when the launch vehicle second stage shut down early and failed to reach orbital velocity.
TROPICS 04 (Time-Resolved Observations of Precipitation structure and storm Intensity with a Constellation of Smallsats)
3U Cubesat - one of a simultaneously-launched pair from NASA in co-operation with MIT Lincoln Laboratory. Carried on first launch of three to set up a constellation of six satellites to study thermodynamics of the troposphere and precipitation in storm centres within the tropical region of the Earth's atmosphere. Lost when the launch vehicle second stage shut down early and failed to reach orbital velocity.

2022-062 Falcon 9 Block 5 (Starlink Group 04-19) Kennedy Space Center						2022 Jun 17, 16:09
Starlink 4091 2022-062A 52830						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 16:25 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 22, 14:00	6679	0.0041	273	328	90.53	53.22	56
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jun 17 Life <1 day
Launched fifty three Starlink satellites. Directed to destructive re-entry above the eastern Pacific Ocean at around 17:30 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-063 Falcon 9 Block 5 Vandenberg Space Force Base						2022 Jun 18, 14:19
SARah 1 2022-063A 52887						in space
German military satellite carrying an imaging radar system. Successor to the SAR-Lupe satellites launched 2006-2008. Orbital data ceased to be published as of 2022 Jun 23.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jun 19, 08:32	7125	0.0006	743	751	99.76	98.40	129	05:59
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jun 18 Life <1 day
Launched SARah 1. Directed to destructive re-entry above the mid Pacific Ocean at around 15:30 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-064 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Jun 19, 04:27
Globalstar-2 M087 (Globalstar-2 FM-15) 2022-064A 52888						in space
Part of constellation of satellites providing on-demand telephone and low-speed data communications. Held as a ground spare for more than ten years after launch of the earlier constellation of Globalstar satellites. Released from the launch vehicle at 06:20 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 20, 16:03	7497	0.0009	1111	1125	107.66	51.98	319
2022 Jul 17, 06:30	7497	0.0010	1111	1126	107.66	51.97	27
USA 328 (Starshield 0005) 2022-064B 52889						in space
US government NRO imaging reconnaissance satellite, possible demonstratorj. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Presence on launch vehicle undeclared prior to lift-off. Orbit about 525 km circular, 53° inclination
Orbit classified as 'Secret' - data withheld
USA 329 (Starshield 0006) 2022-064C 52890						in space
US government NRO imaging reconnaissance satellite, possible demonstrator. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Presence on launch vehicle undeclared prior to lift-off. Orbit about 525 km circular, 53° inclination
Orbit classified as 'Secret' - data withheld
USA 330 (Starshield 0007) 2022-064D 52891						in space
US government NRO imaging reconnaissance satellite, possible demonstrator. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Presence on launch vehicle undeclared prior to lift-off. Orbit about 525 km circular, 53° inclination
Orbit classified as 'Secret' - data withheld
USA 331 (Starshield 0008) 2022-064E 52892						in space
US government NRO imaging reconnaissance satellite, possible demonstrator. Design is related the SpaceX Starlink V2 mini satellite and provides a hosting platform for a variety of missions, possibly using the Starlink infrastructure for communications. Presence on launch vehicle undeclared prior to lift-off. Orbit about 525 km circular, 53° inclination
Orbit classified as 'Secret' - data withheld
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jun 19 Life <1 day
Launched Globalstar FM-15 and four US government Starshield satellites. Directed to destructive re-entry above the eastern Pacific Ocean at around 07:45 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-065 KSLV-II (Nuri) Naro Space Centre, South Korea						2022 Jun 21, 07:00
Performance Verification Satellite 2022-065A 52894						in space
Instrumented payload to monitor performance of the rocket during launch and at satellite separation. Released from the launch vehicle at 07:14 UTC. Carries four Cubesats scheduled for release at intervals. All were released on time: STEP Cube Lab-II - released Jun 29, RANDEV - released Jun 30, SNUGLITE 2 - released Jul 3, MIMAN - released Jul 5.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jun 22, 05:30	7079	0.0008	695	707	98.80	98.02	232	15:36
Dummy satellite 2022-065B 52895						in space
1.6 tonne mass to simulate a satellite payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 21, 21:15	7077	0.0007	694	704	98.76	98.02	254
STEP Cube Lab-II (Space Technology Experimental Project CubeSat Laboratory) 2022-065D 52897						in space
6U Cubesat from Chosun University, equipped for Earth imaging in visible and infrared bands of the spectrum. Released from Performance Verification Satellite Jun 29, 07:50 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jun 29, 12:21	7077	0.0007	694	704	98.76	98.02	227	15:35
RANDEV (Repeater Arrangement & Disaster Early View) 2022-065E 52898						in space
3U Cubesat developed by the Korea Advanced Institute of Science and Technology. carrying an imaging system to study hazardous areas around volcanoes, clouds and coasts. Released from Performance Verification Satellite Jun 30 at about 22:50 UTC
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jul 1, 10:40	7076	0.0009	692	704	98.73	98.01	244	15:35
SNUGLITE 2 (Seoul National University Global navigation satellite system Laboratory satellITE) 2022-065F 52899						in space
3U Cubesat from Seoul National University to demonstrate use of radio occultation of navsat signals as a means of measuring aspects of the Earth's upper atmosphere. Released from Performance Verification Satellite Jul 3 at about 08:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jul 4, 14:02	7077	0.0007	693	704	98.74	98.02	215	15:35
MIMAN (Multi-spectral Imaging for Monitoring Aerosol by Nanosatellite) 2022-065G 52900						in space
3U Cubesat from Yonsei University to monitor dust in the upper atmosphere. Released from Performance Verification Satellite Jul 5 at at about 09:30 UTC. Precise orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jul 7, 09:35	7077	0.0007	694	704	98.75	98.02	198	15:35
Unidentified payload 2022-065H 52983						in space
Released from Performance Verification Satellite Jul 7 around 08:00 UTC. Catalogued by Space-Track as a "Dummy Cubesat". Maybe 6U in size. Not listed in published payload schedule.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 7, 12:54	7078	0.0007	695	704	98.77	98.01	199
KSLV-II upper stage 2022-065C 52896						in space
Launched Performance Verification Satellite and a dummy payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 21, 10:08	7064	0.0016	674	697	98.47	98.07	10

2022-066 Kuaizhou 1A Jiuquan Space Centre						2022 Jun 22, 02:08
Tianxing-1 01 2022-066A 52901						Re-entered - 2023 Mar 29 Life 280 days
Described as a test satellite used for experiments such as space environment detection. Low orbit meant that a thruster firing every few days was needed to maintain height and, thereby, LTDN. Orbit adjustment frequency reduced late 2022 and manoeuvres ceased 2023 February 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jun 22, 04:45	6661	0.0012	275	292	90.18	96.76	278	08:29
2022 Jun 24, 14:13	6663	0.0009	279	291	90.22	96.74	233	08:29
2022 Jun 28, 17:30	6659	0.0010	274	288	90.14	96.74	213	08:29
2022 Jun 29, 03:53	6666	0.0011	281	296	90.28	96.74	267	08:29
2023 Feb 1, 21:33	6680	0.0015	292	312	90.56	96.76	50	08:44
2023 Mar 28, 17:55	6509	0.0009	126	137	87.11	96.69	255	08:49
Kaizhou 1A upper stage 2022-066B 52902						Re-entered - 2022 Jun 23 Life 1 day
Launched Tianxing 1. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 22, 06:24	6688	0.0298	111	509	90.72	96.80	319

2022-067 Ariane 5ECA (VA-257) Centre Spatiale Guyanaise						2022 Jun 22, 21:50
GSat 24 (GSat N1) 2022-067A 52903						in space
High capacity comsat built by the Indian Space Research Organisation for NewSpace India Limited (NSIL) to provide high-quality television, telecommunications and broadcasting services. Initially, the entire capacity will be used by Tata Play for direct to home TV. Separated from launch vehicle at 22:29 UTC. Expected location 83° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Jun 23, 14:05	24383	0.7278	259	35751	631.52	6.01	179
2022 Jun 24, 11:02	24374	0.7278	257	35734	631.17	6.01	179
2022 Jun 24, 16:27	26817	0.5719	5103	35775	728.42	3.32	179
2022 Jun 25, 11:09	31365	0.3444	14186	35789	921.38	1.34	181
2022 Jun 28, 12:00	42056	0.0033	35540	35816	1430.55	0.09	332	85°.3 E
2022 Jun 30, 12:49	42032	0.0027	35539	35769	1429.33	0.10	334	88°.5 E
2022 Jul 4, 07:31	42078	0.0013	35644	35755	1431.66	0.09	328	92°.9 E
2022 Jul 5, 09:21	42135	0.0004	35742	35772	1434.59	0.09	239	93°.2 E
2022 Jul 11, 10:00	42166	0.0009	35750	35825	1436.14	0.08	194	93°.5 E
2022 Nov 15, 21:45	42165	0.0002	35777	35796	1436.10	0.01	96	93°.6 E
2022 Nov 17, 12:53	42244	0.0001	35860	35872	1440.15	0.02	81
2022 Nov 17, 19:13	42165	0.0004	35769	35804	1436.09	0.07	191	83°.1 E
MEASAT 3d 2022-067B 52904						in space
Comsat covering Malaysia, Indonesia, South Asia and Australia, replacing the retired MEASAT 3 (29648/2006-056A). Launched 47 minutes into a 100 minute launch window. Separated from launch vehicle at 22:18 UTC. Expected location alongside Measat 3a and Measat 3b at 91°.5 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Jun 23, 04:41	24378	0.7279	255	35745	631.34	5.98	178
2022 Jun 28, 10:44	42090	0.0012	35660	35763	1432.26	0.08	280	89°.1 E
2022 Jul 1, 10:38	42160	0.0005	35761	35802	1435.84	0.10	143	91°.3 E
2022 Jul 2, 22:06	42164	0.0001	35780	35792	1436.06	0.09	112	91°.5 E
Ariane 5 upper stage 2022-067D 52906						in space
Launched Measat 3d and GSat 24.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 24, 07:45	24340	0.7280	243	35681	629.86	6.17	181

2022-068 CZ 2D Xichang Space Centre						2022 Jun 23, 02:22
Yaogan 35-02 Follower 1 2022-068A 52909						Re-entered - 2024 Apr 19 Life 666 days
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 23, 18:14	6872	0.0008	488	499	94.48	35.00	270
2022 Jul 3, 10:54	6872	0.0008	489	499	94.49	34.99	350
2022 Jul 10, 02:57	6875	0.0007	492	502	94.56	34.99	59
2022 Nov 24, 14:19	6875	0.0010	490	503	94.55	35.00	212
2023 Jan 19, 11:43	6869	0.0007	486	496	94.43	35.00	349
2023 Feb 15, 06:10	6865	0.0008	481	493	94.35	35.00	256
2023 Aug 26, 23:38	6837	0.0006	454	463	93.76	34.99	227
Yaogan 35-02 Leader 2022-068B 52908						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 23, 18:13	6869	0.0010	485	498	94.44	34.99	291
2022 Jul 3, 02:26	6872	0.0011	487	502	94.50	35.00	24
2022 Jul 5, 13:08	6875	0.0008	491	502	94.55	35.00	58
2023 Feb 15, 06:11	6873	0.0015	484	505	94.51	35.00	301
2023 Aug 27, 00:18	6871	0.0012	484	501	94.46	35.00	175
Yaogan 35-02 Follower 2 2022-068C 52907						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Ceased manoeuvring 2022 Nov 24, orbit then began to decay naturally and it fell out of the group.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 23, 15:05	6870	0.0009	486	499	94.46	35.00	281
2022 Jul 2, 12:55	6874	0.0006	492	499	94.52	34.99	323
2022 Jul 7, 18:02	6875	0.0006	493	501	94.55	35.00	28
2023 Feb 15, 13:36	6872	0.0005	491	498	94.50	35.00	263
2023 Aug 27, 00:23	6871	0.0013	484	502	94.48	35.00	247
CZ 2D second stage 2022-068D 52910						Re-entered - 2023 Mar 8 Life 258 days
Launched Yaogan group 35 group 2.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 23, 15:05	6871	0.0009	487	499	94.47	35.00	272

2022-069 CZ 4C Jiuquan Space Centre						2022 Jun 27, 15:46
Gaofen 12-03 2022-069A 52912						in space
Earth observation using radar and high resolution optical sensors for Earth imaging to "support land surveys, crop management, urban and road network planning".
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jun 27, 20:03	6975	0.0003	595	599	96.62	97.98	232	22:02
2022 Jun 28, 12:10	6975	0.0006	593	601	96.62	97.99	260	22:02
2022 Jun 29, 08:09	6992	0.0002	612	615	96.97	97.99	181	22:02
2022 Jun 29, 15:52	7000	0.0009	615	628	97.14	97.98	137	22:02
2022 Jun 30, 06:11	7006	0.0003	626	630	97.26	97.98	31	22:02
2022 Jul 1, 18:18	7007	0.0001	628	629	97.28	97.98	116	22:02
2023 Feb 13, 05:02	7005	0.0003	625	629	97.24	97.97	100	22:09
CZ 4 C upper stage 2022-069B 52913						in space
Launched Gaofen 12-03. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 27, 18:47	6923	0.0074	493	596	95.54	97.97	46

2022-070 Electron (CAPSTONE) Rocket Lab Launch Complex, New Zealand						2022 Jun 28, 09:55
CAPSTONE (Cislunar Autonomous Positioning System Technology Operations and Navigation Experiment) 2022-070A 52914						in space
Lunar spacecraft owned and operated by Advanced Space. Purpose of CAPSTONE is to test and verify orbit operational procedures for NASA's planned Lunar Gateway. Released from Rocket Lab's Photon rocket stage Jul 4 at 07:18 UTC. Enter a Near Rectilinear Halo Orbit (NRHO) in Lunar space 2022 Nov 14 for a test/evaluation programme expected to last six months to test evaluate use of the halo orbit.
Earth-Moon Barycentric Orbit
Electron second stage 2022-070B 52915						Re-entered - 2022 Jun 28 Life <1 day
Launched CAPSTONE.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 28, 12:02	6541	0.0013	154	171	87.74	39.11	267
Photon rocket stage (Photon 3) 2022-070C 52916						in space
Instrumented rocket stage that launched CAPSTONE. Intended to make a fly-by of the Moon and return images but none were published. Engine firing Jul 4 at 06:56 UTC placed it in Barycentric orbit after which it released CAPSTONE.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 28, 10:54	6985	0.0627	169	1045	96.83	39.12	330
2022 Jun 30, 17:09	13242	0.4989	257	13470	252.75	39.09	343
2022 Jul 1, 05:46	26657	0.7505	274	40285	721.91	39.05	344
2022 Jul 3, 03:24	41615	0.8405	258	70215	1408.08	39.08	344

2022-071 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Jun 29, 21:04
SES 22 2022-071A 52933						in space
Comsat providing data services, and TV and radio services to North America, South America and the Caribbean. Released from launch vehicle at 21:37 UTC. Expected location 135° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Jun 30, 13:20	24332	0.7253	305	35603	629.54	16.53	179
2022 Jul 1, 09:00	28901	0.4538	9407	35639	814.96	6.28	180
2022 Jul 4, 10:34	42032	0.0003	35640	35668	1429.31	0.06	153	146°.3 W
2022 Jul 4, 18:17	42025	0.0003	35634	35659	1428.95	0.06	169	145°.7 W
2022 Jul 6, 14:06	42079	0.0009	35663	35740	1431.74	0.06	4	142°.6 W
2022 Jul 7, 06:44	42127	0.0006	35724	35774	1434.15	0.06	267	142°.1 W
2022 Jul 12, 17:36	42165	0.0000	35786	35788	1436.11	0.05	286	142°.0 W
2022 Jul 21, 23:44	42165	0.0001	35783	35789	1436.08	0.06	310	142°.0 W
2022 Jul 25, 12:40	42108	0.0000	35729	35731	1433.22	0.06	59	139°.5 W
2022 Jul 31, 09:57	42108	0.0000	35729	35730	1433.19	0.03	62	135°.2 W
2022 Aug 2, 16:27	42165	0.0002	35777	35796	1436.09	0.03	202	135°.0 W
Falcon 9 upper stage 2022-071B 52934						in space
Launched SES 22.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jun 30, 20:50	24331	0.7253	306	35601	629.52	16.54	180

2022-072 PSLV-CA (PSLV C-53) Satish Dhawan Space Centre						2022 Jun 30, 12:30
DS-EO (Earth Observation Satellite 6) 2022-072A 52935						in space
Multispectral Earth imaging payload for land studies, from Singapore's Defence Science and Technology Agency. Separated from launch vehicle at 12:47 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jul 1, 11:51	6946	0.0007	563	573	96.02	9.99	328	21:59
NeuSAR 2022-072C 52937						in space
Small satellite from Singapore carrying an Earth imaging radar system. Separated from launch vehicle at 12:48 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 1, 12:02	6944	0.0009	560	573	95.99	9.99	336
Scoob 1 2022-072D 52938						in space
3U Cubesat - student built satellite from the Research Centre at Singapore's NTU School of Electrical and Electronic Engineering. Equipped with a Solar spectrometer and an Earth imaging system. Separated from launch vehicle at 12:48 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 1, 02:25	6925	0.0024	531	564	95.59	9.90	194
PSLV upper stage + POEM 1 2022-072B 52936						Re-entered - 2024 May 23 Life 693 days
Launched DC-EO and two other satellites. Carries POEM PSLV Orbital Experimental Module 2 carrying six hosted payloads, two of which are from India.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 1, 23:12	6945	0.0008	562	573	96.01	9.99	337

2022-073 Atlas V 541 Cape Canaveral Space Force Station						2022 Jul 1, 23:15
USA 332 (Wide Field of View Testbed) 2022-073A 52940						in space
Testbed for sensors to be employed in the next generation of missile detection satellite that will replace the Space Based Infrared System (SBIRS). Released from the launch vehicle Jul 2, 05:04 UTC. The first orbit listed is an estimate based on information from ULA then, Jul 17, Space-Track started issuing orbit data with initial hint that orbit was raised around Jul 7.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Jul 2, 05:25	42513	0.0007	36106	36164	1453.95	0.00	201
2022 Jul 17, 17:11	42668	0.0012	36240	36340	1461.89	0.05	126
2022 Jul 24, 03:43	42668	0.0012	36238	36341	1461.87	0.05	150
2022 Aug 1, 14:50	42668	0.0013	36237	36344	1461.90	0.07	154
2022 Aug 5, 00:07	42669	0.0012	36238	36343	1461.91	0.08	153
2022 Aug 13, 08:40	42668	0.0012	36238	36342	1461.90	0.09	167
2022 Aug 18, 17:56	42670	0.0012	36239	36344	1461.97	0.11	168
2022 Aug 26, 11:42	42518	0.0001	36138	36143	1454.20	0.12	209
2022 Aug 29, 22:34	42375	0.0001	35992	36001	1446.84	0.14	169
2022 Aug 31, 12:10	42267	0.0026	35781	35997	1441.32	0.14	255
2022 Sep 1, 15:33	42164	0.0001	35783	35788	1436.04	0.13	170	119°.3 E
2023 Jul 25, 14:05	42164	0.0004	35771	35802	1436.07	0.98	54	119°.3 E
USA 333 (USSF-12 Ring) 2022-073B 52941						in space
EELV Secondary Payload Adapter (ESPA) hosting a quantity of secret test/demonstration payloads. Released from the launch vehicle Jul 2, 05:20 UTC. The first orbit listed is an estimate based on information from ULA.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Jul 2, 05:24	42624	0.0018	36167	36323	1459.60	0.01	172
USA 337 2022-073E 53521						in space
Small satellite, possibly a Cubesat (3U or 6U?) with classified payload. Probably released from USA 333 mid-August.
Orbit classified as 'Secret' - data withheld
Atlas V upper stage (Centaur) 2022-073C 52942						in space
Launched WFOV Testbed and USSF-12 Ring. Orbit raised after releasing satellites. Estimated orbits based on ULA information, all others are from amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6870	0.0287	295	689	94.46	28.21	180
estimated orbit	42624	0.0018	36167	36323	1459.60	0.01	172
2022 Aug 23, 05:52	44499	0.0436	36181	40061	1556.99	0.09	9

2022-074 LauncherOne (STP-27A) Boeing 747, Pacific Ocean off California						2022 Jul 2, 06:52
Recurve 2022-074A 52944						Re-entered - 2024 Aug 2 Life 762 days
6U Cubesat from the US Air Force Research Laboratory (AFRL) intended to test and evaluate radio communications and mesh networking for use in military operations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 3, 05:05	6874	0.0004	493	499	94.54	44.99	268
NACHOS 2 (NanoSat Atmospheric Chemistry Hyperspectral Observation System) 2022-074B 52945						Re-entered - 2024 Jun 27 Life 726 days
3U Cubesat from the US Los Alamos National Laboratory to detect, map, and quantify Earth’s trace gasses in support of volcanology and climate change research.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 3, 05:56	6874	0.0004	493	499	94.53	44.99	255
Slingshot 1 2022-074D 52947						Re-entered - 2024 Sep 11 Life 802 days
12U Cubesat (4x3) testing SatCat5, a data interface that uses Ethernet-type communication between payloads using low power serial communications. Carries an experiment to test precise control of attitude for aiming at targets on Earth, and a GPS receiver.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 3, 05:55	6873	0.0004	492	497	94.50	44.98	228
MISR-B 2022-074F 52949						Re-entered - 2023 Oct 5 Life 460 days
3U or 6U Cubesat from the US Department of Defense to demonstrate communications systems with ground-based sensors and experiments, possibly using Internet links.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 3, 05:56	6874	0.0005	492	499	94.52	44.99	246
CTIM-FD (Compact Total Irradiance Monitor - Flight Demonstration) 2022-074G 52950						Re-entered - 2023 Dec 7 Life 523 days
6U Cubesat from the University of Colorado at Boulder, to test an instrument the Earth's Total Solar Irradiation. One of two satellites flown on the same launch under NASA's ELaNa-39 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 3, 05:56	6874	0.0004	493	498	94.53	45.00	251
Gunsmoke-L 2 & L 3 2022-074H 52951						Re-entered - 2023 Dec 28 Life 544 days
3U Cubesat - pair of conjoined satellites from the US Army's Space and Missile Defense Command to support military operations by providing battlefield imagery from orbit. Design of each is based on Los Alamos National Laboratory's Prometheus 1.5U Cubesat with the Gunsmoke payload occupying a further 1.5U.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 3, 01:13	6874	0.0004	493	499	94.53	44.98	237
GPX-2 2022-074xx 52948						Re-entered - 2024 May 11 Life 679 days
3U Cubesat from NASA Langley Research Center to demonstrate differential GPS to determine satellite position for use in future formation flying in orbit. Equipped with gravity gradient stabilisation boom. One of two satellites flown on the same launch under NASA's ELaNa-39 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 3, 05:56	6871	0.0005	489	497	94.47	44.98	207
LauncherOne upper stage 2022-074C 52946						Re-entered - 2023 Dec 7 Life 523 days
Launched cluster of small satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 3, 05:47	6841	0.0047	430	495	93.85	44.99	214

2022-075 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2022 Jul 7, 09:18
Cosmos 2557 (Uragan-K1 № 16L) 2022-075A 52984						in space
GLONASS-K navigation satellite. It also carries radio receiving equipment for the COSPAS-SARSAT international search and rescue system. Released from launch vehicle around 15:00 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 8, 10:13	25517	0.0003	19130	19148	676.09	64.82	270
2022 Jul 11, 18:07	25537	0.0007	19141	19178	676.89	64.83	359
2022 Jul 21, 15:36	25508	0.0008	19110	19150	675.74	64.81	285
Fregat rocket stage 2022-075B 52985						in space
Launched Cosmos 2557 (GLONASS K) navsat. Orbit raised after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 8, 13:54	25864	0.0107	19208	19764	689.94	64.79	95

