METEOR 2-14
Satellite information METEOR 2-14
| Spacetrack Directory Name | METEOR 2-14 |
| Follow METEOR 2-14 | METEOR 2-14 Tracker |
| Pass predictions METEOR 2-14 | Pass predictions METEOR 2-14 |
| Orbit launches |
1986-05-27 (40 years ago)
|
| Days in orbit | 14779 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Perigee | 933 km |
| Apogee | 957 km |
| Orbit slope (inclination) | 82.54° |
| Laps per day | 14 |
| Height METEOR 2-14 | 956.19 km |
Additional information METEOR 2-14
METEOR 2-14, 16735 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Tue, 27 May 1986 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 2-14 Date of exalting 27.05.1986y. Average height of ISS METEOR 2-14 hundred 956.19 km. Average velocity METEOR 2-14 is 26550.72 km/h. Inclination METEOR 2-14 satellite 82.54°.TLE
Average velocity METEOR 2-14
Average inclination METEOR 2-14
Mean right ascension of the ascending node (RAAN) METEOR 2-14
Mean argument of perigee METEOR 2-14
Mean semi-major axis of the orbit METEOR 2-14
Mean orbital eccentricity METEOR 2-14
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