COSMOS 2252, 22687
Orbit data source: Space-Track
COSMOS 2252, 22687 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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22687 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: 15 hours ago
TLE from 15 hours ago
0 COSMOS 2252
1 22687U 93038A 25258.79539926 .00000041 00000-0 16513-3 0 9994
2 22687 82.5824 43.2879 0007325 235.1189 245.4148 12.63323343485875Epoch: 2025-09-15T19:05Z
TLE epoch observation values (Epoch: 2025-09-15T19:05:22.496Z)
Latitude
58.82621°
Longitude
-70.41519°
Altitude
1,421.539 km
Speed
7.154 km/s
True Right ascension
14h 03m 41s
True Declination
58° 41' 12"
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
02:38:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.279 km
Perigee altitude
1,400.874 km
Semi-major axis
7,784.713 km
Eccentricity
0.00073
Inclination
82.5824°
RAAN
43.2879°
Arg. of periapsis
235.1189°
True anomaly
245.3385°
Mean anomaly
245.4148°
Eccentric anomaly
245.37665°
Mean motion
3.15994 °/min
Orbital period
113.93 mins
BSTAR
0.00016513
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Other satellites on launch #38 in the year 1993 (1993-06-24 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 2252 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-09-16 11:41:55.887Z | 235.781° WSW | 2025-09-16 11:46:55.887Z | 283.594° WNW | 28.734° | 2025-09-16 11:53:55.887Z | 347.711° N |
| 9 mins | 2025-09-16 19:47:55.887Z | 29.686° NE | 2025-09-16 19:51:55.887Z | 62.48° ENE | 18.607° | 2025-09-16 19:56:55.887Z | 103.023° ESE |
| 15 mins | 2025-09-16 21:40:55.887Z | 350.483° N | 2025-09-16 21:47:55.887Z | 286.86° WNW | 44.756° | 2025-09-16 21:55:55.887Z | 178.654° S |
| 6 mins | 2025-09-16 23:38:55.887Z | 304.269° NW | 2025-09-16 23:41:55.887Z | 281.163° WNW | 13.992° | 2025-09-16 23:44:55.887Z | 258.704° W |
| 9 mins | 2025-09-17 08:36:55.887Z | 111.866° ESE | 2025-09-17 08:40:55.887Z | 80.102° E | 17.676° | 2025-09-17 08:45:55.887Z | 41.379° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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