EKRAN 2
Satellite information EKRAN 2
| Spacetrack Directory Name | EKRAN 2 |
| Follow EKRAN 2 | EKRAN 2 Tracker |
| Pass predictions EKRAN 2 | Pass predictions EKRAN 2 |
| Orbit launches |
1977-09-20 (49 years ago)
|
| Days in orbit | 17917 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35609 km |
| Apogee | 35953 km |
| Orbit slope (inclination) | 3.95° |
| Laps per day | 1 |
| Height EKRAN 2 | 35801.82 km |
Additional information EKRAN 2
EKRAN 2, 10365 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Tue, 20 Sep 1977 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 2 Date of exalting 20.09.1977y. Average height of ISS EKRAN 2 hundred 35801.82 km. Average velocity EKRAN 2 is 11066.91 km/h. Inclination EKRAN 2 satellite 4.02°.TLE
Average velocity EKRAN 2
Average inclination EKRAN 2
Mean right ascension of the ascending node (RAAN) EKRAN 2
Mean argument of perigee EKRAN 2
Mean semi-major axis of the orbit EKRAN 2
Mean orbital eccentricity EKRAN 2
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