METEOR 2-3
Satellite information METEOR 2-3
| Spacetrack Directory Name | METEOR 2-3 |
| Follow METEOR 2-3 | METEOR 2-3 Tracker |
| Pass predictions METEOR 2-3 | Pass predictions METEOR 2-3 |
| Orbit launches |
1977-12-14 (48 years ago)
|
| Days in orbit | 17828 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Perigee | 841 km |
| Apogee | 875 km |
| Orbit slope (inclination) | 81.2° |
| Laps per day | 14 |
| Height METEOR 2-3 | 866.99 km |
Additional information METEOR 2-3
METEOR 2-3, 10514 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Wed, 14 Dec 1977 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 2-3 Date of exalting 14.12.1977y. Average height of ISS METEOR 2-3 hundred 866.99 km. Average velocity METEOR 2-3 is 26713.74 km/h. Inclination METEOR 2-3 satellite 81.21°.TLE
Average velocity METEOR 2-3
Average inclination METEOR 2-3
Mean right ascension of the ascending node (RAAN) METEOR 2-3
Mean argument of perigee METEOR 2-3
Mean semi-major axis of the orbit METEOR 2-3
Mean orbital eccentricity METEOR 2-3
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