EKRAN 20
Satellite information EKRAN 20
| Spacetrack Directory Name | EKRAN 20 |
| Follow EKRAN 20 | EKRAN 20 Tracker |
| Pass predictions EKRAN 20 | Pass predictions EKRAN 20 |
| Orbit launches |
1992-10-30 (33 years ago)
|
| Days in orbit | 12377 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35786 km |
| Apogee | 35807 km |
| Orbit slope (inclination) | 13.63° |
| Laps per day | 1 |
| Height EKRAN 20 | 35771.37 km |
Additional information EKRAN 20
EKRAN 20, 22210 is a payload satellite owned by GPKS (CIS) in GEO that was launched on Fri, 30 Oct 1992 UTC via a PROTON-K/DM-2 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 20 Date of exalting 30.10.1992y. Average height of ISS EKRAN 20 hundred 35771.37 km. Average velocity EKRAN 20 is 11070.96 km/h. Inclination EKRAN 20 satellite 13.65°.TLE
Average velocity EKRAN 20
Average inclination EKRAN 20
Mean right ascension of the ascending node (RAAN) EKRAN 20
Mean argument of perigee EKRAN 20
Mean semi-major axis of the orbit EKRAN 20
Mean orbital eccentricity EKRAN 20
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