EKRAN 14
Satellite information EKRAN 14
| Spacetrack Directory Name | EKRAN 14 |
| Follow EKRAN 14 | EKRAN 14 Tracker |
| Pass predictions EKRAN 14 | Pass predictions EKRAN 14 |
| Orbit launches |
1985-03-22 (41 years ago)
|
| Days in orbit | 15163 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 37301 km |
| Apogee | 37489 km |
| Orbit slope (inclination) | 11.78° |
| Laps per day | 1 |
| Height EKRAN 14 | 37394.1 km |
Additional information EKRAN 14
EKRAN 14, 15626 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Fri, 22 Mar 1985 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 14 Date of exalting 22.03.1985y. Average height of ISS EKRAN 14 hundred 37394.1 km. Average velocity EKRAN 14 is 10863.85 km/h. Inclination EKRAN 14 satellite 11.82°.TLE
Average velocity EKRAN 14
Average inclination EKRAN 14
Mean right ascension of the ascending node (RAAN) EKRAN 14
Mean argument of perigee EKRAN 14
Mean semi-major axis of the orbit EKRAN 14
Mean orbital eccentricity EKRAN 14
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