EKRAN 21
Satellite information EKRAN 21
| Spacetrack Directory Name | EKRAN 21 |
| Follow EKRAN 21 | EKRAN 21 Tracker |
| Pass predictions EKRAN 21 | Pass predictions EKRAN 21 |
| Orbit launches |
2001-04-07 (25 years ago)
|
| Days in orbit | 9281 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35838 km |
| Apogee | 36118 km |
| Orbit slope (inclination) | 14.7° |
| Laps per day | 1 |
| Height EKRAN 21 | 35979.57 km |
Additional information EKRAN 21
EKRAN 21, 26736 is a payload satellite owned by GPKS (CIS) in GEO that was launched on Sat, 07 Apr 2001 UTC via a PROTON-M/BRIZ-M 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 21 Date of exalting 07.04.2001y. Average height of ISS EKRAN 21 hundred 35979.57 km. Average velocity EKRAN 21 is 11043.79 km/h. Inclination EKRAN 21 satellite 14.69°.TLE
Average velocity EKRAN 21
Average inclination EKRAN 21
Mean right ascension of the ascending node (RAAN) EKRAN 21
Mean argument of perigee EKRAN 21
Mean semi-major axis of the orbit EKRAN 21
Mean orbital eccentricity EKRAN 21
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