COSMOS 2255, 22690
Orbit data source: Space-Track
COSMOS 2255, 22690 is a payload satellite owned by VKS (CIS) in LEO that was launched on Thu, 24 Jun 1993 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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22690 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 COSMOS 2255
1 22690U 93038D 25259.94498861 .00000022 00000-0 61370-4 0 9999
2 22690 82.5842 44.1610 0005139 237.5800 242.0994 12.63320101486725
TLE epoch observation values (Epoch: 2025-09-16T22:40:47.015Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #38 in the year 1993 (1993-06-24 UTC)
COSMOS 2255 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 | 2025-09-18 08:25:01.219Z | 105.139° ESE | 2025-09-18 08:29:01.219Z | 75.263° E | 14.355° | 2025-09-18 08:32:01.219Z | 52.489° ENE |
14 mins | 2025-09-18 10:16:01.219Z | 181.582° SSW | 2025-09-18 10:22:01.219Z | 144.815° SSE | 44.662° | 2025-09-18 10:30:01.219Z | 9.101° NNE |
9 mins | 2025-09-18 12:14:01.219Z | 260.184° W | 2025-09-18 12:18:01.219Z | 292.436° WNW | 18.328° | 2025-09-18 12:23:01.219Z | 332.993° NNW |
13 mins | 2025-09-18 20:17:01.219Z | 14.089° NNE | 2025-09-18 20:23:01.219Z | 69.063° E | 29.077° | 2025-09-18 20:30:01.219Z | 131.875° SE |
14 mins | 2025-09-18 22:12:01.219Z | 337.826° N | 2025-09-18 22:18:01.219Z | 277.241° WNW | 37.25° | 2025-09-18 22:26:01.219Z | 199.591° SSW |
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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