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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Edit Public Description
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: 12 hours ago
TLE from 12 hours ago
0 COSMOS 2082
1 20624U 90046A 25300.46768976 .00000419 00000-0 24160-3 0 9996
2 20624 71.0393 299.8143 0013266 40.9666 319.2451 14.14798043828783Epoch: 2025-10-27T11:13Z
TLE epoch observation values (Epoch: 2025-10-27T11:13:28.395Z)
Latitude
0°
Longitude
95.37688°
Altitude
838.15 km
Speed
7.438 km/s
True Right ascension
19h 59m 15s
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
18:25:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
850.497 km
Perigee altitude
831.344 km
Semi-major axis
7,219.057 km
Eccentricity
0.00133
Inclination
71.0393°
RAAN
299.8143°
Arg. of periapsis
40.9666°
True anomaly
319.14573°
Mean anomaly
319.2451°
Eccentric anomaly
319.19543°
Mean motion
3.53853 °/min
Orbital period
101.74 mins
BSTAR
0.0002416
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-28 00:54:43.884Z | 174.849° S | 2025-10-28 00:59:43.884Z | 94.578° ESE | 34.812° | 2025-10-28 01:03:43.884Z | 39.21° NE |
| 7 mins | 2025-10-28 02:40:43.884Z | 262.68° W | 2025-10-28 02:43:43.884Z | 306.821° NW | 23.514° | 2025-10-28 02:47:43.884Z | 357.066° N |
| 6 mins | 2025-10-28 09:50:43.884Z | 17.21° NNE | 2025-10-28 09:53:43.884Z | 56.555° ENE | 19.465° | 2025-10-28 09:56:43.884Z | 93.416° ESE |
| 9 mins | 2025-10-28 11:33:43.884Z | 326.362° NNW | 2025-10-28 11:37:43.884Z | 263.641° W | 40.663° | 2025-10-28 11:42:43.884Z | 174.722° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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