2022-076 Falcon 9 Block 5 (Starlink Group 04-21) Cape Canaveral Space Force Station						2022 Jul 7, 13:11
Starlink 4260 2022-076A 52986						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 12, 16:00	6687	0.0031	288	329	90.69	53.22	55
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jul 7 Life <1 day
Launched fifty three Starlink satellites. Directed to re-enter later on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-077 Falcon 9 Block 5 (Starlink Group 03-01) Vandenberg Space Force Base						2022 Jul 11, 01:39
Starlink 4362 2022-077A 53043						in space
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 02:41 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 15, 14:00	6721	0.0002	342	344	91.40	97.66	100
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jul 11 Life <1 day
Launched forty six Starlink satellites. Directed to re-enter on the day of launch, above the mid-Pacific Ocean at about 03:30 UTC.
Not Catalogued - orbit parameters unavailable

2022-078 CZ 3B Xichang Space Centre						2022 Jul 12, 16:30
Tianlian 2-03 2022-078A 53100						in space
Second Generation data communications satellite to provide a data relay, and measurement and control service for Chinese satellites and space stations. Launch completes planned constellation of three second-generation vehicles once satellite is on-station in GEO. Probably moved to Geosynchronous Drift Orbit 2022 Jul 13.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Jul 13, 00:00	24390	0.7305	194	35829	631.78	27.17	175
2022 Jul 24, 22:15	42165	0.0002	35777	35798	1436.12	3.00	190	10°.7 E
CZ 3B fourth stage 2022-078B 53101						Re-entered - 2023 Oct 20 Life 465 days
Launched Tianlian 2-03. Orbit lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 12, 23:57	23780	0.7251	159	34644	608.23	27.12	174

2022-079 Electron (Wise One Looks Ahead, NRO L-162) Rocket Lab Launch Complex, New Zealand						2022 Jul 13, 06:30
USA 334 2022-079A 53102						in space
Satellite built for US National Reconnaissance Office launched as NRO L-162 mission. Precise purpose not known but probably Earth observation. Released from launch vehicle around 07:30 UTC. Launched 90 mins into two hour window with delay due to weather.
Orbit classified as 'Secret' - data withheld
Electron second stage 2022-079B 53103						Re-entered - 2022 Oct 2 Life 81 days
Launched USA 334. Orbit classified as 'Secret' until 2022 September 19.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 19, 09:53	6683	0.0108	233	377	90.62	40.05	88
Electron third stage (kick stage) 2022-079C 53104						in space
Launched USA 334.
Orbit classified as 'Secret' - data withheld

2022-080 Vega-C (VV-21) Centre Spatiale Guyanaise						2022 Jul 13, 13:13
LaReS 2 (Laser Relativity Satellite 2) 2022-080A 53105						in space
Italian Space Agency (ASI) passive satellite with a high density, made of 390 kg of tungsten and being 0.364m in diameter. It has 92 corner cube laser reflectors to be used for extremely accurate measurement of range. Its purpose is to help study aspects of the theory of relativity. Separated from launch vehicle at 14:37 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 15, 02:33	12268	0.0006	5882	5897	225.37	70.14	291
GreenCube 2022-080B 53106						in space
3U Cubesat from the Italian Space Agency and Sapienza University of Rome, carrying an experiment to grow plants in the radiation environment experienced in the Earth's van Allen radiation belts. Released from launch vehicle together with the other Cubesats at ~15:23 UTC. Based on amateur observation, Space-Track has this item incorrectly tagged as 53109/2022-080E.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 16, 04:12	12221	0.0009	5833	5854	224.10	70.15	239
AstroBio 2022-080C 53107						in space
3U Cubesat from the Italian Space Agency working with a group of science institutions, carrying a micro laboratory to provide a platform for an automatic bioanalytical experiments in space. Uses chemiluminescence to identify individual substances. Released from launch vehicle together with the other Cubesats at ~15:23 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 19, 21:57	12227	0.0012	5835	5863	224.26	70.16	252
Trisat-R 2022-080D 53108						in space
3U Cubesat from the University of Maribor Faculty of Electrical Engineering, Slovenia to measure ionizing radiation with the aim of modeling the magnetosphere environment and better understanding space weather. Released from launch vehicle together with the other Cubesats at ~15:23 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 19, 06:59	12227	0.0015	5830	5867	224.25	70.00	251
MTCube 2 (Robusta 1F) 2022-080E 53109						in space
1U Cubesat carrying a payload from the University of Montpellier, France to measure errors induced by radiation into several different types of flash memory. Released from launch vehicle together with the other Cubesats at ~15:23 UTC. Based on amateur observation, Space-Track has this item incorrectly tagged as 53106/2022-080B.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 17, 13:49	12221	0.0009	5832	5854	224.10	70.14	244
Alpha 2022-080F 53110						in space
1U Cubesat from ARCA Dynamics of Italy to study the Earth's magnetosphere. Released from launch vehicle together with the other Cubesats at ~15:23 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 18, 04:46	12222	0.0026	5812	5875	224.11	70.15	149
Celesta 2022-080G 53111						in space
1U Cubesat carrying a payload from the University of Montpellier, France to study short circuits induced by space radiation in electronic circuits. Released from launch vehicle together with the other Cubesats at ~15:23 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 19, 21:51	12222	0.0009	5833	5855	224.11	70.15	223
Vega C upper stage (AVUM+) 2022-080H 53112						in space
Launched LARES 2 and six Cubesats. Navigation warnings issued from CSG indicate planned destructive re-entry above the south western Pacific Ocean around 16:00 UTC on day of launch, but later information from ESA suggested that de-orbit may not have been part of the mission as flown. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 17, 02:36	12221	0.0009	5832	5854	224.09	70.11	258

2022-081 Falcon 9 Block 5 Kennedy Space Center						2022 Jul 15, 00:44
SpaceX Dragon 2 CRS-25 2022-081A 53113						Re-entered - 2022 Aug 20 Life 36 days Returned to Earth
Carrying a cargo to/from the ISS under NASA's Commercial Resupply Services (CRS) contract. Docked with the forward-facing port of the Harmony module of ISS Jul 16 at 16:21 UTC. Undocked Aug 19 at 15:05 UTC. Retro-fire Aug 20 at 18:05 UTC followed separation of the Trunk section, and splashdown in the Atlantic Ocean off Cape Canaveral occurred ~18:53 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 15, 01:07	6579	0.0011	193	208	88.50	51.65	8
2022 Jul 15, 05:05	6616	0.0048	206	269	89.25	51.65	232
2022 Jul 15, 23:22	6618	0.0053	205	275	89.30	51.65	234
2022 Jul 16, 11:34	6792	0.0006	410	418	92.85	51.64	15
2022 Jul 16, 12:56	6795	0.0005	413	420	92.90	51.64	17
2022 Aug 18, 13:01	6794	0.0005	412	420	92.89	51.64	134
2022 Aug 19, 18:41	6784	0.0005	402	409	92.67	51.65	153
2022 Aug 19, 21:40	6665	0.0147	189	385	90.25	51.65	171
2022 Aug 20, 09:33	6666	0.0148	190	386	90.28	51.62	172
2022 Aug 20, 16:44	6666	0.0142	193	382	90.26	51.64	171
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jul 15 Life <1 day
Launched SpaceX Dragon 2 CRS-25. Directed to re-enter later on the day of launch.
Not Catalogued - orbit parameters unavailable
Dragon 2 trunk module 2022-081B 53584						Re-entered - 2022 Aug 31 Life 47 days
Separated from Dragon 2 CRS-25 2022 August 20 prior to retrofire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 21, 15:37	6659	0.0135	192	371	90.14	51.64	175

2022-082 CZ 2C Taiyuan Space Centre						2022 Jul 15, 22:57
Siwei Gaojing 2-01 (Superview Neo 2-01) 2022-082A 53128						in space
One of a simultaneously launched pair of commercial remote sensing satellites from the Siwei Surveying and Mapping Technology Co aimed at producing 3D Earth images using a radar-imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jul 16, 17:42	6870	0.0012	484	500	94.46	97.38	264	06:04
2022 Oct 20, 13:05	6867	0.0012	481	497	94.40	97.39	292	06:05
2022 Oct 23, 16:50	6873	0.0007	490	499	94.50	97.39	314	06:05
2024 Nov 24, 19:56	6870	0.0002	491	493	94.46	97.39	90	06:08
Siwei Gaojing 2-02 (Superview Neo 2-02) 2022-082C 53130						in space
One of a simultaneously launched pair of commercial remote sensing satellites from the Siwei Surveying and Mapping Technology Co aimed at producing 3D Earth images using a radar imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jul 16, 17:42	6868	0.0012	482	498	94.41	97.39	281	06:04
2022 Oct 10, 19:49	6868	0.0011	483	497	94.41	97.39	338	06:05
2022 Oct 11, 02:02	6871	0.0007	489	498	94.47	97.39	350	06:05
2022 Oct 12, 19:06	6873	0.0008	489	500	94.51	97.39	355	06:05
2024 Nov 24, 22:04	6870	0.0002	491	493	94.46	97.39	90	06:08
CZ 2C second stage 2022-082D 53131						Re-entered - 2024 Apr 30 Life 655 days
Launched pair of Siwei Gaojing satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 16, 12:30	6837	0.0049	425	493	93.77	97.36	12

2022-083 Falcon 9 Block 5 (Starlink Group 04-22) Cape Canaveral Space Force Station						2022 Jul 17, 14:20
Starlink 4063 2022-083A 53132						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 14:35 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 21, 18:00	6684	0.0036	282	329	90.63	53.22	52
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Jul 17 Life <1 day
Launched fifty three Starlink satellites. Directed to re-enter later on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-I07 Manual release during EVA International Space Station						2022 Jul 21, 16:02
YuZGU-55 № 8 (Tanyusha 8) 1998-067TR 53306						Re-entered - 2023 Jan 27 Life 190 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 25, 19:19	6794	0.0005	412	419	92.88	51.64	52
Tsiolkovsky-Ryazan № 2 1998-067TS 53307						Re-entered - 2023 Jan 31 Life 194 days
3U Cubesat from Ryazan State Radiotechnical University, carrying radio transmitting equipment to calibrate the sensitivity of radio telescopes of the Pushchino Observatory. Released within a forty minute period during Russian EVA from ISS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 27, 08:52	6793	0.0004	412	418	92.87	51.64	55
YuZGU-55 № 12 (Tanyusha 12) 1998-067TT 53308						Re-entered - 2023 Jan 31 Life 194 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 25, 20:52	6793	0.0004	412	418	92.87	51.64	43
YuZGU-55 № 5 (Tanyusha 5) 1998-067TU 53309						Re-entered - 2023 Jan 31 Life 194 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 25, 19:19	6793	0.0005	412	418	92.87	51.64	61
YuZGU-55 № 9 (Tanyusha 9) 1998-067TV 53310						Re-entered - 2023 Jan 31 Life 194 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 27, 07:30	6793	0.0005	412	418	92.87	51.64	67
Tsiolkovsky-Ryazan № 1 1998-067TW 53311						Re-entered - 2023 Jan 27 Life 190 days
3U Cubesat from Ryazan State Radiotechnical University, carrying radio transmitting equipment to calibrate the sensitivity of radio telescopes of the Pushchino Observatory. Released within forty minutes of the launch time shown, during Russian EVA from ISS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 27, 06:02	6793	0.0004	412	418	92.87	51.64	48
YuZGU-55 № 6 (Tanyusha 6) 1998-067TX 53312						Re-entered - 2023 Jan 31 Life 194 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 25, 19:19	6793	0.0005	411	419	92.87	51.64	58
YuZGU-55 № 7 (Tanyusha 7) 1998-067TY 53313						Re-entered - 2023 Jan 31 Life 194 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 25, 19:18	6793	0.0005	412	418	92.87	51.64	58
YuZGU-55 № 10 (Tanyusha 10) 1998-067TZ 53321						Re-entered - 2023 Jan 31 Life 194 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 27, 08:52	6793	0.0004	412	418	92.87	51.64	65
YuZGU-55 № 11 (Tanyusha 11) 1998-067UA 53322						Re-entered - 2023 Jan 31 Life 194 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students. Acting as demonstrator for an autonomous satellite control system and carrying a number of science sensors. One of ten satellites released during Russian EVA from ISS over a period of about 40 minutes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 25, 20:52	6794	0.0004	413	418	92.88	51.64	49

2022-084 Falcon 9 Block 5 (Starlink Group 03-02) Vandenberg Space Force Base						2022 Jul 22, 17:39
Starlink 4391 2022-084A 53189						in space
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 18:42:03 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 27, 14:00	6710	0.0002	331	333	91.17	97.66	97
Falcon 9 upper stage uncatalogued						in space
Launched forty six Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-085 CZ 5B Wenchang Space Centre						2022 Jul 24, 06:22
Wentian 2022-085A 53239						in space
Module for Chinese Space Station, precise launch time 06:22:32 UTC, released from launch vehicle at 06:30:47 UTC about 5700 km behind CSS. Docked with forward-facing port of Tianhe module of CSS at 19:13 UTC on day of launch. Transferred to side port of docking module 2022 Sep 30 in ~60 min operation completed at 04:44 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6619	0.0089	182	300	89.32	41.45	168
2022 Jul 24, 17:08	6756	0.0008	372	384	92.11	41.46	227
2022 Jul 24, 17:52	6761	0.0007	378	388	92.21	41.47	272
2022 Jul 24, 18:15	6762	0.0007	379	388	92.22	41.47	278
CZ 5 second stage 2022-085B 53240						Re-entered - 2022 Jul 30 Life 6 days
Launched Wentian.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 24, 14:45	6619	0.0089	182	300	89.32	41.45	168
2022 Jul 27, 15:54	6592	0.0064	172	256	88.78	41.48	195
2022 Jul 30, 15:57	6507	0.0016	119	140	87.07	41.47	234

2022-086 Falcon 9 Block 5 (Starlink Group 04-26) Kennedy Space Center						2022 Jul 24, 13:38
Starlink 4056 2022-086A 53242						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 28, 20:00	6682	0.0040	278	331	90.61	53.22	53
Falcon 9 upper stage uncatalogued						in space
Launched fifty three Starlink satellites. Directed to re-enter later on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-087 Lijian 1, Kinetica 1 (Y-1) Jiuquan Space Centre						2022 Jul 27, 04:12
SATech 01 (Space Technology Test Satellite) 2022-087A 53299						Re-entered - 2025 Feb 19 Life 938 days
Satellite from the Institute of Microsatellite Innovation of the Chinese Academy of Sciences, Shanghai. Payload includes SUTRI (Solar Upper Transition Region Imager), a solar imaging camera capable of taking full-disk pictures of solar regions between the solar chromosphere and corona, an x-ray telescope and a gamma-ray astronomy instrument.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Jul 27, 13:40	6881	0.0014	493	512	94.67	97.41	285	10:31
Atmospheric Density Detection Test Satellite 2022-087xx						in space
Spherical satellite for upper atmosphere studies by measuring variations in air drag at orbital altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0013	492	510	94.64	97.40	286	10:31
Electromagnetic Assembly Test Satellite 1 2022-087xx						in space
Small satellite - one of a pair carried on the same launch vehicle. Mission details awaited. May still be attached to its companion satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0013	492	510	94.64	97.40	286	10:31
Electromagnetic Assembly Test Satellite 2 2022-087xx						in space
Small satellite - one of a pair carried on the same launch vehicle. Mission details awaited. May still be attached to its companion satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0013	492	510	94.64	97.40	286	10:31
Jinan 1 2022-087xx						in space
Demonstrator satellite using Quantum Physics to generate security keys for secure communications links between ground and space. Developed jointly by the University of Science and Technology of China, the Jinan Institute of Quantum Technology, the Institute of Microsatellite Innovation of the Chinese Academy of Sciences, and the Shanghai Institute of Technical Physics. Follow-on from QUESS (Micius) - 41731/2016-051A.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0013	492	510	94.64	97.40	286	10:31
Nanyue (Guangdong Science Satellite) 2022-087xx						in space
Small satellite from the South Space Technology Co, carrying remote sensing equipment for Earth studies, in particular soil moisture content and ocean surface winds.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6879	0.0013	492	510	94.64	97.40	286	10:31
Lijian 1 third stage 2022-087F 53304						Re-entered - 2023 Apr 18 Life 265 days
Launched cluster of six satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 28, 07:36	6802	0.0175	305	543	93.05	97.28	309

2022-088 CZ 2D Xichang Space Centre						2022 Jul 29, 13:28
Yaogan 35-03 Follower 1 2022-088A 53316						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 30, 02:01	6872	0.0008	488	499	94.48	35.00	266
2022 Aug 10, 22:43	6873	0.0007	490	500	94.51	35.00	5
2022 Aug 13, 13:19	6875	0.0008	491	502	94.55	35.01	34
2023 Feb 15, 04:54	6871	0.0009	487	500	94.48	35.00	282
Yaogan 35-03 Follower 2 2022-088C 53318						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 30, 02:14	6870	0.0007	488	497	94.46	35.01	266
2022 Aug 8, 17:01	6875	0.0005	494	501	94.56	35.00	323
2023 Feb 15, 04:54	6871	0.0003	491	495	94.48	35.00	272
Yaogan 35-03 Leader 2022-088E 53320						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 30, 02:14	6870	0.0010	485	498	94.44	35.00	287
2022 Aug 10, 04:46	6875	0.0004	494	500	94.55	35.00	326
2023 Feb 15, 04:50	6871	0.0003	491	495	94.48	35.00	262
CZ 2D second stage 2022-088B 53317						Re-entered - 2023 Mar 11 Life 225 days
Launched Yaogan 35 group 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Jul 30, 02:14	6871	0.0009	487	500	94.48	35.00	269

2022-089 Soyuz-2.1v + Volga Plesetsk Cosmodrome						2022 Aug 1, 20:25
Cosmos 2558 2022-089A 53323						in space
Military satellite possibly equipped with sensors that allow it to observe other satellites in orbit. It also may carry an Earth imaging system. Released from Volga rocket stage at 21:49 UTC. Orbit is co-planar with the US imaging reconsat USA 326 (51445/2022-009A) and is raised frequently to overcome decay through air drag and to maintain the LTDN.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 2, 00:53	6822	0.0013	435	452	93.46	97.26	261	12:06
2022 Aug 2, 13:21	6821	0.0010	436	450	93.45	97.25	266	12:06
2022 Sep 8, 10:23	6819	0.0012	432	449	93.40	97.20	133	12:07
2022 Sep 8, 15:03	6822	0.0016	433	455	93.47	97.20	145	12:07
2023 Mar 10, 20:50	6818	0.0007	435	444	93.38	97.19	162	12:06
2023 Mar 13, 14:14	6820	0.0004	439	444	93.42	97.21	136	12:06
2023 Mar 14, 14:10	6826	0.0003	445	450	93.54	97.25	104	12:06
2023 Mar 14, 18:18	6829	0.0007	446	455	93.60	97.26	168	12:06
2023 Mar 15, 16:50	6838	0.0011	452	467	93.78	97.26	243	12:06
2023 Mar 16, 14:38	6842	0.0011	456	471	93.86	97.25	332	12:06
2023 Mar 16, 17:11	6845	0.0011	459	474	93.93	97.29	292	12:06
2023 Apr 24, 17:16	6840	0.0010	455	469	93.84	97.29	164	12:06
2023 Aug 15, 16:23	6840	0.0007	457	467	93.84	97.29	116	12:07
2024 May 20, 17:13	6841	0.0008	457	468	93.84	97.24	162	12:03
2024 Dec 10, 17:24	6843	0.0006	461	469	93.90	97.24	193	11:59
Soyuz upper stage 2022-089B 53324						Re-entered - 2022 Nov 19 Life 110 days
Launched Cosmos 2558.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 2, 00:50	6735	0.0108	284	429	91.67	97.25	70
Volga rocket stage uncatalogued						Re-entered - 2022 Aug 2 Life 1 day
Launched Cosmos 2558. Caused to re-enter above the southern Pacific Ocean on a south-north trajectory Aug 2 at about 08:30 UTC.
Not Catalogued - orbit parameters unavailable

2022-090 CZ 4B Taiyuan Space Centre						2022 Aug 4, 03:08
Jumang (Terrestrial Ecosystem Carbon Monitoring Satellite) 2022-090A 53346						in space
Terrestrial carbon monitoring satellite with a range of instruments to detect and measure such as vegetation biomass, and atmospheric aerosol and chlorophyll fluorescence.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 4, 07:20	6875	0.0009	491	504	94.56	97.47	250	10:25
Head 2G (Jiaotong 4) 2022-090B 53347						Re-entered - 2024 May 30 Life 665 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. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 4, 22:03	6874	0.0012	488	504	94.52	97.47	278
Minhang Junior 2022-090C 53348						Re-entered - 2023 Nov 2 Life 455 days
Small satellite to allow primary and secondary school students to participate in space science research and engineering practice. Carries instruments to monitor carbon sources, and the space environment. Catalogue Number and Designation to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 4, 07:42	6874	0.0010	489	502	94.52	97.47	271
CZ 4B third stage 2022-090D 53349						Re-entered - 2023 Jan 17 Life 166 days
Launched Terrestrial Ecosystem Carbon Monitoring Satellite. Orbit lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 4, 08:55	6770	0.0159	284	499	92.39	97.51	30

2022-091 Electron (Antipodean Adventure, NRO L-199) Rocket Lab Launch Complex, New Zealand						2022 Aug 4, 05:00
USA 335 2022-091A 53352						in space
Satellite built for US National Reconnaissance Office launched as NRO L-199 mission. Precise purpose not known but probably Earth observation. Released from launch vehicle around 06:00 UTC and aimed at orbit around 70° inclination. Launched at the opening of a two hour window. Orbit data based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 20, 22:38	7014	0.0011	628	644	97.43	70.02	329
Electron second stage 2022-091B 53353						Re-entered - 2022 Oct 20 Life 77 days
Launched USA 335. Orbit data based on amateur observation. On launch date, apogee was about 640 km.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 11, 06:11	6796	0.0279	228	607	92.92	70.02	203
Electron third stage (kick stage) 2022-091C 53354						in space
Launched USA 335. Orbit data based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 11, 22:42	7015	0.0005	633	640	97.45	70.00	22

2022-092 Atlas V 421 Cape Canaveral Space Force Station						2022 Aug 4, 10:29
USA 336 (SBIRS GEO 6) 2022-092A 53355						in space
Missile launch detection satellite for the Space-Based Infra Red System with a combination of scanning and staring sensors. A scanning sensor is designed to provide a wide area view in search of missile launches, satellite re-entries and natural terrestrial events, while a staring sensor is designed to observe areas of particular interest with enhanced sensitivity.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Aug 5, 18:00	26652	0.5651	5214	35334	721.71	17.53	178
2022 Aug 11, 15:34	34705	0.2018	21323	35331	1072.36	9.08	178
2022 Aug 15, 15:24	41914	0.0047	35340	35731	1423.29	6.58	358
2022 Aug 16, 08:15	41894	0.0043	35334	35697	1422.28	6.59	354
2022 Aug 17, 15:32	42106	0.0007	35700	35756	1433.10	6.58	166	148°.0 W
2022 Aug 22, 12:38	42128	0.0007	35720	35781	1434.24	6.57	137	144°.9 W
2022 Aug 25, 12:01	42168	0.0002	35781	35798	1436.24	6.57	334	144°.6 W
2023 Jul 26, 14:48	42164	0.0013	35729	35842	1436.04	5.86	176	144°.8 W
Atlas V upper stage (Centaur) 2022-092B 53356						in space
Launched SBIRS GEO 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 5, 04:38	26648	0.5655	5202	35338	721.53	16.48	176

