EKRAN 3
Satellite information EKRAN 3
| Spacetrack Directory Name | EKRAN 3 |
| Follow EKRAN 3 | EKRAN 3 Tracker |
| Pass predictions EKRAN 3 | Pass predictions EKRAN 3 |
| Orbit launches |
1979-02-21 (47 years ago)
|
| Days in orbit | 17396 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35636 km |
| Apogee | 35968 km |
| Orbit slope (inclination) | 4.84° |
| Laps per day | 1 |
| Height EKRAN 3 | 35779.39 km |
Additional information EKRAN 3
EKRAN 3, 11273 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Wed, 21 Feb 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 3 Date of exalting 21.02.1979y. Average height of ISS EKRAN 3 hundred 35779.39 km. Average velocity EKRAN 3 is 11069.84 km/h. Inclination EKRAN 3 satellite 4.91°.TLE
Average velocity EKRAN 3
Average inclination EKRAN 3
Mean right ascension of the ascending node (RAAN) EKRAN 3
Mean argument of perigee EKRAN 3
Mean semi-major axis of the orbit EKRAN 3
Mean orbital eccentricity EKRAN 3
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