EKRAN 10
Satellite information EKRAN 10
| Spacetrack Directory Name | EKRAN 10 |
| Follow EKRAN 10 | EKRAN 10 Tracker |
| Pass predictions EKRAN 10 | Pass predictions EKRAN 10 |
| Orbit launches |
1983-03-12 (43 years ago)
|
| Days in orbit | 15907 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 37172 km |
| Apogee | 37475 km |
| Orbit slope (inclination) | 10.2° |
| Laps per day | 1 |
| Height EKRAN 10 | 37323.34 km |
Additional information EKRAN 10
EKRAN 10, 13878 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Sat, 12 Mar 1983 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 10 Date of exalting 12.03.1983y. Average height of ISS EKRAN 10 hundred 37323.34 km. Average velocity EKRAN 10 is 10872.54 km/h. Inclination EKRAN 10 satellite 10.25°.TLE
Average velocity EKRAN 10
Average inclination EKRAN 10
Mean right ascension of the ascending node (RAAN) EKRAN 10
Mean argument of perigee EKRAN 10
Mean semi-major axis of the orbit EKRAN 10
Mean orbital eccentricity EKRAN 10
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