2022-093 CZ 2F/G Jiuquan Space Centre						2022 Aug 4, 16:00
Reusable Spacecraft Test Vehicle Type 1 Flight 2 2022-093A 53357						Re-entered - 2023 May 8 Life 277 days Returned to Earth
Small re-usable spaceplane, possibly associated with China's space station programme and maybe intended for long duration missions. Vehicle used to test launch and landing technology and spacecraft materials. May be the same craft that flew an earlier mission in 2020. Released a companion satellite to conduct rendezvous and capture experiments during 2022 and 2023. Re-entered 2023 May 8 for landing on the runway at Lop Nor at about 00:20 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 4, 20:44	6848	0.0180	346	593	93.99	49.99	149
2022 Aug 24, 01:59	6847	0.0181	346	593	93.98	49.99	229
2022 Aug 24, 11:48	6851	0.0178	351	595	94.07	49.99	229
2022 Sep 11, 13:18	6851	0.0178	351	595	94.06	49.99	303
2022 Oct 23, 06:05	6849	0.0175	351	591	94.02	49.99	116
2022 Oct 24, 11:02	6980	0.0008	597	608	96.73	49.99	261
2023 Jan 12, 19:33	6980	0.0008	597	608	96.73	49.99	215
2023 Apr 13, 07:01	6979	0.0008	596	607	96.71	49.99	202
2023 Apr 14, 06:57	6929	0.0009	545	557	95.67	49.99	273
2023 Apr 14, 19:37	6720	0.0010	335	349	91.37	49.99	273
2023 May 6, 08:53	6721	0.0007	338	347	91.38	49.97	292
(Banxing 4)? 2022-093J 54218						Re-entered - 2023 May 8 Life 277 days Returned to Earth
Speculative name and purpose but possibly used to inspect the main vehicle while on orbit and may also carry a science/technology payload. Satellites with a similar task were deployed from Shenzhou 7 (33386/2008-047A) and Tiangong 2 (41765/2016-057A). Separated from spaceplane October 29 or October 30 and first reported by Space-Track October 31. Initially kept station with it but started to move away November 2 or 3 before conducting co-ordinated manoeuvres with the spaceplane. May have been captured/re-docked with spaceplane December 12 or 13 then separated again Feb 19 or 20. Continued to conduct close manoeuvres with the spaceplane until it 'disappeared' around 2023 March 30, presumably re-captured and stowed aboard the spaceplane prior to its orbit being lowered April 13/14. Re-entered as cargo aboard the main vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 31, 18:39	6981	0.0008	597	608	96.74	49.99	292
2023 Jan 12, 13:06	6980	0.0007	597	607	96.73	49.99	209
2023 Jan 13, 14:52	6979	0.0025	584	619	96.71	50.06	147
2023 Mar 29, 10:03	6979	0.0008	596	607	96.71	49.99	144
unidentified object 2022-093G 53363						Re-entered - 2022 Sep 5 Life 32 days
Noted on day 1 of mission and assumed to be debris. On Aug 8, a minor orbit change indicated it might be an active satellite but the event could have been due to outgassing or shedding of fragments. Rapid orbit decay tends to support it being debris.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 4, 22:10	6847	0.0222	317	621	93.98	50.02	161
2022 Aug 8, 11:50	6841	0.0215	315	610	93.84	50.02	175
2022 Aug 9, 06:35	6837	0.0212	314	604	93.77	50.03	179
2022 Sep 5, 17:24	6692	0.0064	271	357	90.80	50.03	284
unidentified object 2022-093H 53364						in space
Noted on day 1 of mission and assumed to be debris. Low rate of orbit decay indicates it is a dense object so it may be a payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 4, 22:29	6945	0.0110	491	643	96.00	50.03	202
2023 Jan 25, 19:06	6941	0.0108	488	638	95.92	50.03	166
2023 May 7, 15:59	6938	0.0106	486	633	95.85	50.03	207
2024 Jun 9, 02:49	6922	0.0097	476	611	95.51	50.02	345
CZ 2F third stage 2022-093B 53358						Re-entered - 2024 Feb 12 Life 557 days
Launched experimental spaceplane.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 4, 20:44	6847	0.0180	346	593	93.98	49.99	149

2022-094 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Aug 4, 23:08
Danuri (Korea Pathfinder Lunar Orbiter.) 2022-094A 53365						in space
South Korean lunar mission from the Korea Aerospace Research Institute (KARI), scheduled to operate in orbit around the Moon for one year. Equipped with an array of South Korean experiments and one US built instrument. The objectives are to develop indigenous lunar exploration technologies, demonstrate a "space internet", and conduct scientific investigations of the lunar environment, topography, and resources, as well as identify potential landing sites for future missions. Initially injected into Barycentric orbit then entered orbit around the Moon 2002 Dec 16.
In orbit around the Moon or landed on its surface
Falcon 9 upper stage 2022-094B 53366						in space
Launched KPOL.
Earth-Moon Barycentric Orbit

2022-F04 - failed to reach orbit SSLV (SSLV D-1) Satish Dhawan Space Centre						2022 Aug 7, 03:48
EOS 02 (Earth Observation Satellite 2)
Experimental optical remote sensing satellie from India developed in a short space of time to demonstrate rapid launch on demand ability. Aimed at ~350 km orbit with inclination 37°. Lost when VTM satellite orbit stage carried by SSLV failed to ignite, re-entered after about 0.6 orbits.
AzaadiSat
8U Cubesat - carrying 75 individual experiments provided by female students at schools across India under the 'Space Kidz India' initiative. Includes an amateur radio payload. Aimed at ~350 km orbit with inclination 37°. Lost when VTM satellite orbit stage carried by SSLV failed to ignite, re-entered after about 0.6 orbits.

2022-095 Ceres 1 (Gushenxing 1 Y-3) Jiuquan Space Centre						2022 Aug 9, 04:11
Donghai 1 2022-095xx						in space
Small satellite to demonstrate a micro-miniature remote sensing imaging system. Also carries audio files carrying poetry, or other writing, called "Story of Love" to be played on orbit as an art project.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 10, 13:13	6870	0.0079	437	547	94.45	97.41	72	10:29
Taijing-1 01 2022-095xx						in space
Commercial remote sensing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 10, 04:55	6871	0.0081	438	549	94.48	97.41	75	10:29
Taijing-1 02 (Xingshidai 12) 2022-095xx						in space
Commercial remote sensing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 10, 13:13	6871	0.0081	437	548	94.46	97.41	73	10:29
Ceres 1 fourth stage 2022-095D 53387						Re-entered - 2025 Feb 3 Life 909 days
Launched two Taijing 1 satellites, and Donghai 1. Tentative identification. May have been caused to re-enter after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 11:53	6867	0.0086	430	548	94.39	97.41	69

2022-096 Soyuz-2.1b + Fregat Baikonur Cosmodrome						2022 Aug 9, 05:52
Khayyam 2022-096A 53370						in space
Iranian Government owned imaging satellite built and managed by Russia The design is based on Russia's Canopus V. The imaging payload is operated by Iran. Thruster firings to maintain the orbit ceased 2023 December 9 and it entered a period of natural orbit decay until 2024 April 4 when thruster firings began to maintain the orbit at its new height.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 10, 09:07	6871	0.0002	492	495	94.48	97.44	87	23:00
2022 Oct 30, 21:20	6869	0.0002	490	493	94.43	97.43	76	23:02
2023 Dec 9, 01:21	6870	0.0002	490	493	94.45	97.40	69	23:09
2024 Apr 5, 12:15	6864	0.0001	484	487	94.32	97.40	82	23:11
Polytech Universe 1 2022-096B 53371						Re-entered - 2024 Oct 9 Life 792 days
3U Cubesat from Peter the Great Polytechnic University, St Petersburg. Carries a payload to monitor radiation in LEO. One of a pair carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 15:13	6871	0.0003	491	495	94.47	97.44	138
Polytech Universe 2 2022-096C 53372						Re-entered - 2024 Oct 18 Life 801 days
3U Cubesat from Peter the Great Ploytechnic University, St Petersburg. Carries a payload to monitor radiation in LEO. One of a pair carried on the same launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 19:44	6871	0.0002	491	494	94.47	97.44	127
SXC3 2110 Voenmeh (CYCLOPS) 2022-096D 53373						Re-entered - 2024 Mar 6 Life 575 days
3U Cubesat from the Batlic States University, Russia studying the degradation of materials samples and electronics in orbit. Also carries an amateur radio package,
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 08:59	6871	0.0002	491	494	94.46	97.44	128
Monitor 1 2022-096E 53374						Re-entered - 2024 Mar 28 Life 597 days
3U Cubesat from M V Lomonosov Moscow State University, carrying radiation detectors to register dose rates of cosmic radiation, fluxes of high-energy nuclei, and neutron fluxes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 15:12	6870	0.0003	490	494	94.46	97.44	122
SXC3 218 KuzSTU (Kuzbass 300) 2022-096F 53375						Re-entered - 2024 May 18 Life 648 days
3U Cubesat from Kuzbass State Technical University, Russia equipped with an imaging system to monitor fires on the Earth's surface.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 13:38	6870	0.0003	490	494	94.45	97.44	121
UTMN 2022-096G 53376						Re-entered - 2024 May 9 Life 639 days
3U Cubesat from the Tyumen State University, Russia designed and built as a student project. Equipped with an imaging system to study oil spills in the Arctic region.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 14:59	6870	0.0003	490	494	94.46	97.44	127
SXC3 214 MIET-AIS 2022-096H 53377						Re-entered - 2024 Jun 9 Life 670 days
3U Cubesat equipped with an AIS receiver to monitor positions of ships on the ocean surface.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 11:59	6870	0.0003	490	494	94.45	97.44	115
KAI 1 2022-096J 53378						Re-entered - 2024 Aug 18 Life 740 days
3U Cubesat from the Kazan National Research Technical University, Russia equipped with five Earth imaging cameras for remote sensing. Also carries an amateur radio package.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 11, 16:24	6870	0.0003	490	494	94.45	97.44	118
Skoltech B1 2022-096K 53379						Re-entered - 2024 Nov 27 Life 841 days
3U Cubesat from Skolkovo Institute of Science and Technology, Russia. Aimed at developing space comunications systems and studying cosmic radiation and gamma ray bursts.. Also carries an Earth inmaging system. One of a pair of similar satellites carried on the same launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 15:00	6869	0.0006	487	495	94.43	97.44	87
Skoltech B2 2022-096L 53380						Re-entered - 2024 Sep 29 Life 782 days
3U Cubesat from Skolkovo Institute of Science and Technology, Russia. Aimed at developing space comunications systems and studying cosmic radiation and gamma ray bursts.. Also carries an Earth inmaging system. One of a pair of similar satellites carried on the same launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 11, 05:24	6869	0.0006	487	495	94.43	97.44	92
SXC3 219 ISOI 2022-096M 53381						Re-entered - 2024 Jun 5 Life 666 days
3U Cubesat from the Department of Engineering Cybernetics at Samara University, Russia. Equipped with an Earth imaging system for earth resources studies.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 08:58	6869	0.0006	486	495	94.42	97.44	89
SXC3 2111 SibSU (ReshUCube) 2022-096N 53382						Re-entered - 2024 Jul 21 Life 712 days
3U Cubesat from the M S Reshetnev Siberian State University of Science and Technologies equipped to study the Earth's magnetic field and radiation on orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 15:01	6869	0.0006	486	495	94.42	97.44	91
SXC3 218 KuzSTU (CubeSX HSE-2) 2022-096P 53383						Re-entered - 2024 May 9 Life 639 days
3U Cubesat from Kuzbass State Technical University, Russia. Equipped with an Earth imaging system for remote sensing and an amateur radio payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 08:58	6869	0.0006	486	495	94.42	97.44	88
SXC3 217 Siren 2022-096Q 53384						Re-entered - 2024 Jul 6 Life 697 days
3U Cubesat from Belgorod State University, Russia. Carries a payload to study development of plant (lilac) sprouts in microgravity and the space environment.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 13:37	6869	0.0006	486	495	94.42	97.44	90
Geoscan Eidelweiss 2022-096R 53385						Re-entered - 2024 Feb 21 Life 561 days
3U Cubesat equipped with a cold gas thruster for orbital manoeuvres. Also carries an amateur radio payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 10:50	6868	0.0007	485	495	94.41	97.44	89
SXC3 215 Vizard 2022-096T 53386						Re-entered - 2024 Jan 12 Life 521 days
3U Cubesat developed by school students in the Moscow Area. Equipped with an AIS receiver to monitor positions of ships on the ocean surface.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 10, 10:49	6868	0.0008	484	495	94.40	97.44	86
Fregat rocket stage uncatalogued						Re-entered - 2022 Aug 9 Life <1 day
Launched Khayyam and sixteen cubesats. Expected to re-enter the Earth's atmosphere at about 08:00 UTC after retro-fire.
Not Catalogued - orbit parameters unavailable

2022-097 Falcon 9 Block 5 (Starlink Group 04-26) Kennedy Space Center						2022 Aug 10, 02:14
Starlink 4522 2022-097A 53388						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 15, 18:00	6694	0.0019	303	329	90.84	53.22	52
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Aug 10 Life <1 day
Launched fifty three Starlink satellites. Directed to re-enter later on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-098 CZ 6 (Y-10) Taiyuan Space Centre						2022 Aug 10, 04:50
Jilin-1 High Resolution 03D 09 (Jilin-1 GF3D 09) 2022-098A 53444						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 04:35	6918	0.0010	533	547	95.45	97.53	250	11:59
2024 Oct 18, 10:25	6871	0.0007	488	498	94.48	97.53	360	12:18
Jilin-1 High Resolution 03D 35 (Jilin-1 GF3D 35) 2022-098B 53445						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 01:18	6911	0.0016	521	544	95.29	97.53	270	11:59
2024 Oct 18, 10:22	6875	0.0005	493	500	94.55	97.53	26	12:19
Jilin-1 High Resolution 03D 36 (Jilin-1 GF3D 36) 2022-098C 53446						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 04:35	6918	0.0011	532	548	95.44	97.54	252	11:59
2024 Oct 18, 05:36	6875	0.0006	493	501	94.55	97.53	46	12:19
Jilin-1 High Resolution 03D 37 (Jilin-1 GF3D 37) 2022-098D 53447						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 01:33	6918	0.0011	532	547	95.43	97.53	254	11:59
2024 Oct 18, 11:03	6866	0.0008	483	493	94.37	97.53	357	12:17
Jilin-1 High Resolution 03D 38 (Jilin-1 GF3D 38) 2022-098E 53448						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 01:21	6917	0.0011	531	546	95.42	97.53	264	11:59
2024 Oct 18, 10:11	6875	0.0008	492	502	94.56	97.53	51	12:19
Jilin-1 High Resolution 03D 39 (Jilin-1 GF3D 39) 2022-098F 53449						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 04:35	6917	0.0010	532	546	95.41	97.53	262	11:59
2024 Oct 18, 11:07	6874	0.0006	492	500	94.53	97.53	29	12:16
Jilin-1 High Resolution 03D 40 (Jilin-1 GF3D 40) 2022-098G 53450						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 04:34	6916	0.0007	533	543	95.40	97.53	264	11:59
2024 Oct 18, 11:32	6872	0.0005	490	497	94.48	97.53	57	12:19
Jilin-1 High Resolution 03D 41 (Jilin-1 GF3D 41) 2022-098H 53451						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 04:34	6916	0.0008	532	543	95.39	97.54	267	11:59
2024 Oct 18, 11:12	6865	0.0004	484	490	94.34	97.54	37	12:23
Jilin-1 High Resolution 03D 42 (Jilin-1 GF3D 42) 2022-098J 53452						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 04:35	6916	0.0009	532	543	95.39	97.53	273	11:59
2024 Oct 18, 11:28	6873	0.0005	491	498	94.51	97.53	50	12:17
Jilin-1 High Resolution 03D 43 (Jilin-1 GF3D 43) 2022-098K 53453						in space
High resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 10, 22:05	6915	0.0009	531	543	95.38	97.53	282	11:59
2024 Oct 18, 10:09	6874	0.0005	492	499	94.52	97.53	53	12:19
Yunyao-1 04 2022-098L 53454						Re-entered - 2024 Aug 10 Life 731 days
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 04:34	6915	0.0011	529	544	95.37	97.53	287	11:59
2024 Aug 10, 01:42	6520	0.0016	132	153	87.33	97.50	261	13:16
Yunyao-1 05 2022-098M 53455						Re-entered - 2024 Sep 2 Life 754 days
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 06:09	6915	0.0008	531	542	95.37	97.53	228	11:59
2024 Sep 2, 18:47	6524	0.0015	136	156	87.40	97.50	255	13:19
Yunyao-1 06 2022-098N 53456						Re-entered - 2024 Aug 23 Life 744 days
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 05:53	6915	0.0010	530	543	95.37	97.53	276	11:59
2024 Aug 23, 05:02	6528	0.0015	140	160	87.48	97.50	270	13:15
Yunyao-1 07 2022-098P 53457						Re-entered - 2024 Sep 5 Life 757 days
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 06:08	6914	0.0014	526	545	95.36	97.53	295	11:59
2024 Sep 5, 02:28	6564	0.0015	176	195	88.20	97.48	277	13:19
Yunyao-1 08 2022-098Q 53458						Re-entered - 2024 Aug 31 Life 752 days
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 05:45	6914	0.0009	530	543	95.36	97.53	275	11:59
2024 Aug 28, 02:04	6637	0.0012	251	267	89.69	97.51	267	13:16
Yunyao-1 09? (Tianjin Binhai-1) 2022-098R 53459						Re-entered - 2024 Sep 3 Life 755 days
Small satellite from the China's Tianjin Yunyao Aerospace Technology Co with a meteorological payload that includes an infrared Earth imaging system and an atmosphere studies sensor using occultation of navsat signals to study the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 11, 05:45	6914	0.0011	528	544	95.36	97.53	294	11:59
2024 Sep 1, 22:56	6582	0.0014	194	213	88.57	97.50	277	13:18
CZ 6 third stage uncatalogued						in space
Launched cluster of sixteen Jilin-1 and Yunyao-1 satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-I08 JEM Small Satellite Orbital Deployer International Space Station						2022 Aug 12, 09:45
FUTABA 1998-067UC 53463						Re-entered - 2023 Feb 16 Life 188 days
1U Cubesat from the Kyushu Institute of Technology, Japan to study the effect of 'whiskers' in lead-free solder on the performance of satellite electronics. Also carries an amateur radio payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 12, 19:30	6792	0.0009	408	420	92.85	51.65	139
HSU-Sat 1 1998-067UC 53462						Re-entered - 2023 Mar 11 Life 211 days
1U Cubesat from the Happy Science University, Japan testing satellite components and technologies including infrared-based communication for an uplink. Also carries an amateur radio payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 13, 12:27	6792	0.0007	409	419	92.85	51.64	133
TUMnanoSAT 1998-067UD 53464						Re-entered - 2023 Jan 31 Life 172 days
1U Cubesat from the Technical University of Moldova designed to test structural elements and electronic systems for use in satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 13, 12:27	6792	0.0007	409	419	92.84	51.64	137

2022-099 Falcon 9 Block 5 (Starlink Group 03-03) Vandenberg Space Force Base						2022 Aug 12, 21:40
Starlink 4415 2022-099A 53465						in space
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 22:43 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 19, 14:00	6726	0.0002	346	349	91.49	97.66	119
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Aug 12 Life <1 day
Launched forty six Starlink satellites. Re-entered over the southern Pacific Ocean at about 23:45 UTC following retro-fire.
Not Catalogued - orbit parameters unavailable

2022-100 CZ 2D Xichang Space Centre						2022 Aug 19, 17:37
Yaogan 35-04 Follower 1 2022-100A 53522						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 20, 07:28	6875	0.0008	491	502	94.54	35.00	267
2023 Feb 15, 09:16	6872	0.0005	490	498	94.49	35.00	93
Yaogan 35-04 Leader 2022-100C 53524						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 20, 07:49	6872	0.0009	488	500	94.49	35.00	290
2023 Feb 15, 13:54	6872	0.0006	490	498	94.49	35.00	69
Yaogan 35-04 Follower 2 2022-100E 53526						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 20, 02:35	6873	0.0009	489	501	94.52	35.00	272
2023 Feb 14, 17:31	6872	0.0008	489	500	94.49	35.00	145
CZ 2D second stage 2022-100B 53523						Re-entered - 2023 Mar 29 Life 222 days
Launched Yaogan 35 group 4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 20, 07:30	6874	0.0009	490	502	94.53	35.00	274

2022-101 Falcon 9 Block 5 (Starlink Group 04-27) Cape Canaveral Space Force Station						2022 Aug 19, 19:21
Starlink 4511 2022-101A 53527						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from launch vehicle at 19:36 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 24, 14:00	6682	0.0040	277	330	90.59	53.22	56
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Aug 19 Life <1 day
Launched fifty three Starlink satellites. Caused to re-enter later on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-102 Kuaizhou 1A Xichang Space Centre						2022 Aug 23, 02:36
Chuangxin 16A (Innovation 16A, Shiyan?) 2022-102A 53586						in space
One of a pair of small satellites described as "mainly used in scientific experiments, new technology verification and other fields" and initially as a "double satellite assembly". Chuanxin 16B separated from it Sep 19. Orbit plane matches that of the GECAM gravity wave detection satellites launched 2021 June.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Aug 23, 10:32	6971	0.0005	590	596	96.54	29.01	261
2022 Sep 19, 12:36	6971	0.0005	589	596	96.53	29.00	171
Chuangxin 16B (Innovation 16B, Shiyan?) 2022-102B 53876						in space
One of a pair of small satellites described as "mainly used in scientific experiments, new technology verification and other fields". Separated from Chuangxin 16A Sep 19. Orbit plane matches that of the GECAM gravity wave detection satellites launched 2021 June.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 20, 12:41	6971	0.0005	589	596	96.53	29.00	183
Kuaizhou 1A third stage uncatalogued						in space
Launched Chuangxin 16. Caused to re-enter after releasing payload. First launch of Kuaizhou 1A from Xichang.
Not Catalogued - orbit parameters unavailable

2022-103 CZ 2D Taiyuan Space Centre						2022 Aug 24, 03:01
Beijing 3B (Nanning 1) 2021-103A 53587						in space
Commercial Earth imaging satellite from China's 21st Century Space Technology Application Company. Larger and an updated design compared with Beijing 3A, and capable of providing 3D images.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Aug 24, 06:06	6984	0.0013	597	615	96.81	97.94	264	10:09
2022 Sep 7, 02:17	6984	0.0014	596	616	96.81	97.94	214	10:10
2022 Sep 7, 12:32	6985	0.0013	597	616	96.82	97.94	211	10:10
CZ 2D second stage uncatalogued						in space
Launched Beijing 3B. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable

2022-104 Falcon 9 Block 5 (Starlink Group 04-23) Cape Canaveral Space Force Station						2022 Aug 28, 03:41
Starlink 4691 2022-104A 53588						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from the launch vehicle at 03:56 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 2, 14:00	6685	0.0034	284	330	90.66	53.22	58
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Aug 28 Life <1 day
Launched fifty three Starlink satellites. Directed to re-enter at about 05:00 UTC on the day of launch.
Not Catalogued - orbit parameters unavailable

2022-105 Falcon 9 Block 5 (Starlink Group 03-04) Vandenberg Space Force Base						2022 Aug 31, 05:40
Starlink 4622 2022-105A 53648						in space
One member of a simultaneously-launched cluster of forty six LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 06:43 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
Orbit parameters awaited
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Aug 31 Life <1 day
Launched forty six Starlink satellites. Re-entered over the Indian Ocean at about 06:00 UTC following retro-fire.
Not Catalogued - orbit parameters unavailable

2022-106 CZ 4C Jiuquan Space Centre						2022 Sep 2, 23:44
Yaogan 33-02 2022-106A 53698						in space
Described as being used for remote sensing for natural resources surveys. Specific tasks include land survey, crop yield assessment, and input to disaster monitoring and prevention plans. Equipped with synthetic aperture radar for Earth imaging provided by the Institute of Space and Space Information Innovation of the Chinese Academy of Sciences. Mission is probably military or government.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Sep 3, 06:04	7062	0.0006	680	688	98.44	98.18	245	06:00
2022 Sep 16, 04:39	7066	0.0010	681	695	98.52	98.19	177	06:00
2022 Sep 16, 17:10	7066	0.0010	681	695	98.52	98.19	175	06:00
2022 Sep 17, 05:03	7073	0.0002	694	697	98.67	98.19	171	06:00
2022 Sep 19, 02:45	7074	0.0001	696	696	98.69	98.19	104	06:00
2023 Feb 13, 06:31	7074	0.0002	695	697	98.68	98.19	111	06:00
CZ 2C second stage 2022-106B 53699						in space
Launched Yaogan 33-02. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 3, 07:20	6972	0.0144	493	694	96.55	98.20	51

