EKRAN 9
Satellite information EKRAN 9
| Spacetrack Directory Name | EKRAN 9 |
| Follow EKRAN 9 | EKRAN 9 Tracker |
| Pass predictions EKRAN 9 | Pass predictions EKRAN 9 |
| Orbit launches |
1982-09-16 (44 years ago)
|
| Days in orbit | 16086 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35659 km |
| Apogee | 35880 km |
| Orbit slope (inclination) | 6.86° |
| Laps per day | 1 |
| Height EKRAN 9 | 35804.86 km |
Additional information EKRAN 9
EKRAN 9, 13554 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Thu, 16 Sep 1982 UTC via a PROTON-K/DM launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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 EKRAN 9 Date of exalting 16.09.1982y. Average height of ISS EKRAN 9 hundred 35804.86 km. Average velocity EKRAN 9 is 11066.54 km/h. Inclination EKRAN 9 satellite 6.91°.TLE
Average velocity EKRAN 9
Average inclination EKRAN 9
Mean right ascension of the ascending node (RAAN) EKRAN 9
Mean argument of perigee EKRAN 9
Mean semi-major axis of the orbit EKRAN 9
Mean orbital eccentricity EKRAN 9
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