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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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Identifier
20624, 1990-046A
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Yuzhnoe
Mission
Defense Sigint
Bus & Motor
TSELINA-2, Unknown motor
Mass
3,250 kg wet, 3,250 kg dry
Launch date (UTC)
1990-05-22 (36 years ago)
Launch vehicle
ZENIT-2
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 9.5 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last 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 14.14843340861357
Epoch: 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
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
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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