2022-107 Falcon 9 Block 5 (Starlink Group 04-20) Cape Canaveral Space Force Station						2022 Sep 5, 02:09
Starlink 4725 2022-107A 53700						in space
One member of a simultaneously-launched cluster of fifty one LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 03:22 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 12, 14:00	6711	0.0001	332	333	91.18	53.22	96
Sherpa LTC-2 2022-107BG 53754						in space
Space tug with Hosted Payload Varuna-TDM (Technology Demonstration Mission) - from Boeing, designed to test radio communications at V-band (40 - 75 GHz). A problem with Sherpa's systems prevented its orbit being raised immediately to the target 1000 km but control was restored early-October and orbit raising began. Separated from launch vehicle at 02:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 11, 13:41	6685	0.0010	300	314	90.66	53.21	296
2022 Oct 7, 09:03	6664	0.0009	280	292	90.24	53.21	3
2022 Oct 7, 21:04	6684	0.0034	283	328	90.64	53.21	65
2022 Oct 12, 20:28	6712	0.0015	324	343	91.20	53.22	260
2022 Nov 4, 16:12	6700	0.0014	312	331	90.96	53.21	353
2022 Nov 11, 08:45	6696	0.0013	309	326	90.88	53.21	18
2022 Nov 16, 19:57	6793	0.0131	326	504	92.87	53.22	229
2022 Nov 22, 23:08	7076	0.0522	328	1067	98.73	53.23	244
2022 Nov 23, 14:19	7108	0.0477	391	1069	99.40	53.25	246
Falcon 9 upper stage uncatalogued						in space
Launched fifty one Starlink satellites and Sherpa LTC. Caused to re-enter above the Indian Ocean at about 04:15 UTC after releasing the satellites.
Not Catalogued - orbit parameters unavailable

2022-108 Kuaizhou 1A Jiuquan Space Centre						2022 Sep 6, 02:24
Wei Li Kongjiang 01-03 (Centispace 01-03) 2022-108A 53757						in space
Demonstrator for an LEO navigation enhancement system being developed by Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Will also be used to test the Beidou system and to test an inter-satellite laser communication system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 6, 07:11	7077	0.0008	693	705	98.75	53.53	279
Wei Li Kongjiang 01-04 (Centispace 01-04) 2022-108B 53758						in space
Demonstrator for an LEO navigation enhancement system being developed by Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Will also be used to test the Beidou system and to test an inter-satellite laser communication system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 6, 07:11	7079	0.0008	695	707	98.79	53.53	261
Kuazhou 1A upper stage 2022-108C 53759						Re-entered - 2022 Nov 5 Life 60 days
Launched Centispace S3 & S4. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 6, 07:09	6860	0.0413	199	766	94.25	53.56	80

2022-109 CZ 2D Xichang Space Centre						2022 Sep 6, 04:19
Yaogan 35-05 Follower 2 2022-109A 53760						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 6, 17:02	6875	0.0008	491	502	94.55	35.00	265
2023 Feb 15, 13:03	6872	0.0007	489	498	94.48	35.00	272
Yaogan 35-05 Leader 2022-109B 53761						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 6, 12:08	6873	0.0008	489	500	94.51	34.99	281
2022 Sep 7, 00:58	6873	0.0009	489	501	94.51	35.00	287
2022 Sep 15, 06:39	6874	0.0006	492	501	94.54	35.00	355
2023 Feb 15, 09:50	6872	0.0004	491	496	94.49	34.99	303
Yaogan 35-05 Follower 1 2022-109D 53763						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 6, 12:00	6874	0.0007	491	501	94.53	35.00	264
2022 Sep 10, 08:51	6875	0.0006	493	501	94.55	34.99	309
2023 Feb 15, 09:54	6872	0.0006	490	498	94.49	35.00	291
CZ 2D second stage 2022-109E 53764						Re-entered - 2023 Mar 28 Life 203 days
Launched Yaogan 35 group 5.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 6, 12:08	6874	0.0009	490	502	94.54	34.99	263

2022-I09 Nanoracks Cubesat Deployer International Space Station						2022 Sep 6, 09:10
CapSat 1 (Capacitor Satellite) 1998-067UH 53770						Re-entered - 2023 Jan 31 Life 147 days
1U Cubesat - demonstrator from the Weiss School, Florida to evaluate use of a capacitor-based power system. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 9, 23:06	6792	0.0003	411	416	92.83	51.64	286
JagSat 1998-067UJ 53771						Re-entered - 2023 Jan 22 Life 138 days
2U Cubesat - from the University of South Alabama, equipped to measure plasma electron density in LEO. Results will allow studies of the topside F region of the Earth's ionosphere. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 9, 23:06	6791	0.0003	411	416	92.83	51.64	288
D3 1998-067UK 53772						Re-entered - 2023 Feb 28 Life 175 days
2U Cubesat - from the University of Florida, equipped with an atmospheric drag device that can be re-configured to control the rate of orbital decay. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative. Note - Space-Track has this catalogued as a debris item.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 11, 06:04	6793	0.0002	413	417	92.87	51.64	221

2022-I10 Nanoracks Cubesat Deployer International Space Station						2022 Sep 6, 09:20
BeaverCube 1998-067UF 53768						Re-entered - 2023 Apr 12 Life 218 days
3U Cubesat - from the Massachussetts Institute of Technology, to take temperature measurements of the Earth's sea surface and cloud tops. It also carries a low-power electric thruster that will be used to change the orbit height by about 500 metres. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 9, 23:06	6792	0.0001	413	415	92.85	51.64	311
CLICK A (CubeSat Laser Infrared Crosslink) 1998-067UG 53769						Re-entered - 2023 Apr 1 Life 207 days
3U Cubesat - demonstrator mission from the Massachusetts Institute of Technology, University of Florida and NASA Ames Research Center. It will test laser communications equipment for a later pair of CLICK satellites. Launched under NASA's ELaNa-45 (Educational Launch of Nanosatellites) initiative.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 9, 23:06	6792	0.0001	413	415	92.84	51.64	309

2022-110 Ariane 5ECA (VA-258) Centre Spatiale Guyanaise						2022 Sep 7, 21:45
Eutelsat Konnect VHTS (Very High Throughput Satellite) 2022-110A 53765						in space
Comsat to provide high-speed Internet access across Europe, especially to isolated regions with poor terrestrial coverage. Separated from launch vehicle at 22:13 UTC. Orbit raising from transfer orbit used continuously operating thruster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Sep 8, 20:12	36742	0.8180	308	60418	1168.14	3.37	175
2022 Sep 15, 14:30	37704	0.8077	871	61781	1214.35	3.41	178
2022 Sep 22, 02:50	38585	0.7917	1661	62753	1257.15	3.19	179
2022 Sep 29, 09:53	40215	0.7741	2707	64966	1337.63	2.79	182
2022 Oct 6, 16:48	41810	0.7502	4068	66796	1418.03	2.48	183
2022 Oct 17, 00:00	42837	0.7019	6393	66526	1470.59	2.14	187
2022 Oct 20, 14:34	43052	0.6854	7168	66181	1481.69	1.95	185
2022 Oct 26, 16:59	43432	0.6541	8645	65462	1501.30	1.83	188
2022 Nov 4, 14:31	42914	0.6243	9744	63329	1474.57	1.50	186
2022 Nov 11, 21:36	43777	0.5681	12528	62271	1519.27	1.31	186
2022 Nov 17, 18:24	44277	0.5343	14243	61554	1545.34	1.16	187
2022 Nov 23, 16:16	43894	0.4947	15803	59229	1525.33	1.03	187
2022 Dec 1, 16:00	43831	0.4391	18207	56698	1522.04	0.92	193
2022 Dec 8, 12:51	43833	0.3954	20124	54787	1522.18	0.75	186
2022 Dec 15, 14:59	43734	0.3516	21978	52734	1517.03	0.66	186
2022 Dec 21, 16:43	43678	0.3324	22779	51821	1514.10	0.57	182
2022 Dec 28, 22:00	43400	0.2507	26142	47901	1499.64	0.46	186
2023 Jan 4, 12:00	43060	0.2035	27918	45446	1482.09	0.40	182
2023 Jan 13, 17:18	42774	0.1361	30573	42218	1467.31	0.30	179
2023 Jan 18, 12:34	42502	0.1347	30397	41850	1453.34	0.25	176
2023 Jan 25, 13:03	42476	0.0599	33554	38641	1452.03	0.18	151
2023 Jan 29, 22:33	42369	0.0292	34752	37229	1446.52	0.17	133
2023 Feb 2, 06:52	42261	0.0047	35686	36080	1441.03	0.17	123
2023 Feb 7, 09:05	42166	0.0003	35775	35800	1436.16	0.15	44	2°.7 E
2023 Jul 25, 06:40	42165	0.0003	35774	35799	1436.11	0.05	28	2°.7 E
Ariane 5 upper stage 2022-110B 53766						in space
Launched Eutelsat Konnect VHTS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 10, 07:27	36143	0.8160	274	59256	1139.71	3.14	170

2022-111 Falcon 9 Block 5 (Starlink Group 04-02) Kennedy Space Center						2022 Sep 11, 01:20
Starlink 4718 2022-111A 53773						in space
One member of a simultaneously-launched cluster of thirty four LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 02:09 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 19, 22:00	6728	0.0001	349	351	91.53	53.21	108
BlueWalker 3 2022-111AL 53807						in space
Demonstrator satellite for a potential constellation of comsats to provide direct connection to hand held mobile phones. Its Launch Vehicle Adapter separated from Falcon 9 at 03:23 UTC after the rocket raised its orbit above the Starlink release height. Until about Nov 11 the satellite was contained within the Adapter at which time it was released into independent orbit. On Nov 14, satellite owner AST SpaceMobile announced it had unfolded its 64 square metre arial array.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 14, 18:05	6888	0.0014	500	520	94.83	53.20	117
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Sep 11 Life <1 day
Launched Bluewalker 3 and thirty four Starlink satellites. Caused to re-enter with surviving fragments hitting the south western Pacific Ocean north of New Zealand at about 04:15 UTC, 1.3 circuits after lift-off.
Not Catalogued - orbit parameters unavailable

2022-112 CZ 7A (Y-4) Wenchang Space Centre						2022 Sep 13, 13:18
Zhongxing 1E (Chinasat 1E) 2022-112A 53813						in space
Communications satellite described as carrying high-quality voice, data and radio and TV transmissions. Probably for government/military services. Moved to geosynchronous drift orbit late on September 14.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Sep 13, 22:47	24369	0.7302	197	35785	630.99	13.93	174
2022 Sep 20, 23:33	42158	0.0001	35775	35785	1435.77	1.51	231	81°.4 E
2022 Sep 23, 13:29	42165	0.0003	35776	35797	1436.09	1.50	252	81°.4 E
CZ 7 third stage 2022-112B 53814						Re-entered - 2022 Oct 13 Life 30 days
Launched Zhongxing 1E. Perigee lowered after releasing satellite causing it not to be acknowledged by Space-Track for ten days.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 23, 06:00	21953	0.7044	111	31038	539.51	13.93	181

2022-113 Electron (The Owl Spreads Its Wings) Rocket Lab Launch Complex, New Zealand						2022 Sep 15, 20:38
StriX 1 2022-113A 53815						in space
Imaging satellite equipped with a synthetic aperture radar - produced by the University of Tokyo, the Tokyo Institute of Technology, Keio University, Japan Space Systems, and a private company - Synspective Inc of Tokyo. Will become part of a constellation of 25-30 satellites to monitor ground movement and ground changes in urban areas. The name derives from the scientific name for the owl and its sensitivity to low levels of light. Released from launch vehicle at 21:32 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Sep 16, 21:19	6944	0.0013	557	575	95.99	97.66	294	09:00
Electron second stage 2022-113B 53816						Re-entered - 2022 Sep 28 Life 13 days
Launched Strix 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 16, 05:00	6761	0.0300	180	586	92.21	97.66	224
Electron third stage (kick stage) 2022-113C 53817						in space
Launched Strix 1. Did not perform usual perigee-lowering manoeuvre after satellite release.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 16, 18:07	6944	0.0013	557	575	95.99	97.66	296

2022-114 Falcon 9 Block 5 (Starlink Group 04-34) Cape Canaveral Space Force Station						2022 Sep 19, 00:18
Starlink 4749 2022-114A 53818						Re-entered - 2025 Mar 8 Life 901 days
One member of a simultaneously-launched cluster of fifty four LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. All satellites expected to be injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 23, 16:00	6687	0.0031	288	330	90.70	53.22	55
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Sep 19 Life <1 day
Launched fifty four Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-115 CZ 2D Jiuquan Space Centre						2022 Sep 20, 23:15
Yunhai-1 03 2022-115A 53877						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. Replaces Yunhai 1-01.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Sep 22, 08:44	7143	0.0014	756	775	100.14	98.50	256	05:31
2022 Sep 25, 11:46	7148	0.0010	763	777	100.24	98.50	272	05:31
2022 Sep 26, 05:42	7156	0.0004	775	780	100.41	98.49	2	05:31
2022 Sep 26, 07:19	7160	0.0002	781	784	100.50	98.48	60	05:31
CZ 2D second stage 2022-115B 53878						in space
Launched Yunhai 1-03. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 21, 02:23	7046	0.0125	580	756	98.10	98.55	43

2022-116 Soyuz-2.1a Baikonur Cosmodrome						2022 Sep 21, 13:54
Soyuz MS-22 (Soyuz 11F732A48 № 751, Konstantin Tsiolkovsky) 2022-116A 53879						Re-entered - 2023 Mar 28 Life 188 days Returned to Earth
Carried crew to ISS - Sergey Prokovyev (commander) and Dmitri Petelin (both Roscosmos) and Frank Rubio (NASA). Separated from launch vehicle at 14:03 UTC. Docked with the Rassvet module at 17:06 UTC. Suffered loss of pressure in its cooling system 2022 December leading to a decision to return it to Earth without a crew. It was replaced at ISS by Soyuz MS-23, launched without crew. Soyuz MS-22 undocked 2023 March 28 at 09:57:27 UTC. Retrofire at 10:51 UTC led to landing 147 km south east of Dzhezkazgan at 11:45:58 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 21, 14:26	6590	0.0012	204	220	88.74	51.63	97
2022 Sep 21, 17:00	6794	0.0002	415	418	92.89	51.64	282
2023 Mar 27, 13:27	6796	0.0006	414	422	92.93	51.64	137
Soyuz third stage 2022-116B 53880						Re-entered - 2022 Sep 24 Life 3 days
Launched Soyuz MS-22.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 21, 14:22	6577	0.0021	185	213	88.47	51.65	29

2022-117 Delta 4 Heavy Vandenberg Space Force Base						2022 Sep 24, 22:25
USA 338 (KH-11 Block-5 F-3/Crystal?) 2022-117A 53883						in space
KH-11 reconnaissance satellite. Orbital elements not released by Spacetrack so parameters are based on work by amateur observers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 26, 11:54	6766	0.0008	382	393	92.30	73.57	25
2022 Sep 28, 15:48	6784	0.0012	398	414	92.69	73.58	5
Delta 4 upper stage uncatalogued						Re-entered - 2022 Sep 24 Life <1 day
Launched USA 338. Caused to re-enter above the eastern Pacific Ocean Sep 25 around 00:00 UTC
Not Catalogued - orbit parameters unavailable

2022-118 Kuaizhou 1A Taiyuan Space Centre						2022 Sep 24, 22:55
Shiyan 14 (Test 14) 2022-118A 53884						in space
Purpose unknown - described as "mainly used to conduct scientific experiments and verify new technologies". Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Sep 25, 03:23	6876	0.0013	488	506	94.56	97.52	260	06:02
Shiyan 15 (Test 15) 2022-118B 53885						Re-entered - 2024 Nov 26 Life 794 days
Purpose unknown but probably an imaging satellite - described as being to "provide data in the fields of land survey, urban planning, and disaster prevention and mitigation". Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Sep 25, 03:23	6874	0.0010	488	503	94.52	97.52	269	06:02
Kuaizhou 1A third stage 2022-118C 53942						Re-entered - 2023 Nov 6 Life 408 days
Launched Shiyan 14 and Shiyan 15. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 25, 03:21	6866	0.0277	298	678	94.37	97.52	5

2022-119 Falcon 9 Block 5 (Starlink Group 04-35) Cape Canaveral Space Force Station						2022 Sep 24, 23:32
Starlink 5028 2022-119A 53886						in space
One member of a simultaneously-launched cluster of fifty two LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. All satellites expected to be injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 30, 12:00	6682	0.0034	281	327	90.60	53.22	63
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Sep 25 Life 1 day
Launched fifty three Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-120 CZ 2D Xichang Space Centre						2022 Sep 26, 13:38
Yaogan 36-01 Follower 2 2022-120A 53943						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-01 (launch 2021-101) satellites so may represent an enhancement of the constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 26, 21:27	6871	0.0009	486	498	94.46	34.99	268
2022 Oct 6, 18:50	6871	0.0009	486	499	94.47	35.00	11
2022 Nov 12, 06:53	6875	0.0004	495	500	94.56	35.00	332
2023 Feb 15, 09:31	6871	0.0004	490	496	94.48	35.00	167
2023 Aug 31, 05:27	6871	0.0002	492	494	94.48	34.99	145
Yaogan 36-01 Follower 1 2022-120D 53946						Re-entered - 2024 Jun 28 Life 641 days
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-01 (launch 2021-101) satellites so may represent an enhancement of the constellation. 2023 March, this satellite ceased to manoeuvre and fell out of the operating formation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 27, 05:32	6871	0.0008	488	499	94.48	35.00	270
2022 Oct 6, 18:51	6871	0.0008	487	498	94.46	35.00	349
2022 Nov 12, 04:38	6875	0.0008	491	503	94.55	35.00	319
2023 Feb 15, 09:32	6871	0.0004	490	496	94.48	35.00	142
2023 Aug 31, 01:39	6843	0.0004	462	467	93.89	34.99	129
Yaogan 36-01 Leader 2022-120E 53947						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-01 (launch 2021-101) satellites so may represent an enhancement of the constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 26, 21:26	6870	0.0010	485	498	94.44	35.00	288
2022 Oct 7, 06:01	6871	0.0007	488	497	94.46	35.00	22
2022 Nov 12, 06:49	6875	0.0006	493	501	94.55	35.00	45
2023 Feb 15, 09:27	6872	0.0008	488	499	94.48	35.00	190
2023 Aug 31, 05:23	6871	0.0004	491	496	94.47	34.99	233
CZ 2D second stage 2022-120C 53945						Re-entered - 2023 May 13 Life 229 days
Launched Yaogan 36 Group 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Sep 27, 05:31	6871	0.0010	486	500	94.47	35.00	273

2022-121 CZ 6 (Y-9) Taiyuan Space Centre						2022 Sep 26, 23:50
Shiyan 16A (Test 16A) 2022-121A 53948						Re-entered - 2025 Mar 8 Life 894 days
Purpose unknown but probably an imaging satellite - described as to be "used in the fields of land survey, urban planning, and disaster prevention and mitigation". Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Sep 27, 02:52	6891	0.0011	505	521	94.88	97.45	270	06:59
Shiyan 16B (Test 16B) 2022-121B 53949						Re-entered - 2024 Oct 22 Life 757 days
Purpose unknown but probably an imaging satellite - described as to be "used in the fields of land survey, urban planning, and disaster prevention and mitigation". Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Sep 27, 02:52	6890	0.0010	505	519	94.87	97.45	272	06:59
Shiyan 17 (Test 17) 2022-121C 53950						in space
Purpose unknown but probably an imaging satellite - described as to be "used in the fields of land survey, urban planning, and disaster prevention and mitigation". Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Sep 27, 02:51	6890	0.0012	503	520	94.85	97.46	284	06:59
CZ 6 third stage uncatalogued						in space
Launched Shiyan 16A & B and Shiyan 17. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-122 Firefly Alpha (FLTA002) Vandenberg Space Force Base						2022 Oct 1, 07:01
Serenity 2022-122A 53955						Re-entered - 2022 Oct 6 Life 5 days
3U Cubesat from Teachers In Space to collect atmospheric pressure, temperature, and radiation data and make it available for to schools and colleges for educational use. Amateur Radio users reported possible signal reception until at least Oct 4. Re-entry date is an estimate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 1, 12:39	6627	0.0045	219	279	89.49	136.89	164
Picobus 2022-122xx						Re-entered - 2022 Oct 3 Life 2 days
PockeQube deployer carrying five PocketQube satellites that were expected to be released into orbit soon after Picobus separated from the Firefly upper stage: Qubik-3 Qubik-4 FOSSASat-1B Genesis G (Astroland 1) Genesis J (Astroland 2) Re-entry date is an estimate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6626	0.0044	219	278	89.47	136.90	168
FossaSat-1B 2022-122xx						Re-entered - 2022 Oct 3 Life 2 days
1p PocketQube developed by Spain's Fossa Systems - demonstrator of communications satellite that uses low power radio transmission to provide internet connectivity. Amateur Radio users reported reception of signals up to re-entry Oct 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6626	0.0044	219	278	89.47	136.90	168
Genesis G (Astroland 1) 2022-122xx						Re-entered - 2022 Oct 3 Life 2 days
2p PocketQube from AMSAT-EA carrying an amateur radio payload. Amateur Radio users reported possible signal reception up to re-entry on Oct 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6626	0.0044	219	278	89.47	136.90	168
Genesis J (Astroland 2) 2022-122xx						Re-entered - 2022 Oct 3 Life 2 days
2p PocketQube from AMSAT-EA carrying an amateur radio payload. Amateur Radio users reported possible signal reception up to re-entry on Oct 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6626	0.0044	219	278	89.47	136.90	168
Qubik 3 2022-122xx						Re-entered - 2022 Oct 3 Life 2 days
1p PocketQube from Libre Space Foundation, part of an experiment designed to support identification of individual satellites early in their life and to generate accurate orbital elements from radio tracking. Amateur Radio users reported signal reception up to re-entry in the early hours of Oct 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6626	0.0044	219	278	89.47	136.90	168
Qubik 4 2022-122xx						Re-entered - 2022 Oct 3 Life 2 days
1p PocketQube from Libre Space Foundation, part of an experiment designed to support identification of individual satellites early in their life and to generate accurate orbital elements from radio tracking. Amateur Radio users reported signal reception up to re-entry in the early hours of Oct 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6626	0.0044	219	278	89.47	136.90	168
TechEdSat 15 2022-122xx						Re-entered - 2022 Oct 2 Life 1 day
3U Cubesat from NASA Ames equipped with a moveable drag sail to test control of orbit decay through varying its orientation. Unexpectedly low orbit prevented testing of the sail. Also carried a small quantity of space experiments. Re-entry date is an estimate.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6626	0.0044	219	278	89.47	136.90	168
Firefly Alpha upper stage 2022-122E 53959						Re-entered - 2022 Oct 7 Life 6 days
Launched 3 satellites. Carried Firefly Capsule containing postcards, a book and artwork provided by Teachers In Space and Girl Scouts of Austin. Mission was a test of the launch vehicle, intended to reach 296 x 301 km orbit but fell 20+ km short of planned apogee. Subsequent second firing of upper stage failed to raise perigee sufficiently and resulted in earlier than planned re-entry.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6616	0.0046	208	268	89.26	136.89	167
2022 Oct 2, 04:02	6625	0.0039	222	273	89.45	136.88	171

2022-123 Atlas V 531 Cape Canaveral Space Force Station						2022 Oct 4, 21:36
SES 20 2022-123A 53960						in space
One of a pair of simultaneously launched comsats from SES to provide services to the US. Separated from launch vehicle Oct 5 at 03:14 UTC. Expected location 103° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Oct 6, 15:22	41351	0.0003	34959	34987	1394.73	1.87	159
2022 Oct 13, 15:00	41506	0.0010	35087	35169	1402.58	1.81	177
2022 Oct 16, 07:09	41730	0.0062	35091	35612	1413.92	1.39	105
2022 Oct 19, 15:37	42151	0.0008	35740	35805	1435.38	0.67	247	141°.2 W
2022 Oct 24, 08:01	42165	0.0003	35773	35801	1436.12	0.08	83	141°.2 W
2022 Nov 18, 12:50	42165	0.0003	35773	35801	1436.11	0.02	119	141°.2 W
2022 Nov 21, 11:45	42046	0.0001	35662	35673	1430.02	0.02	300	137°.3 W
2022 Dec 14, 15:09	42157	0.0001	35777	35782	1435.72	0.07	327	103°.2 W
2022 Dec 20, 20:56	42166	0.0001	35785	35791	1436.16	0.08	93	103°.1 W
SES 21 2022-123B 53961						in space
One of a pair of simultaneously launched comsats from SES to provide services to the US. Separated from launch vehicle at 03:54 UTC. Expected location 131° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Oct 6, 08:00	41263	0.0034	34744	35026	1390.28	1.88	184
2022 Oct 13, 16:33	41477	0.0067	34822	35375	1401.08	1.66	168
2022 Oct 24, 16:48	42162	0.0003	35770	35798	1435.96	0.06	126	142°.8 W
2022 Oct 27, 07:09	42166	0.0003	35773	35803	1436.16	0.06	139	142°.9 W
2022 Nov 10, 18:23	42165	0.0001	35784	35789	1436.10	0.04	340	142°.7 W
2022 Nov 14, 17:06	42087	0.0001	35705	35713	1432.14	0.04	98	138°.9 W
2022 Nov 22, 17:57	42122	0.0009	35707	35780	1433.89	0.05	355	131°.0 W
2022 Nov 25, 14:19	42166	0.0002	35779	35797	1436.17	0.04	102	130°.9 W
Atlas V upper stage (Centaur) 2022-123C 53962						in space
Launched SES 20 and SES 21.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 6, 08:12	40232	0.0289	32690	35018	1338.50	1.86	198

