METEOR 2-20
Satellite information METEOR 2-20
| Spacetrack Directory Name | METEOR 2-20 |
| Follow METEOR 2-20 | METEOR 2-20 Tracker |
| Pass predictions METEOR 2-20 | Pass predictions METEOR 2-20 |
| Orbit launches |
1990-09-28 (35 years ago)
|
| Days in orbit | 13141 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Perigee | 940 km |
| Apogee | 958 km |
| Orbit slope (inclination) | 82.52° |
| Laps per day | 14 |
| Height METEOR 2-20 | 960.05 km |
Additional information METEOR 2-20
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). Payloads include a variety of satellites, spacecraft, and rockets 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.
satellite METEOR 2-20 Date of exalting 28.09.1990y. Average height of ISS METEOR 2-20 hundred 960.05 km. Average velocity METEOR 2-20 is 26543.71 km/h. Inclination METEOR 2-20 satellite 82.53°.TLE
Average velocity METEOR 2-20
Average inclination METEOR 2-20
Mean right ascension of the ascending node (RAAN) METEOR 2-20
Mean argument of perigee METEOR 2-20
Mean semi-major axis of the orbit METEOR 2-20
Mean orbital eccentricity METEOR 2-20
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