METEOR 2-1
Satellite information METEOR 2-1
| Spacetrack Directory Name | METEOR 2-1 |
| Follow METEOR 2-1 | METEOR 2-1 Tracker |
| Pass predictions METEOR 2-1 | Pass predictions METEOR 2-1 |
| Orbit launches |
1975-07-11 (51 years ago)
|
| Days in orbit | 18717 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Perigee | 842 km |
| Apogee | 875 km |
| Orbit slope (inclination) | 81.28° |
| Laps per day | 14 |
| Height METEOR 2-1 | 868.47 km |
Additional information METEOR 2-1
METEOR 2-1, 8026 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Fri, 11 Jul 1975 UTC via a VOSTOK 8A92M 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 2-1 Date of exalting 11.07.1975y. Average height of ISS METEOR 2-1 hundred 868.47 km. Average velocity METEOR 2-1 is 26710.99 km/h. Inclination METEOR 2-1 satellite 81.28°.TLE
Average velocity METEOR 2-1
Average inclination METEOR 2-1
Mean right ascension of the ascending node (RAAN) METEOR 2-1
Mean argument of perigee METEOR 2-1
Mean semi-major axis of the orbit METEOR 2-1
Mean orbital eccentricity METEOR 2-1
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