EKRAN 4
Satellite information EKRAN 4
| Spacetrack Directory Name | EKRAN 4 |
| Follow EKRAN 4 | EKRAN 4 Tracker |
| Pass predictions EKRAN 4 | Pass predictions EKRAN 4 |
| Orbit launches |
1979-10-03 (47 years ago)
|
| Days in orbit | 17171 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35778 km |
| Apogee | 35803 km |
| Orbit slope (inclination) | 5.32° |
| Laps per day | 1 |
| Height EKRAN 4 | 35796.45 km |
Additional information EKRAN 4
EKRAN 4, 11561 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Wed, 03 Oct 1979 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 4 Date of exalting 03.10.1979y. Average height of ISS EKRAN 4 hundred 35796.45 km. Average velocity EKRAN 4 is 11067.63 km/h. Inclination EKRAN 4 satellite 5.39°.TLE
Average velocity EKRAN 4
Average inclination EKRAN 4
Mean right ascension of the ascending node (RAAN) EKRAN 4
Mean argument of perigee EKRAN 4
Mean semi-major axis of the orbit EKRAN 4
Mean orbital eccentricity EKRAN 4
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