EKRAN 8
Satellite information EKRAN 8
| Spacetrack Directory Name | EKRAN 8 |
| Follow EKRAN 8 | EKRAN 8 Tracker |
| Pass predictions EKRAN 8 | Pass predictions EKRAN 8 |
| Orbit launches |
1982-02-05 (44 years ago)
|
| Days in orbit | 16311 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35764 km |
| Apogee | 35990 km |
| Orbit slope (inclination) | 6.82° |
| Laps per day | 1 |
| Height EKRAN 8 | 35878 km |
Additional information EKRAN 8
EKRAN 8, 13056 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Fri, 05 Feb 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 8 Date of exalting 05.02.1982y. Average height of ISS EKRAN 8 hundred 35878 km. Average velocity EKRAN 8 is 11056.96 km/h. Inclination EKRAN 8 satellite 6.88°.TLE
Average velocity EKRAN 8
Average inclination EKRAN 8
Mean right ascension of the ascending node (RAAN) EKRAN 8
Mean argument of perigee EKRAN 8
Mean semi-major axis of the orbit EKRAN 8
Mean orbital eccentricity EKRAN 8
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