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: 18 hours ago
TLE from 18 hours ago
0 COSMOS 2212
1 22183U 92068B 25256.13447419 .00000019 00000-0 44058-4 0 9999
2 22183 82.5912 145.5398 0003466 76.0513 284.0964 12.63139753516602Epoch: 2025-09-13T03:13Z
TLE epoch observation values (Epoch: 2025-09-13T03:13:38.57Z)
Latitude
0.00001°
Longitude
104.7569°
Altitude
1,412.086 km
Speed
7.155 km/s
True Right ascension
09h 42m 09s
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
14:01:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.029 km
Perigee altitude
1,404.632 km
Semi-major axis
7,785.468 km
Eccentricity
0.00035
Inclination
82.5912°
RAAN
145.5398°
Arg. of periapsis
76.0513°
True anomaly
284.05787°
Mean anomaly
284.0964°
Eccentric anomaly
284.07714°
Mean motion
3.15948 °/min
Orbital period
113.94 mins
BSTAR
0.000044058
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-14 02:39:52.292Z | 27.392° NE | 2025-09-14 02:44:52.292Z | 66.579° ENE | 16.698° | 2025-09-14 02:48:52.292Z | 97.563° ESE |
| 15 mins | 2025-09-14 04:33:52.292Z | 352.802° N | 2025-09-14 04:40:52.292Z | 164.578° S | 44.898° | 2025-09-14 04:48:52.292Z | 174.491° S |
| 8 mins | 2025-09-14 06:30:52.292Z | 309.314° NW | 2025-09-14 06:33:52.292Z | 285.902° WNW | 15.865° | 2025-09-14 06:38:52.292Z | 247.907° W |
| 7 mins | 2025-09-14 15:30:52.292Z | 101.358° ESE | 2025-09-14 15:33:52.292Z | 77.482° E | 15.664° | 2025-09-14 15:37:52.292Z | 46.849° ENE |
| 15 mins | 2025-09-14 17:20:52.292Z | 185.162° SSW | 2025-09-14 17:27:52.292Z | 8.115° NNE | 44.863° | 2025-09-14 17:35:52.292Z | 7.826° NNE |
| 8 mins | 2025-09-14 19:19:52.292Z | 266.204° W | 2025-09-14 19:23:52.292Z | 298.649° NW | 16.94° | 2025-09-14 19:27:52.292Z | 330.19° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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