EKRAN 6
Satellite information EKRAN 6
| Spacetrack Directory Name | EKRAN 6 |
| Follow EKRAN 6 | EKRAN 6 Tracker |
| Pass predictions EKRAN 6 | Pass predictions EKRAN 6 |
| Orbit launches |
1980-12-26 (45 years ago)
|
| Days in orbit | 16752 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35752 km |
| Apogee | 35819 km |
| Orbit slope (inclination) | 5.91° |
| Laps per day | 1 |
| Height EKRAN 6 | 35773.62 km |
Additional information EKRAN 6
EKRAN 6, 12120 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Fri, 26 Dec 1980 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 6 Date of exalting 26.12.1980y. Average height of ISS EKRAN 6 hundred 35773.62 km. Average velocity EKRAN 6 is 11070.64 km/h. Inclination EKRAN 6 satellite 6.01°.TLE
Average velocity EKRAN 6
Average inclination EKRAN 6
Mean right ascension of the ascending node (RAAN) EKRAN 6
Mean argument of perigee EKRAN 6
Mean semi-major axis of the orbit EKRAN 6
Mean orbital eccentricity EKRAN 6
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