METEOR 2-16
Satellite information METEOR 2-16
| Spacetrack Directory Name | METEOR 2-16 |
| Follow METEOR 2-16 | METEOR 2-16 Tracker |
| Pass predictions METEOR 2-16 | Pass predictions METEOR 2-16 |
| Orbit launches |
1987-08-18 (39 years ago)
|
| Days in orbit | 14280 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Perigee | 939 km |
| Apogee | 955 km |
| Orbit slope (inclination) | 82.56° |
| Laps per day | 14 |
| Height METEOR 2-16 | 958.34 km |
Additional information METEOR 2-16
METEOR 2-16, 18312 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Tue, 18 Aug 1987 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 2-16 Date of exalting 18.08.1987y. Average height of ISS METEOR 2-16 hundred 958.34 km. Average velocity METEOR 2-16 is 26546.81 km/h. Inclination METEOR 2-16 satellite 82.55°.TLE
Average velocity METEOR 2-16
Average inclination METEOR 2-16
Mean right ascension of the ascending node (RAAN) METEOR 2-16
Mean argument of perigee METEOR 2-16
Mean semi-major axis of the orbit METEOR 2-16
Mean orbital eccentricity METEOR 2-16
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