EKRAN 16
Satellite information EKRAN 16
| Spacetrack Directory Name | EKRAN 16 |
| Follow EKRAN 16 | EKRAN 16 Tracker |
| Pass predictions EKRAN 16 | Pass predictions EKRAN 16 |
| Orbit launches |
1987-09-03 (39 years ago)
|
| Days in orbit | 14264 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 36875 km |
| Apogee | 36891 km |
| Orbit slope (inclination) | 12.13° |
| Laps per day | 1 |
| Height EKRAN 16 | 36882.82 km |
Additional information EKRAN 16
EKRAN 16, 18328 is a payload satellite owned by MSvyaz (CIS) in GEO that was launched on Thu, 03 Sep 1987 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 16 Date of exalting 03.09.1987y. Average height of ISS EKRAN 16 hundred 36882.82 km. Average velocity EKRAN 16 is 10927.81 km/h. Inclination EKRAN 16 satellite 12.15°.TLE
Average velocity EKRAN 16
Average inclination EKRAN 16
Mean right ascension of the ascending node (RAAN) EKRAN 16
Mean argument of perigee EKRAN 16
Mean semi-major axis of the orbit EKRAN 16
Mean orbital eccentricity EKRAN 16
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