2022-124 Falcon 9 Block 5 Kennedy Space Center						2022 Oct 5, 16:00
SpaceX Dragon Crew 5 (Dragon Endurance Flight #2) 2022-124A 53963						Re-entered - 2023 Mar 12 Life 158 days Returned to Earth
Crew flight to ISS provided by SpaceX under contract to NASA. Crew members - Nicole Mann (commander) & Josh Cassada (both NASA), Koichi Wakata (JAXA), and Anna Kikina (Roscosmos). Precise launch time 16:00:56. Separated from launch vehicle at 15:13:03 UTC. Docked with forward port of Harmony module Oct 6 at 21:14 UTC, about 30 mins after the originally published time. Undocked, carrying its original crew, 2023 Mar 11 at 07:19 UTC. Retro-fire Mar 12 at 01:11 UTC led to splashdown at about 02:02 UTC in the Gulf of Mexico off Florida.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 5, 16:24	6578	0.0014	191	210	88.50	51.65	358
2022 Oct 5, 19:17	6597	0.0015	209	228	88.87	51.65	250
2022 Oct 6, 11:28	6598	0.0021	206	233	88.89	51.68	223
2022 Oct 6, 17:43	6795	0.0003	415	418	92.90	51.64	278
2022 Oct 6, 19:12	6793	0.0004	412	417	92.86	51.64	263
2022 Oct 7, 15:20	6795	0.0003	415	419	92.92	51.64	266
2023 Mar 10, 13:15	6797	0.0006	415	423	92.96	51.64	69
2023 Mar 11, 09:34	6786	0.0004	405	411	92.72	51.63	76
2023 Mar 11, 14:10	6734	0.0079	303	410	91.66	51.65	56
2023 Mar 11, 23:00	6734	0.0081	301	410	91.65	51.64	57
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Oct 5 Life <1 day
Launched Crew Dragon 5. Caused to re-enter above Indian Ocean at around 17:00 UTC.
Not Catalogued - orbit parameters unavailable
Crew Dragon trunk module 2022-124B 55840						Re-entered - 2023 Apr 27 Life 204 days
Separated from Dragon Crew 5 shortly before retrofire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 12, 10:56	6733	0.0082	299	410	91.64	51.32	58

2022-125 Falcon 9 Block 5 (Starlink Group 04-29) Vandenberg Space Force Base						2022 Oct 5, 23:10
Starlink 4633 2022-125A 53964						in space
One member of a simultaneously-launched cluster of fifty two LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle Oct 6 at 00:13:02 UTC. All satellites expected to be injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 11, 18:00	6707	0.0002	327	330	91.10	53.22	31
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Oct 6 Life 1 day
Launched fifty four Starlink satellites. Caused to re-enter above the Pacific Ocean Oct 6 at around 01:00 UTC.
Not Catalogued - orbit parameters unavailable

2022-126 CZ 11H Mobile floating platform, Yellow Sea - 36°.6 N, 121°.2 E						2022 Oct 7, 13:10
Wei Li Kongjiang 01-05 (Centispace 01-05) 2022-126A 54020						in space
Satellite for a LEO navigation enhancement system being developed by Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Will also be used to test the Beidou system and to test an inter-satellite laser communication system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 7, 19:11	7078	0.0013	691	709	98.78	55.00	295
Wei Li Kongjiang 01-06 (Centispace 01-06) 2022-126B 54021						in space
Satellite for a LEO navigation enhancement system being developed by Beijing Future Navigation Technology Co Ltd. Satellite developed by the Microsatellite Innovation Research Institute of the Chinese Academy of Sciences. Will also be used to test the Beidou system and to test an inter-satellite laser communication system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 7, 16:07	7078	0.0015	689	710	98.76	55.00	293
CZ 11H fourth stage 2022-126C 54022						Re-entered - 2024 Apr 21 Life 562 days
Launched Centispace 1 S5 and S6 duo. Perigee lowered after releasing satellites. Launch location was 3 km offshore mainland China near Qingdao.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 7, 16:08	6928	0.0346	310	790	95.65	56.15	312

2022-127 Electron (It Argos Up From Here) Rocket Lab Launch Complex, New Zealand						2022 Oct 7, 17:09
GAzelle 2022-127A 54023						in space
Satellite from General Atomics of the US hosting Argos 4 payload from the US National Oceanographic and Atmospheric Administration. Argos will collect weather and climate data via radio beacons at remote locations around the Earth.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Oct 7, 19:31	7131	0.0012	744	762	99.89	98.32	300	05:35
Electron third stage (kick stage) 2022-127B 54024						in space
Launched GAzelle. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 7, 21:08	7031	0.0144	552	754	97.79	98.30	21
Electron second stage 2022-127C 54025						Re-entered - 2023 Feb 27 Life 143 days
Launched GAzelle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 7, 19:51	6902	0.0353	280	767	95.11	98.34	219

2022-128 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Oct 8, 23:05
Galaxy 33 2022-128A 54026						in space
Intelsat-owned communications satellite serving North America. Launched together with Galaxy 34. Released from launch vehicle at 23:37 UTC. Expected location 133° west to replace Galaxy 15 (28884/2005-041A).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Oct 9, 01:26	16442	0.5935	305	19823	349.71	26.84	175
2022 Oct 11, 09:44	16538	0.5958	307	20013	352.78	26.88	178
2022 Oct 14, 19:12	24393	0.7254	320	35709	631.90	26.53	180
2022 Oct 16, 02:24	26405	0.5932	4363	35692	711.70	15.58	180
2022 Oct 17, 10:00	30663	0.3725	12863	35706	890.59	6.86	179
2022 Oct 18, 02:51	39022	0.0825	29424	35865	1278.58	1.06	178
2022 Oct 20, 17:58	40647	0.0353	32835	35703	1359.27	0.40	174
2022 Oct 25, 22:10	42137	0.0000	35758	35760	1434.70	0.04	237	133°.0 W
2022 Oct 26, 18:35	42164	0.0003	35773	35799	1436.07	0.03	285	132°.9 W
Galaxy 34 2022-128B 54027						in space
Intelsat-owned communications satellite serving North America. Launched together with Galaxy 33. Released from launch vehicle at 23:43 UTC. Expected location 129° west to replace Galaxy 12 (27715/2003-013).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Oct 9, 02:40	16449	0.5937	305	19837	349.93	26.84	175
2022 Oct 13, 15:00	22768	0.7066	302	32478	569.84	26.63	180
2022 Oct 17, 10:30	24433	0.7235	377	35734	633.48	26.28	182
2022 Oct 18, 00:27	26718	0.5741	5001	35679	724.38	14.36	183
2022 Oct 20, 01:00	30772	0.3651	13161	35628	895.37	6.61	183
2022 Oct 26, 09:55	42101	0.0016	35657	35790	1432.86	0.06	211	149°.2 W
2022 Oct 29, 03:20	42168	0.0002	35782	35797	1436.24	0.06	175	147°.9 W
2022 Nov 24, 05:31	42080	0.0001	35697	35707	1431.78	0.00	243	146°.1 W
2022 Dec 13, 03:08	42165	0.0002	35779	35794	1436.09	0.02	93	129°.0 W
Falcon 9 upper stage 2022-128C 54028						in space
Launched Galaxy 33 and Galaxy 34.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 10, 22:51	16439	0.5936	302	19820	349.60	26.84	178

2022-129 CZ 2D Jiuquan Space Centre						2022 Oct 8, 23:43
Kuafu 1 (Advanced Space-based Solar Observatory, ASO-S) 2022-129A 54029						in space
Science satellite studying solar flares and coronal mass ejection, and the solar magnetic field.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Oct 9, 20:41	7101	0.0013	713	732	99.25	98.27	264	05:59
CZ 2D second stage 2022-129B 54030						in space
Launched Kuafu 1 (ASOS-S). Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 9, 04:32	7088	0.0020	696	725	98.98	98.19	117

2022-130 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2022 Oct 10, 02:52
Cosmos 2559 (Uragan-K1 № 17L) 2022-130A 54031						in space
GLONASS-K navigation satellite. It also carries radio receiving equipment for the COSPAS-SARSAT international search and rescue system. Released from Fregat at about 06:15 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 11, 13:10	25529	0.0002	19147	19155	676.56	64.78	323
2022 Oct 31, 12:34	25508	0.0008	19110	19149	675.73	64.78	225
Fregat rocket stage 2022-130B 54032						in space
Launched Cosmos 2559 (GLONASS K). Apogee raised after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 11, 03:35	25659	0.0035	19190	19372	681.74	64.89	229

2022-F05 - failed to reach orbit Epsilon Uchinoura Space Center, Japan						2022 Oct 12, 00:50
FSI Sat
1U Cubesat from the Future Science institute, Japan to demonstrate a multi-spectral imager and associated data processing system before transmitting data to Earth. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.
Kosen 2
2U Cubesat from Japan's National Institute of Technology (KOSEN) for marine studies including sub-sea crustal deformation. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Also carries demonstrator of a multi-point communications system. Lost when launcher third stage failed to separate properly.
KOYOH
Science satellite from Kanazawa University, Japan fitted with sensors to study x-ray and gamma ray emissions associated with gravity waves. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.
MAGNARO (MAGnetically separating NAno-satellite with Rotation for Orbit control)
3U Cubesat from Nagoyo University, Japan. Consists of two satellites, Magnaro-Tigris (2U) and Magnaro-Piscis (1U), joined magnetically. They were to separated 6-12 months after launch and conduct formation manoeuvres using air resistance to control the distance between them. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.
Mitsuba
2U Cubesat to be used to monitor and measure degradation of off-the-shelf electronic components. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.
PETREL (Platform for Extra and Terrestrial Remote Examination with LCTF)
Small satellite from the Tokyo Institute of Technology carrying a multi-spectral camera for ocean studies. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.
QPS-SAR 3 (Amateru-II)
Small satellite from Japanese company iQPS, equipped with an Earth imaging radar. Precursor for a constellation that will ultimately consist of 36 satellites. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.
QPS-SAR 4 (Amateru-I)
Small satellite from Japanese company iQPS, equipped with an Earth imaging radar. Precursor for a constellation that will ultimately consist of 36 satellites. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.
RAISE 3 (RApid Innovative payload demonstration SatellitE 3)
Small satellite to demonstrate a range of technology including radio systems, an onboard comuter, a water-based thruster, a plasma thruster and a folded, deployable mebrane panel. Also carries a drag sail to accelerate orbit decay. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.
STARS-X (Space Tethered Autonomous Robotic Satellite)
Two-part satellite from Shizuoka University. The two halves are connected by a 1 km tether to carry a 'climber' moving along the tether with a net to capture space debris. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.
Waseda-Sat-Zero
1U Cubesat from Waseda University, Japan to demonstrate a satellite chassis created in one piece by 3D printing. It was intended to unfold and deploy a membrane panel. Aimed at 560 km sun-synchronous orbit with LTDN 09:30. Lost when launcher third stage failed to separate properly.

2022-131 Proton-M + Blok DM3 Baikonur Cosmodrome						2022 Oct 12, 15:00
Angosat 2 2022-131A 54033						in space
Russian built comsat to be operated by Angosat of Angola with coverage of Africa and southern Europe. Replaces Angosat 1 (43087/2017-086A) that failed while in GEO drift orbit. Released from launch vehicle around 21:00 UTC. Anticipated to enter service 2022 Nov. Expected location - 23° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Oct 13, 14:04	42567	0.0001	36183	36195	1456.68	0.03	119
2022 Oct 21, 19:12	42475	0.0002	36088	36105	1451.96	0.02	124
2022 Oct 27, 14:18	42300	0.0001	35916	35927	1443.00	0.05	69
2022 Oct 31, 00:00	42207	0.0002	35820	35838	1438.24	0.03	207	24°.5 E
2022 Nov 3, 11:34	42167	0.0001	35784	35794	1436.23	0.03	208	23°.1 E
Blok DM-03 rocket stage 2022-131B 54034						in space
Launched Angosat. Initial orbit shown is while Angosat was still attached. Apogee raised after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 12, 20:37	24595	0.7312	233	36201	639.78	48.87	359
2022 Oct 17, 19:23	42887	0.0081	36162	36856	1473.16	0.16	173

2022-132 CZ 2C Taiyuan Space Centre						2022 Oct 12, 22:53
Huanjing 2E (S-SAR 01) 2022-132A 54035						in space
Chinese Earth surface imaging satellite equipped with a synthetic aperture radar operating at S-band frequencies.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Oct 13, 07:50	6873	0.0012	487	503	94.51	97.40	271	06:00
2023 May 10, 07:15	6865	0.0002	485	488	94.34	97.39	87	06:01
2023 May 12, 14:25	6878	0.0003	498	502	94.61	97.39	43	06:01
2023 May 17, 13:49	6882	0.0007	499	509	94.70	97.39	351	06:01
CZ 2C second stage 2022-132E 54039						in space
Launched Huanjing 2E.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 13, 08:21	6897	0.0047	487	552	95.01	97.25	209

2022-133 CZ 2D Xichang Space Centre						2022 Oct 14, 19:12
Yaogan 36-02 Follower 1 2022-133A 54042						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-02 (launch 2022-068) satellites so may represent an enhancement of the constellation. 2022 December, this satellite ceased to maintain its orbit and fell out of the operating formation. However, it continued to make periodic thruster firings. NOTE: Until Oct 26, Space-Track identified this object as 54046/2022-133E.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 15, 04:26	6871	0.0008	488	499	94.47	34.99	266
2022 Oct 24, 07:16	6871	0.0007	488	497	94.46	35.00	342
2022 Nov 16, 03:23	6874	0.0008	490	502	94.53	35.00	200
2023 Feb 15, 12:27	6872	0.0008	488	499	94.48	35.00	326
Yaogan 36-02 Follower 2 2022-133B 54043						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-02 (launch 2022-068) satellites so may represent an enhancement of the constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 15, 03:01	6870	0.0009	486	498	94.45	34.99	282
2022 Oct 20, 22:39	6872	0.0008	488	499	94.48	34.99	340
2022 Nov 16, 09:56	6875	0.0009	490	503	94.55	35.00	255
2023 Feb 15, 13:59	6871	0.0012	485	501	94.48	35.00	328
Yaogan 36-02 Leader 2022-133D 54045						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-02 (launch 2022-068) satellites so may represent an enhancement of the constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 15, 03:01	6869	0.0009	485	497	94.43	34.99	288
2022 Oct 24, 00:31	6872	0.0014	484	503	94.48	35.00	2
2022 Nov 16, 03:15	6875	0.0007	492	501	94.54	35.00	244
2023 Feb 15, 13:58	6872	0.0011	486	501	94.48	35.00	342
CZ 2D second stage 2022-133E 54046						Re-entered - 2023 Aug 26 Life 316 days
Launched Yaogan 36 Group 2. Space-Track tags this item as debris but the scatter pattern of objects after launch points to it being the CZ upper stage. NOTE: Until Oct 26, Space-Track identified this object as 54042/2022-133A.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 15, 03:00	6871	0.0009	487	499	94.46	35.00	272

2022-134 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Oct 15, 05:22
Eutelsat Hot Bird 13F 2022-134A 54048						in space
Comsat providing direct TV service to homes in Europe. Released from launch vehicle at 05:58 UTC. Expected location - 13° east as part of the replacement program for Hotbirds 9A, 13B and 13C.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Oct 16, 17:20	34452	0.8041	372	55775	1060.65	26.83	181
2022 Oct 22, 09:36	35443	0.7960	854	57277	1106.79	25.11	182
2022 Nov 1, 18:55	37475	0.7709	2207	59987	1203.30	21.37	185
2022 Nov 11, 07:12	39494	0.7553	3285	62947	1301.85	18.39	187
2022 Nov 21, 17:38	41992	0.7300	4962	66266	1427.27	15.19	188
2022 Nov 21, 18:05	41400	0.7258	4974	65069	1397.19	15.12	187
2022 Nov 22, 20:00	41194	0.7358	4506	65125	1386.79	14.97	189
2022 Nov 29, 04:39	42609	0.7064	6133	66328	1458.84	13.45	190
2022 Dec 7, 22:56	43212	0.6812	7397	66271	1489.93	11.87	191
2022 Dec 14, 04:38	43826	0.6372	9520	65375	1521.79	10.07	191
2022 Dec 22, 09:42	43802	0.5944	11386	63461	1520.53	8.21	193
2022 Dec 27, 21:49	43955	0.5623	12862	62293	1528.54	7.49	195
2023 Jan 4, 22:00	44160	0.5140	15083	60481	1539.25	5.89	196
2023 Jan 11, 20:00	44088	0.4682	17068	58352	1535.46	5.13	196
2023 Jan 18, 20:00	44069	0.4208	19149	56233	1534.49	4.14	198
2023 Jan 25, 12:41	43657	0.3715	21060	53497	1513.00	3.56	200
2023 Feb 3, 00:00	43669	0.3019	24107	50475	1513.63	2.55	201
2023 Feb 8, 06:01	43763	0.2723	25466	49303	1518.50	2.47	205
2023 Feb 15, 16:01	41050	0.2246	25451	43892	1379.51	1.78	203
2023 Feb 23, 14:24	43197	0.1476	30443	43195	1489.15	1.28	204
2023 Mar 1, 10:40	42869	0.0967	32347	40634	1472.21	0.87	204
2023 Mar 10, 21:35	42263	0.0219	34958	36811	1441.10	0.31	196
2023 Mar 16, 01:10	42166	0.0000	35787	35789	1436.17	0.12	325	1°.6 E
2023 Apr 2, 06:24	42164	0.0001	35783	35789	1436.06	0.08	158	1°.6 E
2023 Apr 3, 09:03	42207	0.0001	35825	35833	1438.25	0.08	159	1°.1 E
2023 Apr 5, 09:14	42169	0.0002	35783	35800	1436.33	0.07	105	0°.4 E
2023 Apr 6, 20:37	42164	0.0001	35781	35791	1436.07	0.07	74	0°.4 E
2023 Jul 25, 23:54	42165	0.0002	35780	35793	1436.09	0.08	335	1°.4 E
Falcon 9 upper stage 2022-134B 54049						in space
Launched Hotbird 13F.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 18, 22:20	34702	0.8048	397	56251	1072.25	26.84	181

2022-135 Angara 1.2 Plesetsk Cosmodrome						2022 Oct 15, 19:55
Cosmos 2560 2022-135A 54050						Re-entered - 2022 Dec 10 Life 56 days
Possible imaging reconnaissance satellite carried on a test launch of the Angara 1.2 rocket. LTDN matches Cosmos 2555 (52330/2022-044A) and Cosmos 2551 (49127/2021-081A), First launch attempt cancelled late in countdown on Oct 14. Re-entered naturally.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Oct 15, 23:16	6714	0.0011	329	344	91.26	96.35	250	11:30
2022 Dec 9, 19:24	6540	0.0005	159	166	87.74	96.31	286	11:19
orbit insertion stage uncatalogued						Re-entered - 2022 Oct 15 Life <1 day
Launched Cosmos 2560. Apogee raised after releasing satellite. Caused to re-enter above central Pacific Ocean at about 23:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6908	0.0291	329	731	95.24	96.35	250

2022-136 Falcon 9 Block 5 (Starlink Group 04-36) Cape Canaveral Space Force Station						2022 Oct 20, 14:50
Starlink 5195 2022-136A 54051						in space
One member of a simultaneously-launched cluster of fifty four LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 15:05 UTC. All satellites expected to be injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 25, 16:00	6681	0.0032	282	324	90.58	53.22	56
Falcon 9 upper stage uncatalogued						in space
Launched fifty four Starlink satellites. Caused to re-enter above the Indian Ocean at around (probably) 16:00 UTC.
Not Catalogued - orbit parameters unavailable

2022-137 Soyuz-2.1v + Volga Plesetsk Cosmodrome						2022 Oct 21, 19:20
Cosmos 2561 2022-137A 54109						in space
Military satellite, one of a simultaneously-launched, but not necessarily related, pair - purpose unknown but may have an Earth observation mission. Released from Volga stage shortly after 20:17 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Oct 22, 10:36	6793	0.0008	409	421	92.86	97.08	263	10:58
2023 Jan 30, 22:22	6782	0.0007	399	409	92.64	97.07	257	10:58
2023 Jan 31, 12:16	6784	0.0009	399	412	92.67	97.07	245	10:58
2023 Apr 5, 21:22	6771	0.0009	387	399	92.42	97.06	16	10:59
2023 Apr 6, 14:20	6784	0.0011	398	414	92.69	97.06	219	10:59
2023 Sep 19, 12:39	6767	0.0008	383	395	92.34	97.05	242	11:02
2023 Sep 19, 20:22	6775	0.0012	389	405	92.50	97.05	243	11:02
2023 Sep 21, 10:56	6775	0.0012	389	405	92.49	97.04	237	11:02
2023 Sep 21, 16:16	6782	0.0013	395	413	92.64	97.03	258	11:02
2023 Sep 22, 10:07	6785	0.0012	398	415	92.69	97.04	240	11:02
2023 Sep 26, 14:35	6784	0.0012	397	414	92.68	97.05	224	11:01
2023 Sep 26, 19:14	6794	0.0013	407	424	92.88	97.05	241	11:01
2023 Oct 29, 13:41	6788	0.0014	401	419	92.77	97.04	125	11:01
2023 Oct 29, 18:20	6796	0.0008	413	423	92.93	97.04	183	11:01
2023 Oct 30, 19:08	6804	0.0012	417	434	93.08	97.04	245	11:01
2023 Oct 31, 19:59	6811	0.0012	425	441	93.23	97.04	241	11:00
2023 Nov 1, 14:39	6818	0.0013	431	449	93.38	97.04	236	11:00
2023 Nov 3, 21:13	6828	0.0012	441	458	93.58	97.04	240	11:00
Cosmos 2562 2022-137B 54110						Re-entered - 2023 Nov 8 Life 383 days
Military satellite, one of a simultaneously-launched, but not necessarily related, pair. Released from Volga stage shortly after 20:17 UTC. 2022 November - Resurs-P 3 (41386, 2016-016A) manoeuvred alongside it and was then used as a rendezvous target, possibly to test a satellite servicing mission profile. Manoeuvres ceased 2023 July 26 and the orbit then decayed naturally up to re-entry.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Oct 22, 13:42	6791	0.0008	408	419	92.83	97.08	255	10:58
2022 Oct 28, 10:35	6791	0.0009	407	419	92.82	97.08	231	10:58
2022 Oct 28, 16:46	6789	0.0010	404	417	92.78	97.08	247	10:58
2022 Oct 31, 12:51	6786	0.0012	400	416	92.73	97.08	247	10:58
2022 Nov 14, 21:39	6785	0.0013	398	415	92.69	97.08	190	10:58
2022 Nov 16, 09:08	6770	0.0005	389	395	92.40	97.10	223	10:58
2023 Jan 15, 21:27	6763	0.0013	376	393	92.24	97.19	30	11:04
2023 Jan 16, 13:19	6769	0.0016	380	402	92.38	97.19	348	11:04
2023 Jan 23, 15:49	6768	0.0015	379	400	92.35	97.19	320	11:05
2023 Jan 24, 17:59	6764	0.0012	377	394	92.26	97.19	359	11:05
2023 Jan 25, 12:27	6763	0.0012	377	393	92.26	97.18	357	11:05
2023 Jan 25, 18:36	6763	0.0012	377	394	92.26	97.18	356	11:05
2023 Feb 13, 13:17	6760	0.0011	374	389	92.18	97.18	280	11:07
2023 Feb 13, 18:26	6763	0.0014	375	394	92.25	97.18	270	11:07
2023 Feb 15, 20:40	6763	0.0014	375	395	92.25	97.18	265	11:08
2023 Feb 16, 21:16	6760	0.0010	375	389	92.19	97.18	266	11:08
2023 Mar 27, 22:26	6753	0.0011	367	382	92.04	97.17	113	11:12
Soyuz upper stage 2022-137C 54111						Re-entered - 2022 Nov 3 Life 13 days
Launched Cosmos 2661 and 2662 pair. Originally planned for launch Oct 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 22, 04:27	6672	0.0156	189	398	90.39	97.08	71
Volga rocket stage 2022-137D 54112						Re-entered - 2022 Oct 22 Life 1 day
Launched Cosmos 2561 and 2562 pair. Orbit circularised at about 20:17 UTC. First orbit listed covers the period when Volga and the satellites were still attached to each other. Caused to re-enter after releasing the satellites, possibly as late as Oct 22, around 07:15 UTC. Originally planned for launch Oct 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6673	0.0161	188	403	90.42	97.08	72
2022 Oct 21, 22:47	6793	0.0007	410	419	92.86	97.08	263

