COSMOS 2215, 22186
Orbit data source: Space-Track
COSMOS 2215, 22186 is a payload satellite owned by VKS (CIS) in LEO that was launched on Tue, 20 Oct 1992 UTC via a TSIKLON-3 launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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22186 intel report (Beta)
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TLE from 16 hours ago
0 COSMOS 2215
1 22186U 92068E 25199.50812235 .00000006 00000-0 -27449-4 0 9993
2 22186 82.5976 224.4462 0012018 205.9377 154.1112 12.60950732506817
TLE epoch observation values (Epoch: 2025-07-18T12:11:41.771Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #68 in the year 1992 (1992-10-20 UTC)
COSMOS 2215 Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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8 mins | 2025-07-19 11:41:44.364Z | 35.762° NE | 2025-07-19 11:44:44.364Z | 60.217° ENE | 17.217° | 2025-07-19 11:49:44.364Z | 99.71° ESE |
14 mins | 2025-07-19 13:34:44.364Z | 352.197° N | 2025-07-19 13:41:44.364Z | 185.502° SSW | 44.839° | 2025-07-19 13:48:44.364Z | 175.511° S |
8 mins | 2025-07-19 15:31:44.364Z | 309.838° NW | 2025-07-19 15:34:44.364Z | 286.908° WNW | 15.378° | 2025-07-19 15:39:44.364Z | 249.248° W |
8 mins | 2025-07-20 00:31:44.364Z | 108.943° ESE | 2025-07-20 00:35:44.364Z | 77.711° E | 16.736° | 2025-07-20 00:39:44.364Z | 46.637° ENE |
15 mins | 2025-07-20 02:22:44.364Z | 187.186° SSW | 2025-07-20 02:29:44.364Z | 304.615° NW | 44.944° | 2025-07-20 02:37:44.364Z | 6.979° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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