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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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Defense Communications
Bus & Motor
STRELA-3, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
1.257 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 COSMOS 2212
1 22183U 92068B 25310.86667417 .00000009 00000-0 -87723-5 0 9999
2 22183 82.5853 110.6081 0001857 330.9847 29.1141 12.63142501523510Epoch: 2025-11-06T20:48Z
TLE epoch observation values (Epoch: 2025-11-06T20:48:00.648Z)
Latitude
-0.00002°
Longitude
112.28656°
Altitude
1,411.468 km
Speed
7.155 km/s
True Right ascension
07h 22m 25s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:33:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,408.766 km
Perigee altitude
1,405.874 km
Semi-major axis
7,785.457 km
Eccentricity
0.00019
Inclination
82.5853°
RAAN
110.6081°
Arg. of periapsis
330.9847°
True anomaly
29.12446°
Mean anomaly
29.1141°
Eccentric anomaly
29.11928°
Mean motion
3.15949 °/min
Orbital period
113.94 mins
BSTAR
-0.0000087723
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Other satellites on launch #68 in the year 1992 (1992-10-20 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.COSMOS 2212 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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2025-11-07 12:05:41.773Z | 205.017° SW | 2025-11-07 12:13:41.773Z | 285.849° WNW | 39.856° | 2025-11-07 12:21:41.773Z | 359.899° N |
| 16 mins | 2025-11-07 22:06:41.773Z | 359.533° N | 2025-11-07 22:14:41.773Z | 78.534° E | 40.89° | 2025-11-07 22:22:41.773Z | 157.462° SSE |
| 11 mins | 2025-11-08 00:03:41.773Z | 324.006° NNW | 2025-11-08 00:08:41.773Z | 280.758° WNW | 24.579° | 2025-11-08 00:14:41.773Z | 228.408° WSW |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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