2022-138 LVM3 (M2) Satish Dhawan Space Centre						2022 Oct 22, 18:37
OneWeb 0490 2022-138A 54113						in space
Broadband distribution satellite for the UK company OneWeb. One of 36 similar satellites carried on this launch, released from the upper stage of the launch vehicle in nine batches of four over a period of three hours.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 25, 16:00	6975	0.0011	588	604	96.61	87.43	285
LVM3 third stage 2022-138AN 54149						in space
Launched 36 OneWeb satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 25, 12:13	6985	0.0023	591	623	96.83	87.39	274

2022-139 Soyuz-2.1b + Fregat Vostochny Cosmodrome						2022 Oct 22, 19:57
Gonets 35 (Gonets M-35) 2022-139A 54150						in space
Store and forward communications satellite for Russia's civil/commercial system. Released from Fregat at 21:35 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 23, 02:01	7870	0.0012	1483	1502	115.81	82.50	263
2022 Nov 7, 05:00	7876	0.0017	1485	1511	115.94	82.50	212
2022 Dec 3, 18:17	7873	0.0022	1477	1512	115.86	82.51	157
Gonets 34 (Gonets M-34) 2022-139B 54151						in space
Store and forward communications satellite for Russia's civil/commercial system. Released from Fregat at 21:35 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 23, 01:56	7870	0.0012	1482	1501	115.79	82.49	271
2022 Nov 20, 23:01	7873	0.0016	1481	1507	115.86	82.50	193
Gonets 33 (Gonets M-33) 2022-139C 54152						in space
Store and forward communications satellite for Russia's civil/commercial system. Released from Fregat at 21:35 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 23, 03:26	7868	0.0013	1479	1500	115.76	82.50	263
2022 Nov 29, 03:10	7872	0.0020	1478	1510	115.86	82.51	176
Skif-D 2022-139D 54153						in space
Demonstrator satellite for a broadband distribution system. Released from Fregat Oct 23 at 00:04 UTC. The first orbit listed is based on radio observations made by the amateur community while awaiting Space-Track data that eventually surfaced more than three months after launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 1, 12:40	14438	0.0007	8050	8070	287.75	90.01	200
Fregat rocket stage 2022-139E 54154						in space
Launched three Gonets-M and the Skif-D satellite. The first orbit listed is based on visual observations made by the amateur community while awaiting Space-Track data that eventually surfaced more than three months after launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Feb 1, 14:28	14493	0.0005	8109	8122	289.41	90.01	25

2022-140 Soyuz-2.1a Baikonur Cosmodrome						2022 Oct 26, 00:20
Progress MS-21 (Progress 7K-MS №451) 2022-140A 54155						Re-entered - 2023 Feb 19 Life 116 days
Supplies and equipment to ISS. Docked with the Poisk module of ISS Oct 28 at 02:49 UTC. Undocked 2023 February 18, 02:56:23 UTC but stayed alongside ISS to allow damage inspection of area around coolant leak. Retro-fire February 19, 03:15 UTC above central Asia led to destructive re-entry with any surviving debris hitting the surface of the southern Pacific Ocean around 03:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 26, 06:28	6648	0.0021	256	284	89.91	51.64	5
2022 Oct 27, 18:20	6796	0.0006	414	422	92.94	51.64	11
2023 Feb 17, 12:46	6794	0.0009	410	423	92.89	51.64	0
2023 Feb 18, 10:23	6795	0.0008	411	423	92.91	51.64	11
Soyuz upper stage 2022-140B 54156						Re-entered - 2022 Oct 28 Life 2 days
Launched Progress MS-21.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 26, 06:25	6580	0.0024	186	217	88.52	51.66	73

2022-141 Falcon 9 Block 5 (Starlink Group 04-31) Vandenberg Space Force Base						2022 Oct 28, 01:14
Starlink 5290 2022-141A 54157						in space
One member of a simultaneously-launched cluster of fifty three LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at about 01:40 UTC. All satellites expected to be injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 3, 14:00	6687	0.0020	295	322	90.70	53.22	197
Falcon 9 upper stage uncatalogued						in space
Launched fifty three Starlink satellites. Caused to re-enter after releasing satellites
Not Catalogued - orbit parameters unavailable

2022-142 CZ 2D Jiuquan Space Centre						2022 Oct 29, 01:01
Shiyan 20C (Chuangxin 3C?) 2022-142A 54214						in space
Space Technology Demonstrator - precise purpose unknown.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 29, 13:51	7151	0.0033	749	796	100.30	60.00	156
2022 Nov 2, 11:35	7179	0.0010	794	808	100.89	60.00	271
CZ 2D second stage 2022-142B 54215						in space
Launched Shiyan 20C.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 29, 04:23	7158	0.0027	761	799	100.46	59.90	199

2022-143 CZ 5B Wenchang Space Centre						2022 Oct 31, 07:37
Mengtian 2022-143A 54216						in space
Chinese Space Station module. Separated from launch vehicle at 07:45 UTC. Docked with the forward-facing port of Tianhe at 20:27 UTC on day of launch. Nov 3, after a manoeuvre lasting for about one hour, a robotic arm docked it with a side port opposite Wentian at 01:32 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 31, 11:45	6627	0.0109	177	320	89.48	41.46	167
2022 Oct 31, 14:42	6690	0.0032	291	333	90.77	41.52	232
2022 Oct 31, 18:08	6762	0.0005	380	387	92.22	41.47	272
2022 Oct 31, 22:47	6762	0.0005	380	387	92.22	41.47	276
CZ 5B second stage 2022-143B 54217						Re-entered - 2022 Nov 4 Life 4 days
Launched Mengtian.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Oct 31, 13:19	6620	0.0106	171	312	89.34	41.47	174

2022-144 Falcon Heavy Kennedy Space Center						2022 Nov 1, 13:41
LDPE 2/ESPA 2 (Long Duration Propulsive Evolved Expendable Launch Vehicle Secondary Payload Adapter) 2022-144A 54219						in space
Secondary satellite carried on the USSF-44 mission. Platform built by Northrop Grumman carrying a number of undisclosed payloads that may include one or more small satellites. Probably separated from launch vehicle as it climbed to graveyard orbit.
Near-geosynchronous altitude - parameters awaited
USA 339 (USSF-44 main payload) 2022-144B 54220						in space
Primary payload of the USSF-44 mission, details are classified secret but it may have a communications mission. Probably separated from launch vehicle ~19:40 UTC. Aimed at an unannounced geosynchronous location.
Geosynchronous orbit - location unknown
USA 340 (Tetra 1) 2022-144E 55138						in space
Demonstrator for satellite systems for use at geosynchronous orbital altitude including communications systems and clandestine observation of activities on the Earth's surface. TETRA may be an acronym but the meaning is unknown. Association with USA 340 is uncertain, TETRA may be USA 341. Probably released from ESPA 2 within days of launch. Catalogued 2023 January 10 and first unclassified orbit data was released 2023 Mar 28.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2023 Mar 28, 12:54	42291	0.0008	35881	35944	1442.54	2.24	256
2023 May 16, 18:20	42229	0.0000	35850	35851	1439.35	3.02	88	49°.0 W
2023 Jun 16, 15:49	42374	0.0001	35992	36000	1446.79	3.21	124
2023 Jul 20, 17:39	42229	0.0000	35850	35851	1439.37	3.19	251	131°.3 W
2023 Aug 2, 11:21	42067	0.0003	35677	35701	1431.12	3.20	158	132°.5 W
2023 Aug 25, 07:55	42062	0.0006	35659	35709	1430.85	3.28	278	102°.9 W
USA 341 2022-144F 55139						in space
Probably a demonstrator for satellite systems for use at geosynchronous orbital altitude including communications systems and clandestine observation of activities on the Earth's surface. Probably released from ESPA 2 within days of launch. Catalogued 2023 January 14.
Near-geosynchronous altitude - parameters awaited
LINUSS 1 (Lockheed Martin In-space Upgrade Satellite System) 2022-144G 55246						in space
12U Cubesat (4x3) - one of a pair carried on the USSF-44 mission. Demonstrator mission with re-configurable software to control how its imaging/detector system works and equipped with a low thrust engine to control its orbit. Probably released from ESPA 2 within days of launch but not catalogued 2023 until January 14. First orbit data released 2023 March 28.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 28, 01:37	42509	0.0011	36085	36176	1453.71	2.52	298
LINUSS 2 (Lockheed Martin In-space Upgrade Satellite System) 2022-144H 55247						in space
12U Cubesat (4x3) - one of a pair carried on the USSF-44 mission. Demonstrator mission with re-configurable software to control how its imaging/detector system works and equipped with a low thrust engine to control its orbit. Probably released from ESPA 2 within days of launch but not catalogued 2023 until January 14. First orbit data released 2023 March 28.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 24, 03:43	42509	0.0009	36091	36171	1453.74	2.51	299
USA 344 2022-144J 56307						in space
Mission details awaited. Probably a Cubesat released from LDPE 2 (2022-144A), possibly during 2023 April but may have been earlier.
Near-geosynchronous altitude - parameters awaited
USA 399 2022-144K 60741						in space
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
Falcon 9 third stage 2022-144C 54221						in space
Launched USA 339 and other payloads.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 28, 02:18	42783	0.0053	36179	36630	1467.78	3.10	195
debris item 2022-144D 54222						in space
Separated from Falcon 9 or LDPE 2.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Mar 28, 16:31	42567	0.0002	36179	36199	1456.71	2.84	251

2022-145 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2022 Nov 2, 06:48
Cosmos 2563 (EKS 6/Tundra 16L) 2022-145A 54223						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 2, 14:19	26458	0.6975	1625	38536	713.85	63.83	270
2022 Nov 10, 14:40	26483	0.6982	1614	38596	714.85	63.83	270
2022 Nov 23, 13:05	26553	0.6996	1599	38751	717.68	63.82	270
Fregat rocket stage 2022-145B 54224						in space
Launched Cosmos 2663.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 3, 18:17	26435	0.6982	1601	38513	712.91	63.87	270

2022-146 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Nov 3, 05:22
Eutelsat Hotbird 13G 2022-146A 54225						in space
Comsat providing direct TV service to homes in Europe, North. Africa and the Middle East. Released from launch vehicle at 05:58 UTC. Expected location - 13° east as part of the replacement program for Hotbirds 9A, 13B and 13C.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Nov 3, 07:57	35295	0.8080	399	57435	1099.84	27.66	180
2022 Nov 15, 08:02	36895	0.7914	1319	59714	1175.46	24.20	183
2022 Nov 23, 06:54	36555	0.7846	1495	58859	1159.26	21.06	188
2022 Dec 1, 09:36	39757	0.7881	2046	64712	1314.85	18.56	188
2022 Dec 2, 02:24	40281	0.7568	3419	64387	1340.95	18.62	185
2022 Dec 5, 21:25	41301	0.7441	4191	65655	1392.20	16.98	187
2022 Dec 10, 19:12	42025	0.7339	4806	66488	1428.98	15.48	188	20°.5 W
2022 Dec 28, 08:54	43017	0.6707	7786	65493	1479.88	10.73	191
2023 Jan 4, 04:53	44152	0.6431	9378	66170	1538.82	9.04	194
2023 Jan 10, 12:00	44422	0.5890	11879	64209	1552.96	7.99	193
2023 Jan 18, 20:00	44475	0.5395	14101	62094	1555.75	6.61	194
2023 Jan 25, 18:00	44528	0.4961	16058	60241	1558.49	5.56	195
2023 Feb 1, 13:23	44354	0.4498	18026	57925	1549.36	4.85	197
2023 Feb 7, 11:05	44613	0.4298	19058	57411	1562.95	4.14	197
2023 Feb 15, 09:34	44169	0.3523	22231	53350	1539.70	3.36	200
2023 Feb 21, 00:00	44064	0.3223	23482	51889	1534.21	3.19	203
2023 Feb 28, 10:03	43176	0.2634	25424	48171	1488.06	2.24	200
2023 Mar 7, 11:08	42943	0.1916	28336	44795	1476.05	1.72	200
2023 Mar 14, 09:25	43287	0.1482	30496	43323	1493.84	1.24	206
2023 Mar 21, 14:55	42780	0.0954	32320	40482	1467.62	0.55	163
2023 Mar 28, 08:33	42294	0.0504	33785	38046	1442.70	0.48	198
2023 Apr 5, 00:41	42058	0.0096	35276	36083	1430.64	0.16	193	11°.9 E
2023 Apr 13, 08:17	42165	0.0001	35783	35791	1436.11	0.06	257	11°.2 E
2023 May 22, 06:49	42165	0.0002	35780	35793	1436.09	0.03	275	11°.2 E
2023 May 22, 15:07	42152	0.0006	35747	35801	1435.44	0.03	220	11°.3 E
2023 May 25, 08:08	42115	0.0002	35730	35745	1433.56	0.02	286	13°.0 E
2023 May 26, 19:12	42164	0.0001	35783	35789	1436.07	0.02	2	13°.0 E
Falcon 9 upper stage 2022-146B 54226						in space
Launched Hotbird 13G.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 3, 08:07	35174	0.8075	392	57199	1094.17	27.60	180

2022-147 Electron (Catch Me If You Can) Rocket Lab Launch Complex, New Zealand						2022 Nov 4, 17:27
MATS (Mesospheric Airglow/Aerosol Tomography and Spectroscopy) 2022-147A 54227						in space
Swedish satellite designed to investigate atmospheric waves - density variations in the upper atmosphere caused by lower-level winds encountering such as mountains as they move across the Earth's surface. Released from launch vehicle about one hour after launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 5, 21:29	6967	0.0012	581	597	96.46	97.65	303	05:50
Electron third stage (kick stage) 2022-147B 54228						in space
Launched MATS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 5, 13:26	6968	0.0012	581	598	96.47	97.65	312
Electron second stage 2022-147C 54229						Re-entered - 2022 Nov 20 Life 16 days
Launched MATS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 5, 15:40	6760	0.0284	190	574	92.19	97.55	227

2022-148 CZ 3B Xichang Space Centre						2022 Nov 5, 11:50
Zhongxing 19 (Chinasat 19) 2022-148A 54230						in space
Comsat providing services for important trans-Pacific routes, the eastern Pacific Ocean and the west coast of North America. Manoeuvred to Geosynchronous Drift Orbit, probably November 7.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Nov 5, 15:13	24381	0.7294	220	35787	631.46	28.38	179
2022 Nov 15, 12:23	42165	0.0007	35758	35815	1436.10	0.03	354	163°.5 E
CZ 3B fourth stage 2022-148B 54231						Re-entered - 2023 May 10 Life 186 days
Launched Zhongxing 19.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 5, 23:03	23688	0.7232	180	34441	604.73	28.40	179

2022-149 Antares 230+ Wallops Flight Facility						2022 Nov 7, 10:32
Cygnus NG-18 (SS Sally Ride) 2022-149A 54232						Re-entered - 2023 Apr 22 Life 166 days
Northrop Grumman vehicle carrying supplies to ISS under CRS-2 contract with NASA. One of its two solar panels failed to open after arrival on orbit. Captured by ISS Remote Manipulator Nov 9, 10:22 UTC and docked with the downward-facing port of Unity at 13:05 UTC. Undocked 2023 Apr 21 at 08:37 UTC and released from the RMS at 11:22 UTC. Retro-fire Apr 21 at ~02:30 UTC was followed by destructive re-entry above the Pacific Ocean at around 03:10 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6616	0.0111	164	311	89.25	51.63	150
2022 Nov 7, 13:38	6659	0.0080	228	334	90.13	51.67	147
2022 Nov 8, 13:04	6704	0.0127	240	411	91.04	51.68	124
2022 Nov 9, 03:21	6790	0.0012	404	420	92.81	51.65	42
Antares second stage 2022-149B 54233						Re-entered - 2022 Nov 9 Life 2 days
Launched Cygnus NG-18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 7, 13:36	6607	0.0095	166	291	89.07	51.65	146

2022-150 Atlas V 401 Vandenberg Space Force Base						2022 Nov 10, 09:49
NOAA 21 (Joint Polar Satellite System 2) 2022-150A 54234						in space
US meteorological satellite belonging to the National Oceanographic and Atmospheric Agency measuring weather conditions in the Earth's atmosphere and providing weather images from polar orbit. Released from launch vehicle at 10:17 UTC. Accepted into service and name changed to NOAA 21 on Nov 21.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 10, 16:19	7189	0.0023	794	827	101.10	98.70	239	01:25
2022 Nov 17, 14:55	7190	0.0025	794	829	101.12	98.70	224	01:25
2022 Dec 7, 08:50	7197	0.0013	810	829	101.28	98.70	162	01:25
2022 Dec 15, 12:45	7196	0.0012	809	827	101.26	98.70	141	01:25
2022 Dec 19, 11:23	7205	0.0001	826	828	101.44	98.70	80	01:25
LOFTID (Low-Earth Orbit Flight Test of an Inflatable Decelerator) uncatalogued						in space
Test of a 6 metre diameter inflatable aeroshell and heatshield - joint project between NASA and ULA (operators of the Atlas V). Released from Atlas upper stage at 11:04 UTC. Re-entered 11:36 UTC, data recorder separated 11:42 UTC then descended by parachute for splashdown shortly before 12:00 UTC mid-Pacific about 500 km east of Hawaii. The heat shield itself landed close by at 12:02 UTC also by parachute.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6690	0.0509	-29	653	90.76	98.01	165
Atlas V upper stage (Centaur) uncatalogued						Re-entered - 2022 Nov 10 Life <1 day
Launched JPSS 2 and LOFTID. Second orbit listed followed 10:34 UTC retro-firing. Third orbit is the re-entry trajectory set up for LOFTID after retro-firing at 10:54 UTC. Re-entered mid Pacific at about 11:35 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	7188	0.0013	801	819	101.08	98.70	240
estimated orbit	7077	0.0249	523	875	98.75	98.46	320
estimated orbit	6690	0.0509	-29	653	90.76	98.01	165

2022-151 CZ 6A (Y-2) Taiyuan Space Centre						2022 Nov 11, 22:52
Yunhai 3-01 2022-151A 54235						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. The first two listed orbits should be treated with caution.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 12, 05:07	7226	0.0011	840	856	101.89	98.82	264	05:59
2022 Nov 15, 13:00	7230	0.0032	829	875	101.96	98.81	54	05:59
2022 Nov 30, 11:29	7226	0.0001	847	849	101.89	98.82	122	05:59
CZ 6A third stage 2022-151B 54236						in space
Launched Yunhai 3. Was observed from North America about one hour after launch and seen to be trailed by a debris cloud, probably related to it later breaking into several hundred items of debris Nov 12 at around 05:25 UTC, probably as the result of a propellant explosion.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 12, 08:58	7210	0.0036	806	857	101.54	98.87	4
2022 Nov 12, 15:15	7210	0.0028	812	853	101.56	98.82	350

2022-152 CZ 7 (Y-6) Wenchang Space Centre						2022 Nov 12, 02:03
Tianzhou 5 2022-152A 54237						Re-entered - 2023 Sep 12 Life 304 days
Supplies to Chinese Space Station - support for the upcoming Shenzhou 15 mission. Inital orbit similar to the CZ 7 rocket stage. Docked with Tianhe rear port 04:10 UTC. 2022 December 18, Tianzhou released the Macau Student Satellite (54816/2021-035C) from its external Cubesat deployer - see launch entry for that date. Undocked 2023 May 5, 07:26:53 UTC and moved away from CSS to await Shenzhou 15 undocking. Docked with Tianhe forward-facing port Jun 5 at 19:10 UTC. Undocked 2023 September 11 at 08:46 UTC. Retro-fire shortly after 00:30 UTC on September 12 resulted in destructive re-entry into the Earth's atmosphere at 01:13 UTC above the southern Pacific Ocean. Any survivng debris would have hit the ocean surface about 10 minutes later.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 12, 09:34	6766	0.0010	381	395	92.31	41.48	274
2023 May 5, 02:27	6758	0.0006	375	384	92.14	41.47	197
2023 May 6, 06:35	6754	0.0007	371	381	92.07	41.48	160
2023 May 23, 04:00	6752	0.0010	367	380	92.02	41.47	277
2023 May 23, 15:12	6770	0.0054	355	428	92.39	41.50	347
2023 May 24, 10:56	6786	0.0029	388	428	92.72	41.48	310
2023 May 24, 19:03	6777	0.0009	393	405	92.54	41.48	296
2023 Jun 4, 05:31	6776	0.0007	393	403	92.52	41.47	10
2023 Jun 4, 16:57	6792	0.0019	401	427	92.84	41.47	260
2023 Jun 5, 06:31	6754	0.0003	374	378	92.07	41.47	283
2023 Jun 5, 21:27	6766	0.0004	386	391	92.32	41.48	304
2023 Sep 9, 10:58	6760	0.0010	375	389	92.19	41.48	333
2023 Sep 11, 10:59	6763	0.0011	378	392	92.26	41.47	16
CZ 7 third stage 2022-152B 54238						Re-entered - 2022 Nov 14 Life 2 days
Launched Tianzhou 5.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 12, 06:29	6689	0.0166	200	421	90.73	41.84	180

2022-153 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Nov 12, 16:06
Galaxy 31 2022-153A 54243						in space
Intelsat-owned communications satellite serving North America. Launched together with Galaxy 32. Expected location 121° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Nov 12, 20:21	35736	0.8136	283	58433	1120.51	24.20	180
2022 Nov 14, 14:50	39375	0.6084	9042	56952	1295.97	8.91	182
2022 Nov 15, 06:44	40742	0.5866	10463	58265	1364.03	8.92	181
2022 Nov 16, 15:55	52298	0.2359	33584	58256	1983.76	1.61	181
2022 Nov 17, 18:09	52958	0.2071	35613	57547	2021.43	1.33	181
2022 Nov 21, 07:26	42168	0.0017	35719	35862	1436.28	0.02	106	148°.1 W
2022 Nov 23, 17:58	42201	0.0009	35785	35862	1437.96	0.02	113	148°.7 W
2022 Nov 24, 14:52	42167	0.0002	35782	35796	1436.23	0.02	72	148°.9 W
2022 Nov 28, 11:19	42165	0.0001	35782	35792	1436.10	0.02	116	149°.0 W
2022 Dec 21, 07:03	42146	0.0004	35752	35785	1435.16	0.05	237	148°.8 W
2022 Dec 23, 16:28	42111	0.0002	35724	35740	1433.33	0.04	158	147°.6 W
2023 Jan 27, 13:26	42109	0.0002	35721	35740	1433.23	0.05	53	123°.1 W
2023 Feb 1, 14:47	42154	0.0003	35762	35790	1435.56	0.05	76	121°.2 W
2023 Feb 5, 23:47	42164	0.0003	35772	35800	1436.07	0.05	46	121°.0 W
Galaxy 32 2022-153C 54244						in space
Intelsat-owned communications satellite serving North America. Launched together with Galaxy 31. Expected location 91° west
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Nov 12, 20:06	35761	0.8131	306	58459	1121.69	22.26	178
2022 Nov 14, 14:55	37981	0.6302	7666	55539	1227.74	8.76	183
2022 Nov 15, 06:54	40901	0.5826	10693	58353	1372.01	8.75	181
2022 Nov 16, 15:12	52403	0.2351	33705	58346	1989.75	1.49	182
2022 Nov 16, 22:55	53360	0.2128	35630	58335	2044.50	1.22	182
2022 Nov 21, 02:51	42146	0.0014	35707	35828	1435.13	0.05	342	149°.3 W
2022 Nov 24, 05:59	42166	0.0002	35780	35796	1436.16	0.04	289	149°.0 W
2023 Jan 17, 16:40	42047	0.0002	35659	35679	1430.10	0.10	46	141°.6 W
2023 Feb 14, 14:26	42046	0.0003	35655	35680	1430.02	0.04	53	99°.0 W
2023 Feb 23, 23:14	42165	0.0003	35775	35798	1436.08	0.02	326	91°.0 W
Falcon 9 upper stage 2022-153C 54248						Re-entered - 2024 Mar 30 Life 504 days
Launched Galaxy 31 and Galaxy 32.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 14, 16:55	35588	0.8166	150	58270	1113.58	24.43	180

