METEOR 2-17
Satellite information METEOR 2-17
| Spacetrack Directory Name | METEOR 2-17 |
| Follow METEOR 2-17 | METEOR 2-17 Tracker |
| Pass predictions METEOR 2-17 | Pass predictions METEOR 2-17 |
| Orbit launches |
1988-01-30 (38 years ago)
|
| Days in orbit | 14114 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Perigee | 933 km |
| Apogee | 956 km |
| Orbit slope (inclination) | 82.54° |
| Laps per day | 14 |
| Height METEOR 2-17 | 955.83 km |
Additional information METEOR 2-17
METEOR 2-17, 18820 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Sat, 30 Jan 1988 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 2-17 Date of exalting 30.01.1988y. Average height of ISS METEOR 2-17 hundred 955.83 km. Average velocity METEOR 2-17 is 26551.38 km/h. Inclination METEOR 2-17 satellite 82.54°.TLE
Average velocity METEOR 2-17
Average inclination METEOR 2-17
Mean right ascension of the ascending node (RAAN) METEOR 2-17
Mean argument of perigee METEOR 2-17
Mean semi-major axis of the orbit METEOR 2-17
Mean orbital eccentricity METEOR 2-17
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