METEOR 2-20 DEB
Satellite information METEOR 2-20 DEB - 0 METEOR 2-20 DEB
| Spacetrack Directory Name | METEOR 2-20 DEB |
| Alternative name | 0 METEOR 2-20 DEB |
| Follow METEOR 2-20 DEB | METEOR 2-20 DEB Tracker |
| Pass predictions METEOR 2-20 DEB | Pass predictions METEOR 2-20 DEB |
| 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 | 919 km |
| Apogee | 940 km |
| Orbit slope (inclination) | 82.53° |
| Laps per day | 14 |
| Height METEOR 2-20 DEB | 941.24 km |
Additional information METEOR 2-20 DEB
METEOR 2-20 DEB, 59998 is space debris in LEO originally from a launch on Fri, 28 Sep 1990 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite METEOR 2-20 DEB Date of exalting 28.09.1990y. Average height of ISS METEOR 2-20 DEB hundred 941.24 km. Average velocity METEOR 2-20 DEB is 26577.82 km/h. Inclination METEOR 2-20 DEB satellite 82.53°.TLE
Average velocity METEOR 2-20 DEB
Average inclination METEOR 2-20 DEB
Mean right ascension of the ascending node (RAAN) METEOR 2-20 DEB
Mean argument of perigee METEOR 2-20 DEB
Mean semi-major axis of the orbit METEOR 2-20 DEB
Mean orbital eccentricity METEOR 2-20 DEB
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