2022-154 CZ 4C Xichang Space Centre						2022 Nov 15, 01:38
Yaogan 34-03 2022-154A 54249						in space
Imaging satellite - orbit is similar to the Yaogan 31 electronic surveillance satellites, and the Initial orbit plane has RAAN about three degrees to the east of that of the fourth Yaogan 31 triplet (launch no 2021-020). Expected to move into formation with the Yaogan 31 group.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 15, 14:26	7473	0.0003	1092	1097	107.14	63.41	272
2022 Nov 17, 20:51	7462	0.0009	1077	1091	106.92	63.41	251
CZ 4C third stage 2022-154B 54250						in space
Launched Yaogan 34-03. Perigee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 15, 13:22	7382	0.0122	914	1093	105.20	63.41	45

2022-155 Ceres 1 (Gushenxing 1 Y-4) Jiuquan Space Centre						2022 Nov 15, 02:20
Jilin-1 High Resolution 03D 54 (Jilin-1 GF3D 54) 2022-155A 54251						in space
High resolution, multi-spectral imaging satellite. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 16, 13:48	6916	0.0013	529	547	95.41	97.54	292	12:38
Jilin-1 High Resolution 03D 53 (Jilin-1 GF3D 53) 2022-155B 54252						in space
High resolution, multi-spectral imaging satellite. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 16, 14:21	6916	0.0013	529	548	95.41	97.54	290	12:38
Jilin-1 High Resolution 03D 52 (Jilin-1 GF3D 52) 2022-155C 54253						in space
High resolution, multi-spectral imaging satellite. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 16, 15:52	6917	0.0013	530	548	95.42	97.54	286	12:38
Jilin-1 High Resolution 03D 51 (Jilin-1 GF3D 51) 2022-155D 54254						in space
High resolution, multi-spectral imaging satellite. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 16, 15:52	6917	0.0014	529	548	95.41	97.54	289	12:38
Jilin-1 High Resolution 03D 08 (Jilin-1 GF3D 08) 2022-155E 54255						in space
High resolution, multi-spectral imaging satellite. Designation and Catalogue Number to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 16, 18:58	6916	0.0014	529	548	95.41	97.54	288	12:38
Ceres 1 fourth stage uncatalogued						Re-entered - 2022 Nov 15 Life <1 day
Launched group of five Jilin -1 HR imaging sats. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-156 SLS Kennedy Space Center						2022 Nov 16, 06:47
Artemis 1 (Orion) 2022-156A 54257						Re-entered - 2022 Dec 11 Life 25 days
Primary goals for Artemis I are to demonstrate Orion’s systems in a spaceflight environment and ensure a safe re-entry, descent, splashdown, and recovery prior to the first flight with crew on Artemis 2. The mission will last 4-6 weeks and involve six days orbiting the Moon. Slashdown expected in the Pacific Ocean off California. Artemis released ten Cubesats into Barycentric orbit. Entered orbit around the Moon following engine firing that commenced November 25 at 22:52 UTC. Departed Lunar orbit Dec 5, splashed down off California Dec 11 at 17:40 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 16, 09:07	195034	0.9646	518	376794	14286.48	30.53	21
ArgoMoon uncatalogued						in space
6U Cubesat - will perform station-keeping manoeuvres alongside the SLS upper stage. Released from ICPS Orion Adapter after departure of Artemis.
Earth-Moon Barycentric Orbit
BioSentinel uncatalogued						in space
6U Cubesat - from NASA Ames Research Center to spend 18 months studying the effects of deep space radiation on living organisms, namely dry yeast cells. Released from ICPS Orion Adapter after departure of Artemis.
Earth-Moon Barycentric Orbit
CuSP (Cubesat to study Solar Particles) uncatalogued						in space
6U Cubesat - to observe particles and magnetic fields streaming away from the sun before they reach Earth. Released from ICPS Orion Adapter after departure of Artemis. Activated as expected but ceased to operate within about 12 hrs of launch.
Earth-Moon Barycentric Orbit
EQUULEUS (Equilibrium Lunar-Earth point 6U Spacecraft) uncatalogued						in space
6U Cubesat - trajectory will take it beyond the Moon to the Earth-Moon Lagrange point 2 from where it will study the Earth's plasmasphere by way of imaging. Released from ICPS Orion Adapter after departure of Artemis.
Earth-Moon Barycentric Orbit
Lunar Ice Cube uncatalogued						in space
6U Cubesat - from NASA Goddard to enter orbit around the Moon and investigate the distribution of water and other volatiles and how they vary by time of day, latitude, and lunar soil composition. Released from ICPS Orion Adapter after departure of Artemis.
Earth-Moon Barycentric Orbit
Lunar Polar Hydrogen Mapper (LunaH-Map) uncatalogued						in space
6U Cubesat - carries instruments to determine the amount of water ice beneath the surface of the lunar south pole. Released from ICPS Orion Adapter after departure of Artemis.
Earth-Moon Barycentric Orbit
LunIR uncatalogued						in space
6U Cubesat - developed by Lockheed Martin to collect thermal images of the Moon’s surface and demonstrate the performance of CubeSat components in deep space. Released from ICPS Orion Adapter after departure of Artemis.
Earth-Moon Barycentric Orbit
NEA Scout (Near-Earth Asteroid Scout) uncatalogued						in space
6U Cubesat - developed under NASA’s Advanced Exploration Systems Program, and will deploy a 86 square meter solar sail to fly by a near-Earth asteroid and take photographs to help determine the asteroid’s physical properties. Released from ICPS Orion Adapter after departure of Artemis.
Earth-Moon Barycentric Orbit
OMOTENASHI (Outstanding Moon exploration Technologies demonstrated by Nano Semi-Hard Impactor) uncatalogued						in space
6U Cubesat - developed by JAXA and the University of Tokyo to prove the capability of small, cost-effective lunar landers to explore the Moon's surface. Intended to use a solid-propellant rocket to make a semi-hard landing on the lunar surface. Released from ICPS Orion Adapter after departure of Artemis. Excessive rotation followed by OMOTENASHI taking up an attitude that prevented output from its solar panels meant that a lunar landing was not possible.
Earth-Moon Barycentric Orbit
Team Miles uncatalogued						in space
6U Cubesat - to demonstrate navigation in deep space using a new type of plasma thruster. Released from ICPS Orion Adapter after departure of Artemis.
Earth-Moon Barycentric Orbit
SLS upper stage (Interim Cryogenic Propulsion Stage) 2022-156B 54258						in space
Launched Artemis 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 16, 09:07	191343	0.9640	517	369413	13882.82	30.50	21

2022-157 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Nov 23, 02:57
Eutelsat 10B 2022-157A 54259						in space
Comsat providing land, maritime and aeronautical services to the Atlantic Ocean, Europe, the Mediterranean basin, Africa and the Indian Ocean. Released from launch vehicle at 03:32 UTC. Equipped with electric thruster to move from transfer orbit to operational orbit. Originally Catalogued by Space-Track as 54260/2022-157B. Expected location - 10° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Nov 23, 20:55	36403	0.8180	247	59803	1152.03	22.66	178
2022 Dec 1, 14:24	36930	0.8091	673	60430	1177.12	22.56	180
2022 Dec 6, 22:47	37965	0.7993	1243	61931	1226.98	20.29	182
2022 Dec 13, 15:08	39399	0.7870	2013	64029	1297.15	18.05	184
2022 Dec 28, 00:22	43086	0.7479	4482	68933	1483.40	12.52	189
2023 Jan 4, 22:30	43941	0.7133	6220	68905	1527.78	10.47	190
2023 Jan 10, 10:00	44312	0.6858	7544	68323	1547.16	9.34	192
2023 Jan 19, 00:00	44903	0.6378	9886	67164	1578.24	7.82	194
2023 Jan 25, 18:00	44938	0.5957	11792	65329	1580.11	6.73	195
2023 Feb 1, 14:28	44506	0.5386	14158	62098	1557.35	5.90	197
2023 Feb 6, 23:24	44763	0.5106	15528	61242	1570.87	5.35	198
2023 Feb 13, 00:00	44769	0.4665	17506	59275	1571.16	4.55	200
2023 Feb 19, 04:37	46039	0.4473	19066	60256	1638.52	4.41	206
2023 Feb 27, 14:24	44099	0.3569	21984	53458	1536.03	3.47	203
2023 Mar 6, 00:25	43401	0.3008	23970	50076	1499.71	2.82	205
2023 Mar 13, 09:21	43531	0.2651	25612	48693	1506.44	2.35	204
2023 Mar 20, 15:20	43534	0.2648	25630	48682	1506.62	1.62	211
2023 Mar 27, 18:22	42938	0.1684	29330	43789	1475.77	1.37	207
2023 Apr 3, 00:45	43071	0.1645	29607	43780	1482.66	1.06	214
2023 Apr 13, 13:24	43072	0.1643	29618	43770	1482.70	0.42	218
2023 Apr 19, 05:20	42240	0.0101	35434	36289	1439.92	0.19	185	1°.7 E
2023 Apr 21, 14:10	42165	0.0015	35722	35852	1436.11	0.14	168	1°.6 E
2023 Jul 8, 01:59	42165	0.0003	35775	35799	1436.11	0.04	19	1°.6 E
2023 Jul 11, 08:36	42021	0.0000	35641	35644	1428.74	0.04	143	5°.9 E
2023 Jul 14, 04:17	42163	0.0002	35777	35793	1436.00	0.05	121	10°.0 E
Falcon 9 upper stage 2022-157B 54260						in space
Launched Eutelsat 10B.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 24, 18:28	36295	0.8173	252	59581	1146.89	22.74	179

2022-158 PSLV-XL (PSLV C-54) Satish Dhawan Space Centre						2022 Nov 26, 06:26
EOS 06 (Earth Observation Satellite 6) 2022-158A 54361						in space
Indian civil Earth observation satellite for ocean studies. Released from launch vehicle at 06:43 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 26, 10:58	7117	0.0014	729	749	99.59	98.34	264	11:59
Thybolt 1 2022-158C 54363						Re-entered - 2024 May 20 Life 541 days
0.5U Cubesat carrying a demonstration communications payload and a store-forward communications package operating in the amateur radio band. Released from launch vehicle around 07:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 27, 04:11	6887	0.0011	501	516	94.80	97.45	256
Thybolt 2 2022-158D 54364						Re-entered - 2024 May 24 Life 545 days
0.5U Cubesat carrying a demonstration communications payload and a store-forward communications package operating in the amateur radio band. Released from launch vehicle around 07:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 27, 04:22	6887	0.0011	501	516	94.80	97.45	257
INS 2B (India-Bhutan Sat) 2022-158E 54365						Re-entered - 2024 Jun 13 Life 565 days
Small satellite built by ISRO for Bhutan. Equipped with a multi-spectral visible-light imaging system and an amateur radio payload. Released from launch vehicle around 07:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 27, 04:22	6886	0.0011	500	515	94.78	97.45	267	12:01
Anand 2022-158F 54366						Re-entered - 2024 Sep 21 Life 665 days
Technology demonstration satellite carrying a miniaturised Earth imaging system. Released from launch vehicle around 07:30 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Nov 27, 04:22	6885	0.0009	501	514	94.77	97.44	269	12:01
Astrocast 16 (Astrocast 0304) 2022-158G 54367						in space
3U Cubesat in a planned eighty satellite constellation to provide communications for internet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 27, 04:21	6884	0.0007	501	511	94.74	97.45	265
Astrocast 15 (Astrocast 0303) 2022-158H 54368						Re-entered - 2024 Dec 3 Life 738 days
3U Cubesat in a planned eighty satellite constellation to provide communications for internet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 26, 23:57	6883	0.0007	500	510	94.73	97.45	288
Astrocast 14 (Astrocast 0302) 2022-158J 54369						in space
3U Cubesat in a planned eighty satellite constellation to provide communications for internet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 27, 01:08	6883	0.0008	499	511	94.72	97.45	285
Astrocast 13 (Astrocast 0301) 2022-158K 54370						in space
3U Cubesat in a planned eighty satellite constellation to provide communications for internet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 27, 04:10	6883	0.0008	499	510	94.72	97.45	286
PSLV upper stage 2022-158B 54362						in space
Launched EOS 6 and several small satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 27, 00:04	6894	0.0022	500	531	94.94	97.46	247

2022-159 Falcon 9 Block 5 Kennedy Space Center						2022 Nov 26, 19:20
SpaceX Dragon 2 CRS-26 2022-159A 54371						Re-entered - 2023 Jan 11 Life 46 days Returned to Earth
Carrying a cargo to/from the ISS under NASA's Commercial Resupply Services (CRS) contract. Separated from launch vehicle at 02:28 UTC, docked with the upward-facing port of the Harmony module of ISS Nov 27 at 12:39 UTC. Undocked 2023 Jan 9 at 22:05 UTC. retrofire Jan 11 at 09:35 UTC led to splashdown in the Gulf of Mexico at 10:19 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 26, 21:14	6603	0.0023	210	240	89.00	51.64	240
2022 Nov 27, 06:18	6783	0.0003	403	406	92.65	51.66	124
2023 Jan 9, 14:15	6795	0.0005	413	420	92.90	51.65	242
2023 Jan 10, 03:43	6783	0.0003	403	407	92.67	51.64	255
2023 Jan 10, 13:07	6661	0.0132	195	371	90.18	51.65	157
2023 Jan 11, 07:00	6670	0.0118	213	370	90.35	51.65	158
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Nov 26 Life <1 day
Launched Dragon CRS-26. Caused to re-enter above the southern Pacific Ocean at about 20:20 UTC.
Not Catalogued - orbit parameters unavailable
Dragon 2 trunk module 2022-159B 55241						Re-entered - 2023 Jan 21 Life 56 days
Separated from Dragon 2 CRS-26 2023 January 11 prior to retrofire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 12, 21:41	6662	0.0110	211	357	90.19	51.64	164

2022-160 CZ 2D Xichang Space Centre						2022 Nov 27, 12:23
Yaogan 36-03 Leader 2022-160A 54372						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-05 (launch 2022-109) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 27, 20:13	6873	0.0009	489	501	94.51	34.99	282
2022 Dec 5, 07:53	6877	0.0006	495	503	94.59	35.00	295
Yaogan 36-03 Follower 2 2022-160C 54374						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-05 (launch 2022-109) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 28, 04:15	6874	0.0009	490	502	94.53	35.00	274
2022 Dec 3, 17:44	6877	0.0005	496	503	94.60	35.00	274
Yaogan 36-03 Follower 1 2022-160E 54376						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-05 (launch 2022-109) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 27, 23:31	6875	0.0008	491	502	94.55	35.00	260
2022 Dec 3, 17:46	6877	0.0010	492	506	94.59	34.99	311
CZ 2D second stage 2022-160B 54373						Re-entered - 2023 Oct 24 Life 331 days
Launched Yaogan 36 Group 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 27, 22:58	6874	0.0009	490	502	94.54	34.99	264

2022-161 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2022 Nov 28, 15:17
Cosmos 2564 (Uragan-M) 2022-161A 54377						in space
GLONASS navigation satellite to fill a space in the constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 29, 06:02	25517	0.0006	19124	19153	676.07	64.78	272
2022 Dec 2, 05:44	25458	0.0027	19010	19149	673.74	64.79	232
2022 Dec 19, 13:21	25508	0.0043	19020	19240	675.72	64.75	141
Fregat rocket stage 2022-161B 54378						in space
Launched Cosmos 2564. Moved to higher orbit after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 28, 21:14	25707	0.0070	19149	19509	683.67	64.75	61

2022-162 CZ 2F Jiuquan Space Centre						2022 Nov 29, 15:08
Shenzhou 15 2022-162A 54379						Re-entered - 2023 Jun 3 Life 186 days Returned to Earth
Crew to CSS - Fei Junlong (commander), Deng Qingming and Zhang Lu. Separated from launch vehicle at 15:17 UTC. Matched orbit with CSS at about 19:30 UTC then docked with the forward-facing port of the Tianhe module at 21:42 UTC. Undocked carrying original crew 2023 Jun 3 at 13:29 UTC. Retrofire at 21:41 UTC led to landing in the Gobi Desert, Mongolia reportedly at 22:33 UTC but more likely 22:31 UTC. The first orbit listed is an estimate based on Chinese data.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 28, 15:18	6659	0.0121	200	361	90.12	41.48	125
2022 Nov 29, 19:40	6768	0.0006	386	393	92.34	41.48	336
2022 Nov 30, 08:10	6768	0.0006	386	393	92.34	41.48	340
2023 Jun 3, 14:12	6767	0.0004	386	391	92.33	41.47	289
CZ 2F third stage 2022-162B 54380						Re-entered - 2022 Dec 11 Life 12 days
Launched Shenzhou 15.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Nov 30, 06:21	6647	0.0110	196	342	89.89	41.47	128
Shenzhou 15 Orbital Module 2022-162C 56873						Re-entered - 2024 Apr 2 Life 490 days
Released from Shenzhou 15 2023 Jun 3 at 21:42 UTC. Re-entry observed from the Los Angeles area 2024 April 2 at about 08:45 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jun 7, 12:01	6770	0.0008	387	397	92.40	41.49	327
2024 Apr 2, 05:50	6525	0.0000	147	147	87.42	41.47	55

2022-163 Soyuz-2.1b Plesetsk Cosmodrome						2022 Nov 30, 21:10
Cosmos 2565 (Lotos-S1 № 6) 2022-163A 54381						in space
Electronic intelligence gathering - signals intelligence (SIGINT) satellite. Vehicle is based on the design of the Yantar satellite. Launch time estimated from initial orbit data. Perigee raised towards operational height Dec 2 around 07:20 UTC. Settled into operational orbit Dec 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 1, 01:49	6948	0.0476	239	900	96.06	67.14	92
2022 Dec 2, 23:17	7283	0.0009	898	912	103.09	67.15	334
2022 Dec 4, 21:21	7281	0.0008	897	908	103.04	67.16	322
2022 Dec 5, 19:41	7285	0.0006	903	911	103.13	67.15	280
2022 Dec 7, 02:37	7284	0.0007	900	911	103.10	67.15	270
Cosmos 2566 2022-163D 54817						in space
Small military satellite, purpose undisclosed. Separated from Cosmos 2565 on December 2 at around 23:20 UTC. Orbit raised by 2 km on December 24 at about 14:00 UTC as it separated from 54383/2022-163C. Minor orbit change 2023 March 10/11. Possibly intended to move away and conduct independent manoeuvres, including rendezvous with 54383/2022-163C but did not do so. The mission appears to have been re-flown by Cosmos 2571 (58162, 2023-165C).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 24, 19:19	7283	0.0011	896	913	103.09	67.15	322
Soyuz third stage 2022-163B 54382						Re-entered - 2023 May 22 Life 173 days
Launched Cosmos 2565.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 1, 01:02	6937	0.0464	237	881	95.84	67.14	92
Carrier vehicle/support structure 2022-163C 54383						in space
Separated from Cosmos 2566 on December 24 at around 14:00 UTC when orbit lowered by about 1 km.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 3, 02:44	7282	0.0010	896	911	103.07	67.15	328
2022 Dec 25, 06:58	7281	0.0012	895	911	103.05	67.14	313

2022-I11 JEM Small Satellite Orbital Deployer International Space Station						2022 Dec 2, 07:50
Space-Tuna 1 1998-067UL 54534						Re-entered - 2023 May 16 Life 165 days
1U Cubesat developed by Kindai University, Japan. Covered in a selection of reflective materials to return laser transmissions from the ground. Also fitted with blue LED lights for ground telescope observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 5, 14:50	6793	0.0007	410	420	92.86	51.64	135
PearlAfricaSat 1 1998-067UM 54535						Re-entered - 2023 Apr 25 Life 144 days
1U Cubesat from Uganda, equipped with an Earth-imaging system. One of three satellites in the BIRDS 5 cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 5, 14:50	6793	0.0008	410	420	92.86	51.64	135
TAKA 1998-067UN 54536						Re-entered - 2023 May 31 Life 180 days
2U Cubesat from Kyushu Institute of Technology, Japan. Equipped with a demonstration store and forward messaging system, an amateur radio payload, science instruments for monitoring the space environment, and an Earth imaging system to look at natural resources. One of three satellites in the BIRDS 5 cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 5, 14:50	6793	0.0008	410	420	92.86	51.64	135
ZimSat 1 1998-067UP 54537						Re-entered - 2023 May 16 Life 165 days
1U Cubesat built by Zimbabwean engineers working with the Kyushu Institute of Technology in Japan. Equipped with an Earth imaging system to study natural resources. Also equipped with an amateur radio payload. One of three satellites in the BIRDS 5 cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 5, 16:23	6793	0.0008	409	420	92.86	51.64	136

2022-164 Kuaizhou 11 Jiuquan Space Centre						2022 Dec 7, 01:15
VDES Test Satellite (Jiaotong?) 2022-164A 54588						in space
Demonstrator for VDES (VHF Data Exchange System). VDES adds two-way capability to the existing AIS service so ocean-going ships can both receive and send short messages from/to other ships or land-based stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Dec 7, 16:20	7122	0.0008	738	750	99.69	98.35	279	07:30
Kuaizhou 11 third stage 2022-164B 54589						in space
Launched VDES Test satellite. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 7, 17:14	6922	0.0382	280	809	95.53	98.37	103

2022-165 CZ 2D Taiyuan Space Centre						2022 Dec 8, 18:31
Gaofen 5-01A 2022-165A 54640						in space
Environmental satellite with multi-spectral imaging equipment and detectors for greenhouse gasses, infrared radiation and trace gasses. Launched to similar LTDN as Gaofen 5-01 (43461/2018-043A).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Dec 9, 08:42	7054	0.0011	668	683	98.27	98.12	268	01:35
2022 Dec 11, 10:09	7062	0.0011	675	691	98.43	98.12	313	01:35
2022 Dec 13, 10:03	7074	0.0006	692	700	98.68	98.11	340	01:35
2022 Dec 14, 05:57	7079	0.0002	700	702	98.79	98.12	73	01:35
2022 Dec 14, 22:07	7079	0.0001	700	701	98.78	98.12	87	01:35
CZ 2D second stage 2022-165B 54641						in space
Launched Gaofen 5-01A.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 9, 08:42	7054	0.0034	652	700	98.27	98.03	302

