COSMOS 2092, 20737
Orbit data source: Space-Track
COSMOS 2092, 20737 is a payload satellite owned by UNKS (CIS) in LEO that was launched on Wed, 08 Aug 1990 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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20737 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 COSMOS 2092
1 20737U 90070C 25319.76350522 .00000027 00000-0 91415-4 0 9998
2 20737 82.5677 82.4469 0003573 248.9712 266.8529 12.63343765626406Epoch: 2025-11-15T18:19Z
TLE epoch observation values (Epoch: 2025-11-15T18:19:26.851Z)
Latitude
24.02229°
Longitude
-70.8196°
Altitude
1,412.086 km
Speed
7.156 km/s
True Right ascension
17h 16m 31s
True Declination
23° 54' 19"
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
14:10:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,409.274 km
Perigee altitude
1,403.711 km
Semi-major axis
7,784.63 km
Eccentricity
0.00036
Inclination
82.5677°
RAAN
82.4469°
Arg. of periapsis
248.9712°
True anomaly
266.81202°
Mean anomaly
266.8529°
Eccentric anomaly
266.83246°
Mean motion
3.15999 °/min
Orbital period
113.92 mins
BSTAR
0.000091415
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Other satellites on launch #70 in the year 1990 (1990-08-08 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 2092 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-11-16 18:49:28.640Z | 15.503° NNE | 2025-11-16 18:55:28.640Z | 67.048° ENE | 25.997° | 2025-11-16 19:02:28.640Z | 126.466° SE |
| 14 mins | 2025-11-16 20:44:28.640Z | 341.548° N | 2025-11-16 20:51:28.640Z | 256.715° W | 39.997° | 2025-11-16 20:58:28.640Z | 194.436° SSW |
| 11 mins | 2025-11-17 07:38:28.640Z | 130.271° SE | 2025-11-17 07:43:28.640Z | 85.547° E | 25.425° | 2025-11-17 07:49:28.640Z | 33.024° NE |
| 14 mins | 2025-11-17 09:31:28.640Z | 207.353° SW | 2025-11-17 09:38:28.640Z | 294.549° NW | 40.027° | 2025-11-17 09:45:28.640Z | 358.733° N |
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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