METEOR 1-26
Satellite information METEOR 1-26
| Spacetrack Directory Name | METEOR 1-26 |
| Follow METEOR 1-26 | METEOR 1-26 Tracker |
| Pass predictions METEOR 1-26 | Pass predictions METEOR 1-26 |
| Orbit launches |
1976-10-15 (49 years ago)
|
| Days in orbit | 18254 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | PLMSC (Plesetsk Missile and Space Complex, Russia) |
| Perigee | 843 km |
| Apogee | 877 km |
| Orbit slope (inclination) | 81.22° |
| Laps per day | 14 |
| Height METEOR 1-26 | 870.02 km |
Additional information METEOR 1-26
METEOR 1-26, 9481 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Fri, 15 Oct 1976 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 1-26 Date of exalting 15.10.1976y. Average height of ISS METEOR 1-26 hundred 870.02 km. Average velocity METEOR 1-26 is 26708.13 km/h. Inclination METEOR 1-26 satellite 81.22°.TLE
Average velocity METEOR 1-26
Average inclination METEOR 1-26
Mean right ascension of the ascending node (RAAN) METEOR 1-26
Mean argument of perigee METEOR 1-26
Mean semi-major axis of the orbit METEOR 1-26
Mean orbital eccentricity METEOR 1-26
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