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METEOR 2-20, 20826

Orbit data source: Space-Track

METEOR 2-20, 20826 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Fri, 28 Sep 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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Identifier
20826, 1990-086A
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
VNIIEM
Mission
Civil Weather
Bus & Motor
METEOR-2, Unknown motor
Mass
~1,500 kg wet, ~1,500 kg dry
Launch date (UTC)
1990-09-28 (36 years ago)
Launch vehicle
TSIKLON-3
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Pan, 2.3 m
Radar Cross Section
5.718 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 METEOR 2-20
1 20826U 90086A   26171.40677343  .00000027  00000-0  10902-4 0  9997
2 20826  82.5235 195.0334 0013788  22.6853 337.4914 13.84460334804765
Epoch: 2026-06-20T09:45Z
TLE epoch observation values (Epoch: 2026-06-20T09:45:45.224Z)
Latitude
0.00001°
Longitude
139.97312°
Altitude
941.679 km
Speed
7.386 km/s
True Right ascension
13h 00m 08s
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
00:28:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.359 km
Perigee altitude
935.164 km
Semi-major axis
7,323.398 km
Eccentricity
0.00138
Inclination
82.5235°
RAAN
195.0334°
Arg. of periapsis
22.6853°
True anomaly
337.43082°
Mean anomaly
337.4914°
Eccentric anomaly
337.46112°
Mean motion
3.46317 °/min
Orbital period
103.95 mins
BSTAR
0.000010902
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