COSMOS 2212, 22183
Orbit data source: Space-Track
COSMOS 2212, 22183 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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22183 intel report (Beta)
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TLE from 13 hours ago
0 COSMOS 2212
1 22183U 92068B 25199.42196688 .00000035 00000-0 13244-3 0 9996
2 22183 82.5887 181.7075 0001988 172.0252 188.0871 12.63137754509444
TLE epoch observation values (Epoch: 2025-07-18T10:07:37.938Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #68 in the year 1992 (1992-10-20 UTC)
COSMOS 2212 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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15 mins | 2025-07-18 23:31:25.572Z | 182.823° SSW | 2025-07-18 23:38:25.572Z | 150.424° SSE | 44.779° | 2025-07-18 23:46:25.572Z | 8.677° NNE |
9 mins | 2025-07-19 01:30:25.572Z | 260.829° W | 2025-07-19 01:34:25.572Z | 292.784° NW | 17.897° | 2025-07-19 01:39:25.572Z | 332.965° NNW |
13 mins | 2025-07-19 09:33:25.572Z | 13.634° NNE | 2025-07-19 09:39:25.572Z | 68.828° E | 29.54° | 2025-07-19 09:46:25.572Z | 132.575° SE |
14 mins | 2025-07-19 11:28:25.572Z | 337.435° NNW | 2025-07-19 11:34:25.572Z | 277.608° WNW | 36.757° | 2025-07-19 11:42:25.572Z | 200.495° SSW |
13 mins | 2025-07-19 22:21:25.572Z | 140.711° SSE | 2025-07-19 22:27:25.572Z | 85.361° E | 29.271° | 2025-07-19 22:34:25.572Z | 25.74° NE |
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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