2022-166 Falcon 9 Block 5 Kennedy Space Center						2022 Dec 8, 22:27
OneWeb 0527 2022-166A 54642						in space
Broadband distribution satellite for the UK company OneWeb. One of 40 similar satellites carried on this launch, all initially in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 12, 16:00	6972	0.0007	589	599	96.57	86.52	222
Falcon 9 second stage uncatalogued						Re-entered - 2022 Dec 9 Life 1 day
Launched forty OneWeb satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-167 Jielong 3 (Y2) Mobile floating platform, Yellow Sea - 37°.3 N, 123°.7 E						2022 Dec 9, 06:35
Jilin-1 High Resolution 03D 44 (Jilin-1 GF3D 44) 2022-167A 54682						Re-entered - 2024 Oct 30 Life 691 days
High resolution, multi-spectral imaging satellite. Carries an amateur radio payload. One of four similar satellites carried on this launch, all are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Dec 10, 06:07	6919	0.0013	531	550	95.45	97.54	262	14:41
CAS 5A 2022-167C 54684						Re-entered - 2025 Mar 11 Life 823 days
6U Cubesat carrying an amateur radio payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 10, 13:51	6918	0.0013	531	549	95.45	97.54	262
Fengtai 2 2022-167xx						in space
Small scientific satellite carrying a microgravity experiment. May be a Cubesat.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6916	0.0013	529	547	95.40	97.54	278
Golden Bauhinia 1-05 (Jinzijing 1-05) 2022-167xx						in space
Satellite from the Hong Kong Aerospace Technology Group for a future constellation of 165 LEO remote sensing satellites equipped with optical and radar imagers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6916	0.0013	529	547	95.40	97.54	278	14:41
Golden Bauhinia 1-06 (Jinzijing 1-06) 2022-167xx						in space
Satellite from the Hong Kong Aerospace Technology Group for a future constellation of 165 LEO remote sensing satellites equipped with optical and radar imagers.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6916	0.0013	529	547	95.40	97.54	278	14:41
Head 2H (Jiaotong 5) 2022-167xx						in space
Application satellite from Head Aerospace in the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications between internet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6916	0.0013	529	547	95.40	97.54	278
Jilin-1 High Resolution 03D 47 (Jilin-1 GF3D 47) 2022-167xx						in space
High resolution, multi-spectral imaging satellite. One of four similar satellites carried on this launch, all are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6916	0.0013	529	547	95.40	97.54	278	14:41
Jilin-1 Platform 01 A01 (Jilin-1 P01 A01) 2022-167xx						in space
Imaging satellite, also carries a payload to improve navigation accuracy of systems on the ground.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
estimated orbit	6916	0.0013	529	547	95.40	97.54	278	14:41
Tianqi 7 2022-167xx						in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Part of the planned 38 satellite Guodian Gaoke (Apocalypse) constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6916	0.0013	529	547	95.40	97.54	278
Jielong 3 fourth stage 2022-167B 54683						Re-entered - 2023 Oct 6 Life 301 days
Launched fourteen satellites. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 10, 00:44	6823	0.0206	304	585	93.48	97.59	323

2022-168 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Dec 11, 07:38
HAKUTO-R 1 2022-168A 54696						in space
Lunar lander from Japanese private company ispace inc. Aimed to enter orbit around the Moon and then to land on the surface to release Rashid (from UAE). Separated from launch vehicle at 08:24 UTC. Entered orbit around the Moon 2023 Mar 21.
In orbit around the Moon
Lunar Flashlight 2022-168B 54697						in space
6U Cubesat from NASA's Jet Propulsion Laboratory aimed to enter orbit round the Moon and use near-infrared lasers and an onboard spectrometer to map ice in permanently shadowed regions near the Moon's south pole. Released from launch vehicle at 08:30 UTC. Problems with its thrusters meant it was not able to enter lunar orbit. It will pass by the moon at intervals and be able to use its instruments.
Earth-Moon Barycentric Orbit
Falcoln 9 upper stage 2022-168C 54698						in space
Launched HAKUTO-R 1 and Lunar Flashlight. Orbit shown is the coast around Earth before the stage was fired for a second time to achieve Barycentric orbit before releasing the satellites. A third firing disposed of it to heliocentric orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 11, 07:46	6610	0.0098	167	297	89.13	29.00	60

2022-169 CZ 4C Jiuquan Space Centre						2022 Dec 12, 08:22
Shiyan 20A (Chuangxin 3A?) 2022-169A 54699						in space
Unspecified demonstration payload. Initial Right Ascension of orbit Ascending Node is 60° west of Shiyan 20C (2022-142 launch). Dec 28 - settled into identical orbit to Shiyan 20B, but 30° ahead of it around the orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 12, 11:32	7173	0.0007	790	799	100.76	59.99	246
2022 Dec 29, 10:03	7174	0.0004	793	799	100.80	60.00	269
Shiyan 20B (Chuangxin 3B?) 2022-169B 54700						in space
Unspecified demonstration payload. Initial Right Ascension of orbit Ascending Node is 60° west of Shiyan 20C (2022-142 launch).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 12, 11:33	7172	0.0007	789	799	100.74	60.00	257
2022 Dec 13, 11:06	7174	0.0006	792	800	100.79	59.99	214
2022 Dec 29, 11:20	7174	0.0007	791	801	100.79	60.00	252
CZ 4C third stage 2022-169C 54701						in space
Launched Shiyan 20 A and 20 B pair. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 12, 11:29	7106	0.0093	661	794	99.35	59.95	41

2022-170 Ariane 5ECA (VA-259) Centre Spatiale Guyanaise						2022 Dec 13, 20:30
Galaxy 35 2022-170A 54741						in space
Intelsat-owned comsat covering North America to replace Galaxy 3C. Separated from launch vehicle at 20:57 UTC. Expected location 95° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Dec 15, 09:42	24281	0.7257	283	35522	627.56	5.90	177
2022 Dec 15, 21:37	27082	0.5572	5615	35793	739.25	3.29	179
2022 Dec 21, 22:56	42130	0.0011	35705	35798	1434.31	0.05	160	150°.5 W
2022 Dec 23, 17:15	42163	0.0002	35776	35795	1436.03	0.05	154	150°.1 W
2023 Feb 13, 12:23	42066	0.0018	35613	35763	1431.05	0.03	164	147°.3 W
2023 Feb 14, 17:39	42008	0.0002	35620	35641	1428.12	0.01	339	144°.7 W
2023 Mar 15, 12:02	42165	0.0003	35774	35800	1436.13	0.01	275	94°.8 W
Galaxy 36 2022-170B 54742						in space
Intelsat-owned comsat covering North America to replace Galaxy 28. Separated from launch vehicle at 21:00 UTC. Expected location 89° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Dec 15, 09:36	24369	0.7280	251	35732	630.99	6.02	179
2022 Dec 16, 10:31	26845	0.5691	5191	35743	729.55	3.43	179
2022 Dec 22, 00:59	42132	0.0008	35720	35789	1434.45	0.02	36	150°.2 W
2022 Dec 23, 17:26	42165	0.0002	35779	35794	1436.10	0.01	293	150°.0 W
2023 Jan 29, 04:58	42063	0.0004	35670	35701	1430.92	0.03	197	148°.5 W
2023 Jan 29, 04:58	42026	0.0009	35608	35687	1429.00	0.03	356	148°.4 W
2023 Jan 30, 09:34	41978	0.0002	35590	35610	1426.58	0.04	199
2023 Feb 22, 15:16	42088	0.0002	35700	35720	1432.18	0.02	211	91°.3 W
2023 Feb 26, 03:35	42165	0.0002	35777	35797	1436.10	0.01	306	89°.0 W
MTG - I1 (Meteosat Third Generation - Imager 1) 2022-170C 54743						in space
First of a new generation of meteorological imaging and data collection satellites covering Europe and Africa. Separated from launch vehicle at 21:04 UTC. Expected longitude 0°. Will be renamed Meteosat 12 on acceptance into service.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2022 Dec 13, 23:42	24379	0.7283	246	35755	631.35	6.05	178
2022 Dec 15, 21:47	24576	0.7142	646	35750	639.04	5.52	179
2023 Jan 4, 21:54	42165	0.0000	35785	35788	1436.10	0.95	129	3°.4 W
2023 Feb 4, 22:32	42167	0.0002	35780	35798	1436.20	0.88	87	3°.4 W
2023 Feb 18, 06:40	42165	0.0003	35775	35798	1436.11	0.85	109	3°.6 W
2023 Jul 25, 06:38	42164	0.0003	35775	35797	1436.05	0.64	143	3°.2 W
Ariane 5 upper stage 2022-170E 54745						in space
Launched MTG-I1, Galaxy 35 and Galaxy 36.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 13, 23:14	24423	0.7283	258	35832	633.08	6.05	178

2022-F06 - failed to reach orbit Zhuque-2 (Y1) Jiuquan Space Centre						2022 Dec 14, 08:30
Multiple satellites
Possibly as many as 14 unspecified payloads - lost when launch vehicle developed a problem soon after lift-off and failed to reach orbit. Reportedly the second stage failed to run its full duration so the whole stack fell short of orbital velocity. Aimed at sun-synchronous orbit with LTDN about 14:50.

2022-171 CZ 2D Xichang Space Centre						2022 Dec 14, 18:25
Yaogan 36-04 Follower 1 2022-171A 54746						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-03 (launch 2022-088) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 15, 06:40	6875	0.0008	491	502	94.55	35.00	265
2022 Dec 31, 02:20	6877	0.0007	494	504	94.59	34.99	38
2023 Feb 15, 04:25	6872	0.0007	489	499	94.50	35.00	188
Yaogan 36-04 Follower 2 2022-171C 54748						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-03 (launch 2022-088) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 15, 10:17	6873	0.0009	489	501	94.52	35.00	278
2022 Dec 31, 02:18	6877	0.0006	495	503	94.60	35.00	101
2023 Feb 15, 04:25	6873	0.0004	492	497	94.50	35.00	112
Yaogan 36-04 Leader 2022-171E 54750						in space
Chinese government or military remote sensing reconnaissance satellite. One of three similar satellites carried on the same launch vehicle and orbiting in formation. Launched into the same orbit plane as the three Yaogan 35-03 (launch 2022-088) satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 15, 08:49	6873	0.0009	488	501	94.50	35.00	287
2022 Dec 31, 02:14	6877	0.0013	490	508	94.59	34.99	45
2023 Feb 15, 04:19	6873	0.0011	487	502	94.51	35.00	121
CZ 2D second stage 2022-171B 54747						Re-entered - 2023 Nov 6 Life 327 days
Launched Yaogan 36 Group 4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 15, 10:18	6874	0.0009	490	502	94.53	35.00	271

2022-172 CZ 11 Xichang Space Centre						2022 Dec 16, 06:17
Shiyan 21 (Test 21) 2022-172A 54752						in space
Demonstrator mission with unspecified purpose. Orbit maintained by periodic thruster firings.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 16, 17:20	6861	0.0014	474	493	94.27	36.00	304
2023 Jan 11, 06:59	6860	0.0013	473	491	94.24	36.00	179
2023 Jan 11, 23:36	6866	0.0006	483	492	94.36	36.00	162
2023 Jan 15, 06:26	6866	0.0006	483	492	94.36	36.00	192
2023 Jan 16, 18:14	6861	0.0004	480	485	94.26	36.00	137
2023 Jan 31, 22:12	6837	0.0042	430	488	93.77	36.00	308
2023 Feb 5, 11:11	6856	0.0088	418	538	94.16	35.93	156
2023 Feb 5, 19:29	6861	0.0028	464	502	94.26	36.00	21
2023 Feb 22, 12:56	6860	0.0026	464	500	94.25	36.00	172
2023 Feb 22, 19:23	6861	0.0026	465	501	94.27	36.01	177
2023 Sep 30, 02:15	6878	0.0017	488	512	94.61	35.98	63
2023 Oct 2, 23:56	6863	0.0041	457	513	94.31	36.06	18
CZ 11 fourth stage uncatalogued						in space
Launched Shiyan 21. Caused to re-enter after releasing satellite.
Not Catalogued - orbit parameters unavailable

2022-173 Falcon 9 Block 5 Vandenberg Space Force Base						2022 Dec 16, 11:46
SWOT (Surface Water and Ocean Topography) 2022-173A 54754						in space
Joint NASA/CNES satellite to undertake global survey of Earth's surface water, observe fine details of ocean surface topography, and measure how water bodies change over time. Released from launch vehicle at 12:38 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 17, 12:41	7236	0.0003	856	860	102.10	77.59	31
2023 Jan 3, 03:35	7239	0.0001	860	861	102.15	77.60	69
2023 Jan 3, 15:01	7241	0.0002	861	864	102.20	77.59	80
2023 Jan 12, 12:01	7238	0.0001	860	861	102.15	77.60	267
2023 Jan 14, 23:38	7238	0.0005	856	863	102.13	77.60	104
Falcon 9 second stage uncatalogued						in space
Launched SWOT. Caused to re-enter the Earth's atmosphere above the central Pacific Ocean about two hours after launch.
Not Catalogued - orbit parameters unavailable

2022-174 Falcon 9 Block 5 Cape Canaveral Space Force Station						2022 Dec 16, 22:48
O3b mPower FM01 2022-174A 54755						in space
Second generation communications satellite, owned by SES, to provide broadband links between ground stations lying in the range ±45° latitude. In addition to the broad area coverage of 1st gen satellites, mPower satellites are equipped with spot beam aerials. Released from launch vehicle Dec 17 at 00:48 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 17, 09:21	11264	0.1871	2779	6993	198.29	9.61	182
2023 Jan 10, 16:30	11728	0.1643	3422	7276	210.65	8.05	248
2023 Jan 12, 18:42	11776	0.1623	3487	7309	211.96	7.97	252
2023 Jan 14, 02:37	11803	0.1588	3551	7299	212.70	7.86	255
2023 Jan 22, 06:34	12045	0.1424	3951	7383	219.27	7.10	274
2023 Jan 24, 12:04	12104	0.1358	4082	7369	220.87	6.88	280
2023 Jan 28, 15:49	12229	0.1300	4261	7441	224.32	6.61	289
2023 Jan 29, 22:36	12241	0.1301	4270	7456	224.65	6.52	291
2023 Feb 8, 18:17	12459	0.1184	4606	7556	230.67	5.89	313
2023 Feb 13, 12:24	12610	0.1114	4827	7636	234.86	5.48	321
2023 Feb 14, 15:50	12637	0.1097	4872	7645	235.63	5.40	323
2023 Feb 21, 01:54	12760	0.1048	5045	7719	239.08	4.99	335
2023 Feb 28, 16:50	13002	0.0956	5381	7868	245.92	4.27	348
2023 Mar 7, 14:01	13218	0.0855	5711	7970	252.07	3.54	360
2023 Mar 14, 04:44	13365	0.0790	5931	8042	256.27	3.02	10
2023 Mar 21, 10:27	13569	0.0676	6274	8108	262.17	2.34	21
2023 Mar 28, 17:12	13762	0.0574	6594	8174	267.79	1.54	31
O3b mPower FM02 2022-174B 54756						in space
Second generation communications satellite, owned by SES, to provide broadband links between ground stations lying in the range ±45° latitude. In addition to the broad area coverage of 1st gen satellites, mPower satellites are equipped with spot beam aerials. Released from launch vehicle Dec 17 at 00:48 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 17, 09:30	11263	0.1869	2779	6991	198.27	9.61	182
2023 Feb 8, 18:00	12769	0.1043	5059	7723	239.32	4.97	308
2023 Feb 15, 06:14	13021	0.0870	5510	7775	246.44	4.58	318
2023 Feb 22, 20:19	13192	0.0862	5677	7951	251.33	3.88	332
2023 Mar 1, 08:52	13377	0.0774	5963	8034	256.62	3.31	341
2023 Mar 8, 01:32	13609	0.0675	6312	8150	263.34	2.64	351
2023 Mar 15, 16:08	13847	0.0559	6695	8242	270.26	1.82	3
2023 Mar 21, 13:01	14009	0.0462	6984	8278	275.02	1.21	8
2023 Mar 28, 18:40	14209	0.0312	7388	8273	280.93	0.58	15
Falcon 9 second stage 2022-174C 54757						in space
Launched 2x O3b satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 17, 08:04	11267	0.1868	2784	6994	198.38	9.62	182

2022-175 Falcon 9 Block 5 (Starlink Group 04-37) Kennedy Space Center						2022 Dec 17, 21:32
Starlink 5464 2022-175A 54758						in space
One member of a simultaneously-launched cluster of fifty four LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from launch vehicle at 21:47 UTC. All satellites expected to be injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 28, 02:00	6718	0.0002	338	340	91.32	53.22	32
Falcon 9 second stage uncatalogued						Re-entered - 2022 Dec 17 Life <1 day
Launched 54 Starlink satellites. Caused to re-enter above the Indian Ocean about 50 minutes after launch
Not Catalogued - orbit parameters unavailable

2022-C01 External Cubesat Deployer - Tianzhou 5 Chinese Space Station						2022 Dec 18, 01:30
Macau Student Science Satellite 1 2021-035C 54816						Re-entered - 2023 Mar 15 Life 87 days
8U Cubesat (4x2) built for China's Macau University of Science and Technology (MUST). it carries a number of educational payloads to "…teach students about imaging, radio communication and other spaceflight activities". Includes Amsat China's CAMSAT XW-4 payload for use by amateur radio operators with an Earth imaging system to collect and store pictures and then download them on demand. Released from a cubesat deployer on the outside of Tianzhou 5.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 20, 22:27	6763	0.0008	380	390	92.25	41.48	207

2022-F07 - failed to reach orbit Vega-C (VV-22) Centre Spatiale Guyanaise						2022 Dec 21, 01:47
Pléiades Neo 5
French digital imaging satellites with very high resolution sensors for use by commercial organisations, government and the Military. Lost when the launch vehicle second stage failed part-way through its firing.
Pléiades Neo 6
French digital imaging satellites with very high resolution sensors for use by commercial organisations, government and the Military. Lost when the launch vehicle second stage failed part-way through its firing.

2022-176 CZ 4B Taiyuan Space Centre						2022 Dec 27, 07:37
Gaofen 11-04 2022-176A 54818						in space
Chinese remote sensing imaging satellite operating at optical wavelengths. Initially operating in elliptical orbit with low perigee. Circularised orbit at 500 kilometres 2023 March.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2022 Dec 27, 18:41	6849	0.0329	246	696	94.01	97.27	189	14:46
2023 Feb 13, 13:07	6792	0.0261	237	592	92.85	97.27	16	14:48
2023 Mar 15, 05:23	6749	0.0209	230	512	91.97	97.27	265	14:53
2023 Mar 15, 09:50	6753	0.0204	237	513	92.04	97.27	263	14:53
2023 Mar 18, 08:29	6794	0.0200	280	552	92.89	97.20	270	14:53
2023 Mar 20, 04:42	6854	0.0212	331	622	94.13	97.09	243	14:52
2023 Mar 20, 15:49	6874	0.0001	495	496	94.53	97.27	232	14:53
CZ 4B third stage 2022-176B 54819						Re-entered - 2023 Feb 17 Life 52 days
Launched Gaofen 11-04. Apogee lowered after releasing satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 27, 21:25	6739	0.0181	239	483	91.77	97.23	175

2022-177 Falcon 9 Block 5 (Starlink Group 05-01) Cape Canaveral Space Force Station						2022 Dec 28, 09:34
Starlink 5382 2022-177A 54820						in space
One member of a simultaneously-launched cluster of fifty four LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Released from the launch vehicle at 09:52 UTC. All satellites were injected initially into similar orbits at about 330 km altitude.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 4, 16:00	6675	0.0026	280	315	90.46	43.00	211
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Dec 28 Life <1 day
Launched fifty four Starlink satellites. Caused to re-enter after releasing satellites.
Not Catalogued - orbit parameters unavailable

2022-178 CZ 3B Xichang Space Centre						2022 Dec 29, 04:43
Shiyan 10-02 (Test 10-02) 2022-178A 54878						in space
Satellite described as being for science/engineering tests but probably designed for electronic surveillance. Moved to 63° inclination orbit probably around 2023 January 1. Orbit maintained by periodic thruster firings.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 29, 19:08	26518	0.7525	185	40096	716.28	50.98	225
2023 Jan 27, 01:53	26557	0.6923	1794	38565	717.85	63.32	269
2023 Apr 20, 09:24	26552	0.6959	1695	38652	717.63	63.37	269
2023 Apr 24, 09:07	26559	0.6956	1708	38655	717.94	63.37	269
2023 Aug 2, 06:06	26552	0.7000	1587	38762	717.65	63.44	269
2023 Aug 12, 20:30	26559	0.7000	1589	38772	717.91	63.46	269
2023 Sep 26, 17:08	26552	0.7020	1533	38814	717.63	63.50	269
2023 Sep 27, 12:48	26560	0.7016	1547	38816	717.95	63.49	269
2024 Nov 17, 10:11	26558	0.7130	1245	39114	717.87	63.86	269
CZ 3B fourth stage 2022-178B 54879						Re-entered - 2023 Jun 30 Life 183 days
Launched Shiyan 10-02. Engine firing for HEO occurred near New Zealand at around 05:10 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 29, 20:01	26686	0.7520	240	40376	723.09	51.31	226

2022-I12 Nanoracks Cubesat Deployer International Space Station						2022 Dec 29, 12:05
DanteSat 1998-067UU 55127						Re-entered - 2023 Feb 7 Life 40 days
3U Cubesat from Italian company NPC Spacemind to act as a 'flag' for Dante Alighieri. It carries engravings of the script of his Divine Comedy. Fitted with a drag sail to create rapid orbit decay. The first orbit listed is an estimate - first actual data came through five days after release so it had already undergone significant decay because of the drag sail.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
estimated orbit	6793	0.0003	413	417	92.88	51.64	290
2023 Jan 3, 15:04	6782	0.0002	403	405	92.65	51.64	282
2023 Feb 7, 01:29	6522	0.0006	140	147	87.36	51.61	276
TJREVERB (Thomas Jefferson Research and Education Vehicle for Evaluating Radio Broadcasts) 1998-067UU 55128						Re-entered - 2023 Jun 13 Life 166 days
2U Cubesat from the Thomas Jefferson High School for Science and Technology, Virginia to study Iridium satellite transmissions at the height of the ISS orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 3, 15:48	6793	0.0005	411	418	92.86	51.64	249

2022-I13 Nanoracks Cubesat Deployer International Space Station						2022 Dec 29, 12:15
MARIO (Measurement of Actuator Response and Impedance on Orbit) 1998-067UQ 55123						Re-entered - 2023 May 4 Life 126 days
3U Cubesat from the University of Michigan to study and measure the behaviour and degradation of fibre materials when used as mechanical components.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 3, 15:12	6792	0.0003	412	416	92.84	51.64	274
NUTSat (2?) (National University of Taiwan Satellite) 1998-067UR 55124						Re-entered - 2023 Apr 4 Life 96 days
2U Cubesat - from Taiwan to demonstrate monitoring of ADS-B transmissions from aircraft in flight.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 4, 20:34	6791	0.0003	411	415	92.83	51.64	278

2022-I14 Nanoracks Cubesat Deployer International Space Station						2022 Dec 29, 13:45
LORIS (Low Orbit Reconnaissance Imagery Satellite) 1998-067US 55125						Re-entered - 2023 Jun 3 Life 156 days
2U Cubesat from Dalhousie Space Systems Lab of Canada. Designed to allow students to experience building and controlling a satellite. Equipped with an Earth imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 3, 15:12	6792	0.0004	411	417	92.85	51.64	269
ORCASat (Optical Reference Calibration Satellite) 1998-067UT 55126						Re-entered - 2023 Jul 11 Life 194 days
2U Cubesat - student-designed satellite built by the University of Victoria, Canada. Will act as a target equipped with lights to allow telescopes to be calibrated and determine differences between the true and observed brightness of celestial objects.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 3, 15:12	6792	0.0004	411	417	92.85	51.64	269

2022-I15 Nanoracks Cubesat Deployer International Space Station						2022 Dec 29, 13:55
SPORT (Scintillation Prediction Observations Research Task) 1998-067UW 55129						Re-entered - 2023 Oct 11 Life 286 days
6U Cubesat - NASA/Brazil co-operative mission to study electrons and plasma in the ionosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 3, 10:35	6793	0.0003	413	417	92.88	51.64	235
petitSat (Plasma Enhancements in the Ionosphere-Thermosphere Satellite) 1998-067UX 55130						Re-entered - 2023 Apr 10 Life 102 days
6U Cubesat - NASA mission to observe 'bubbles' of electrons and plasma in the Earth's ionosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2023 Jan 3, 14:20	6794	0.0004	413	418	92.88	51.65	221

2022-179 Falcon 9 Block 5 Vandenberg Space Force Base						2022 Dec 30, 07:38
Eros C-3 2022-179A 54880						in space
Israeli government/military Earth imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2022 Dec 30, 09:17	6872	0.0013	485	503	94.49	139.36	263
Falcon 9 upper stage uncatalogued						Re-entered - 2022 Dec 30 Life <1 day
Launched Eros C-3. Caused to re-enter after releasing satellite, probably mid-Pacific Ocean around 09:30 UTC.
Not Catalogued - orbit parameters unavailable