METEOR 3-3
Satellite information METEOR 3-3
| Spacetrack Directory Name | METEOR 3-3 |
| Follow METEOR 3-3 | METEOR 3-3 Tracker |
| Pass predictions METEOR 3-3 | Pass predictions METEOR 3-3 |
| Orbit launches |
1989-10-24 (36 years ago)
|
| Days in orbit | 13480 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| WWW | Here |
| Perigee | 1238 km |
| Apogee | 1250 km |
| Orbit slope (inclination) | 82.55° |
| Laps per day | 13 |
| Height METEOR 3-3 | 1255.63 km |
Additional information METEOR 3-3
METEOR 3-3, 20305 is a payload satellite owned by GMS (CIS) in LEO that was launched on Tue, 24 Oct 1989 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 3-3 Date of exalting 24.10.1989y. Average height of ISS METEOR 3-3 hundred 1255.63 km. Average velocity METEOR 3-3 is 26024.6 km/h. Inclination METEOR 3-3 satellite 82.55°.TLE
Average velocity METEOR 3-3
Average inclination METEOR 3-3
Mean right ascension of the ascending node (RAAN) METEOR 3-3
Mean argument of perigee METEOR 3-3
Mean semi-major axis of the orbit METEOR 3-3
Mean orbital eccentricity METEOR 3-3
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