EKRAN 1
Satellite information EKRAN 1
| Spacetrack Directory Name | EKRAN 1 |
| Follow EKRAN 1 | EKRAN 1 Tracker |
| Pass predictions EKRAN 1 | Pass predictions EKRAN 1 |
| Orbit launches |
1976-10-26 (49 years ago)
|
| Days in orbit | 18247 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35501 km |
| Apogee | 36047 km |
| Orbit slope (inclination) | 3.28° |
| Laps per day | 1 |
| Height EKRAN 1 | 35798.15 km |
Additional information EKRAN 1
EKRAN 1, 9503 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Tue, 26 Oct 1976 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 1 Date of exalting 26.10.1976y. Average height of ISS EKRAN 1 hundred 35798.15 km. Average velocity EKRAN 1 is 11067.4 km/h. Inclination EKRAN 1 satellite 3.35°.TLE
Average velocity EKRAN 1
Average inclination EKRAN 1
Mean right ascension of the ascending node (RAAN) EKRAN 1
Mean argument of perigee EKRAN 1
Mean semi-major axis of the orbit EKRAN 1
Mean orbital eccentricity EKRAN 1
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