METEOR 2-6
Satellite information METEOR 2-6
| Spacetrack Directory Name | METEOR 2-6 |
| Follow METEOR 2-6 | METEOR 2-6 Tracker |
| Pass predictions METEOR 2-6 | Pass predictions METEOR 2-6 |
| Orbit launches |
1980-09-09 (46 years ago)
|
| Days in orbit | 16827 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Perigee | 831 km |
| Apogee | 884 km |
| Orbit slope (inclination) | 81.23° |
| Laps per day | 14 |
| Height METEOR 2-6 | 867.34 km |
Additional information METEOR 2-6
METEOR 2-6, 11962 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Tue, 09 Sep 1980 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 2-6 Date of exalting 09.09.1980y. Average height of ISS METEOR 2-6 hundred 867.34 km. Average velocity METEOR 2-6 is 26713.08 km/h. Inclination METEOR 2-6 satellite 81.22°.TLE
Average velocity METEOR 2-6
Average inclination METEOR 2-6
Mean right ascension of the ascending node (RAAN) METEOR 2-6
Mean argument of perigee METEOR 2-6
Mean semi-major axis of the orbit METEOR 2-6
Mean orbital eccentricity METEOR 2-6
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