EKRAN 17
Satellite information EKRAN 17 - Ekran-M
| Spacetrack Directory Name | EKRAN 17 |
| Alternative name | Ekran-M |
| Follow EKRAN 17 | EKRAN 17 Tracker |
| Pass predictions EKRAN 17 | Pass predictions EKRAN 17 |
| Orbit launches |
1987-12-27 (38 years ago)
|
| Days in orbit | 14148 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Type | Satellite |
| Perigee | 36897 km |
| Apogee | 37231 km |
| Orbit slope (inclination) | 13.38° |
| Laps per day | 1 |
| Height EKRAN 17 | 37063.86 km |
Additional information EKRAN 17
EKRAN 17, 18715 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Sun, 27 Dec 1987 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 17 Date of exalting 27.12.1987y. Average height of ISS EKRAN 17 hundred 37063.86 km. Average velocity EKRAN 17 is 10905.07 km/h. Inclination EKRAN 17 satellite 13.4°.TLE
Average velocity EKRAN 17
Average inclination EKRAN 17
Mean right ascension of the ascending node (RAAN) EKRAN 17
Mean argument of perigee EKRAN 17
Mean semi-major axis of the orbit EKRAN 17
Mean orbital eccentricity EKRAN 17
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