COSMOS 2167, 21781
Orbit data source: Space-Track
COSMOS 2167, 21781 is a payload satellite owned by UNKS RF (CIS) in LEO that was launched on Tue, 12 Nov 1991 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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21781 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 2167
1 21781U 91077C 25258.97307633 .00000042 00000-0 16858-3 0 9990
2 21781 82.6031 55.6988 0006630 353.0903 125.0261 12.64281567561292
TLE epoch observation values (Epoch: 2025-09-15T23:21:13.794Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #77 in the year 1991 (1991-11-12 UTC)
COSMOS 2167 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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7 mins | 2025-09-16 20:15:18.677Z | 32.974° NE | 2025-09-16 20:19:18.677Z | 62.481° ENE | 13.156° | 2025-09-16 20:22:18.677Z | 84.609° E |
15 mins | 2025-09-16 22:08:18.677Z | 357.334° N | 2025-09-16 22:15:18.677Z | 76.976° E | 43.797° | 2025-09-16 22:23:18.677Z | 165.716° S |
9 mins | 2025-09-17 00:05:18.677Z | 313.896° NW | 2025-09-17 00:09:18.677Z | 279.479° WNW | 20.201° | 2025-09-17 00:14:18.677Z | 238.92° WSW |
14 mins | 2025-09-17 10:55:18.677Z | 174.322° S | 2025-09-17 11:01:18.677Z | 113.136° SE | 43.618° | 2025-09-17 11:09:18.677Z | 11.868° NNE |
11 mins | 2025-09-17 12:52:18.677Z | 251.379° W | 2025-09-17 12:57:18.677Z | 293.833° NW | 21.062° | 2025-09-17 13:03:18.677Z | 341.714° 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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