EKRAN 12
Satellite information EKRAN 12
| Spacetrack Directory Name | EKRAN 12 |
| Follow EKRAN 12 | EKRAN 12 Tracker |
| Pass predictions EKRAN 12 | Pass predictions EKRAN 12 |
| Orbit launches |
1984-03-16 (42 years ago)
|
| Days in orbit | 15535 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 36976 km |
| Apogee | 37043 km |
| Orbit slope (inclination) | 10.11° |
| Laps per day | 1 |
| Height EKRAN 12 | 37009.45 km |
Additional information EKRAN 12
EKRAN 12, 14821 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Fri, 16 Mar 1984 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 12 Date of exalting 16.03.1984y. Average height of ISS EKRAN 12 hundred 37009.45 km. Average velocity EKRAN 12 is 10911.82 km/h. Inclination EKRAN 12 satellite 10.15°.TLE
Average velocity EKRAN 12
Average inclination EKRAN 12
Mean right ascension of the ascending node (RAAN) EKRAN 12
Mean argument of perigee EKRAN 12
Mean semi-major axis of the orbit EKRAN 12
Mean orbital eccentricity EKRAN 12
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