COSMOS 2082, 20624
Orbit data source: Space-Track
COSMOS 2082, 20624 is a payload satellite owned by GRU (CIS) in LEO that was launched on Tue, 22 May 1990 UTC via a ZENIT-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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20624 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Yuzhnoe
Mission
Defense Sigint
Bus & Motor
TSELINA-2, Unknown motor
Mass
3,250 kg wet, 3,250 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 9.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 COSMOS 2082
1 20624U 90046A 26165.74179521 -.00000269 00000-0 -11463-3 0 9996
2 20624 71.0384 177.3600 0012900 49.9582 310.2671 14.14843340861357Epoch: 2026-06-14T17:48Z
TLE epoch observation values (Epoch: 2026-06-14T17:48:11.106Z)
Latitude
0.00007°
Longitude
7.27557°
Altitude
839.233 km
Speed
7.437 km/s
True Right ascension
11h 49m 26s
True Declination
0° 00' 00"
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
14:02:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
850.079 km
Perigee altitude
831.454 km
Semi-major axis
7,218.903 km
Eccentricity
0.00129
Inclination
71.0384°
RAAN
177.36°
Arg. of periapsis
49.9582°
True anomaly
310.15419°
Mean anomaly
310.2671°
Eccentric anomaly
310.21066°
Mean motion
3.53864 °/min
Orbital period
101.73 mins
BSTAR
-0.00011463
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Other satellites on launch #46 in the year 1990 (1990-05-22 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 2082 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-15 11:20:34.780Z | 358.287° N | 2026-06-15 11:24:34.780Z | 75.816° E | 34.608° | 2026-06-15 11:28:34.780Z | 130.039° SE |
| 7 mins | 2026-06-15 13:04:34.780Z | 301.934° NW | 2026-06-15 13:07:34.780Z | 262.809° W | 22.428° | 2026-06-15 13:11:34.780Z | 210.911° SW |
| 9 mins | 2026-06-16 02:10:34.780Z | 207.381° SW | 2026-06-16 02:14:34.780Z | 272.253° WNW | 44.466° | 2026-06-16 02:19:34.780Z | 20.215° 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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