COSMOS 2226, 22282
Orbit data source: Space-Track
COSMOS 2226, 22282 is a payload satellite owned by VTS VS Rossii (CIS) in LEO that was launched on Tue, 22 Dec 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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22282 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Defense Geodetic
Bus & Motor
KAUR-1 11F666, Unknown motor
Mass
1,536 kg wet, 1,536 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 2.9 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 COSMOS 2226
1 22282U 92092A 25265.55054687 .00000002 00000-0 13899-3 0 9993
2 22282 73.6211 104.2734 0029040 49.1751 13.2788 12.41298662483994Epoch: 2025-09-22T13:12Z
TLE epoch observation values (Epoch: 2025-09-22T13:12:47.249Z)
Latitude
58.44583°
Longitude
-67.13483°
Altitude
1,488.295 km
Speed
7.135 km/s
True Right ascension
08h 50m 51s
True Declination
58° 18' 24"
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
13:50:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,521.855 km
Perigee altitude
1,476.105 km
Semi-major axis
7,877.117 km
Eccentricity
0.0029
Inclination
73.6211°
RAAN
104.2734°
Arg. of periapsis
49.1751°
True anomaly
13.35551°
Mean anomaly
13.2788°
Eccentric anomaly
13.31713°
Mean motion
3.1045 °/min
Orbital period
115.96 mins
BSTAR
0.00013899
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Other satellites on launch #92 in the year 1992 (1992-12-22 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 2226 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-09-22 23:07:45.609Z | 359.754° N | 2025-09-22 23:14:45.609Z | 56.772° ENE | 25.845° | 2025-09-22 23:21:45.609Z | 111.104° ESE |
| 15 mins | 2025-09-23 01:06:45.609Z | 333.358° NNW | 2025-09-23 01:13:45.609Z | 254.527° W | 42.799° | 2025-09-23 01:21:45.609Z | 176.343° S |
| 16 mins | 2025-09-23 14:06:45.609Z | 183.526° SSW | 2025-09-23 14:14:45.609Z | 88.746° E | 42.684° | 2025-09-23 14:22:45.609Z | 24.748° NE |
| 13 mins | 2025-09-23 16:07:45.609Z | 255.847° W | 2025-09-23 16:13:45.609Z | 308.065° NW | 25.477° | 2025-09-23 16:20:45.609Z | 2.24° NNE |
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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