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: 14 hours ago
TLE from 14 hours ago
0 COSMOS 2092
1 20737U 90070C 25350.31323470 .00000007 00000-0 -18837-4 0 9992
2 20737 82.5694 62.8919 0004674 174.0262 253.8488 12.63344820630261Epoch: 2025-12-16T07:31Z
TLE epoch observation values (Epoch: 2025-12-16T07:31:03.478Z)
Latitude
66.749°
Longitude
-117.4911°
Altitude
1,421.7 km
Speed
7.156 km/s
True Right ascension
05h 21m 53s
True Declination
66° 38' 05"
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
19:47:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.127 km
Perigee altitude
1,402.85 km
Semi-major axis
7,784.626 km
Eccentricity
0.00047
Inclination
82.5694°
RAAN
62.8919°
Arg. of periapsis
174.0262°
True anomaly
253.79736°
Mean anomaly
253.8488°
Eccentric anomaly
253.82308°
Mean motion
3.16 °/min
Orbital period
113.92 mins
BSTAR
-0.000018837
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-17 04:11:35.595Z | 124.866° SE | 2025-12-17 04:16:35.595Z | 84.339° E | 21.538° | 2025-12-17 04:22:35.595Z | 35.442° NE |
| 14 mins | 2025-12-17 06:04:35.595Z | 199.402° SSW | 2025-12-17 06:10:35.595Z | 261.715° W | 42.842° | 2025-12-17 06:18:35.595Z | 2.164° NNE |
| 5 mins | 2025-12-17 08:05:35.595Z | 286.163° WNW | 2025-12-17 08:07:35.595Z | 300.998° NW | 12.153° | 2025-12-17 08:10:35.595Z | 322.824° NNW |
| 14 mins | 2025-12-17 16:05:35.595Z | 7.194° NNE | 2025-12-17 16:11:35.595Z | 67.439° ENE | 36.905° | 2025-12-17 16:19:35.595Z | 148.732° SSE |
| 13 mins | 2025-12-17 18:00:35.595Z | 330.059° NNW | 2025-12-17 18:06:35.595Z | 274.79° WNW | 29.008° | 2025-12-17 18:13:35.595Z | 215.425° SW |
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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