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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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: 19 hours ago
TLE from 19 hours ago
0 COSMOS 2092
1 20737U 90070C 26135.08190755 .00000037 00000-0 14651-3 0 9997
2 20737 82.5680 327.0177 0004015 195.0749 288.2046 12.63349849649178Epoch: 2026-05-15T01:57Z
TLE epoch observation values (Epoch: 2026-05-15T01:57:56.812Z)
Latitude
56.12806°
Longitude
-126.43682°
Altitude
1,417.473 km
Speed
7.158 km/s
True Right ascension
09h 03m 28s
True Declination
55° 58' 56"
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
05:18:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,409.593 km
Perigee altitude
1,403.342 km
Semi-major axis
7,784.605 km
Eccentricity
0.0004
Inclination
82.568°
RAAN
327.0177°
Arg. of periapsis
195.0749°
True anomaly
288.16089°
Mean anomaly
288.2046°
Eccentric anomaly
288.18274°
Mean motion
3.16001 °/min
Orbital period
113.92 mins
BSTAR
0.00014651
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-05-15 22:50:24.230Z | 22.957° NE | 2026-05-15 22:55:24.230Z | 61.607° ENE | 18.297° | 2026-05-15 23:00:24.230Z | 102.117° ESE |
| 15 mins | 2026-05-16 00:44:24.230Z | 350.789° N | 2026-05-16 00:51:24.230Z | 301.95° NW | 44.763° | 2026-05-16 00:59:24.230Z | 178.059° S |
| 6 mins | 2026-05-16 02:42:24.230Z | 305.061° NW | 2026-05-16 02:45:24.230Z | 281.884° WNW | 14.243° | 2026-05-16 02:48:24.230Z | 259.115° W |
| 8 mins | 2026-05-16 11:41:24.230Z | 105.533° ESE | 2026-05-16 11:44:24.230Z | 81.04° E | 17.311° | 2026-05-16 11:49:24.230Z | 42.198° NE |
| 15 mins | 2026-05-16 13:31:24.230Z | 188.932° SSW | 2026-05-16 13:38:24.230Z | 266.746° W | 44.832° | 2026-05-16 13:46:24.230Z | 6.28° NNE |
| 8 mins | 2026-05-16 15:31:24.230Z | 271.924° WNW | 2026-05-16 15:34:24.230Z | 295.469° NW | 15.533° | 2026-05-16 15:39:24.230Z | 333.246° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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