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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Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 COSMOS 2215
1 22186U 92068E 25256.23966391 .00000045 00000-0 19266-3 0 9999
2 22186 82.6048 188.4546 0013843 82.4262 277.8400 12.60951539513961
TLE epoch observation values (Epoch: 2025-09-13T05:45:06.961Z)
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
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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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6 mins | 2025-09-14 05:15:00.203Z | 39.093° NE | 2025-09-14 05:18:00.203Z | 61.428° ENE | 12.698° | 2025-09-14 05:21:00.203Z | 83.336° E |
14 mins | 2025-09-14 07:08:00.203Z | 358.83° N | 2025-09-14 07:15:00.203Z | 105.419° ESE | 43.211° | 2025-09-14 07:22:00.203Z | 164.068° S |
10 mins | 2025-09-14 09:04:00.203Z | 319.002° NNW | 2025-09-14 09:09:00.203Z | 276.904° WNW | 20.712° | 2025-09-14 09:14:00.203Z | 236.862° WSW |
15 mins | 2025-09-14 19:56:00.203Z | 175.044° S | 2025-09-14 20:03:00.203Z | 87.772° E | 43.788° | 2025-09-14 20:11:00.203Z | 11.51° NNE |
11 mins | 2025-09-14 21:54:00.203Z | 252.453° W | 2025-09-14 21:59:00.203Z | 295.247° NW | 21.03° | 2025-09-14 22:05:00.203Z | 342.357° N |
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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