EUTE 16C (SESAT 1)
Satellite information EUTE 16C (SESAT 1) - SESAT, SESAT 1
| Spacetrack Directory Name | EUTE 16C (SESAT 1) |
| Alternative name | SESAT, SESAT 1 |
| Follow EUTE 16C (SESAT 1) | EUTE 16C (SESAT 1) Tracker |
| Pass predictions EUTE 16C (SESAT 1) | Pass predictions EUTE 16C (SESAT 1) |
| Orbit launches |
2000-04-17 (26 years ago)
|
| Days in orbit | 9636 |
| Country/organisation of origin | European Telecommunications Satellite Organization (EUTELSAT) (EUTE) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| WWW | Here |
| Perigee | 36150 km |
| Apogee | 36170 km |
| Orbit slope (inclination) | 11.05° |
| Laps per day | 1 |
| Height EUTE 16C (SESAT 1) | 36159.67 km |
Additional information EUTE 16C (SESAT 1)
EUTE 16C (SESAT 1), 26243 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Mon, 17 Apr 2000 UTC via a PROTON-K/DM-2M 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 EUTE 16C (SESAT 1) Date of exalting 17.04.2000y. Average height of ISS EUTE 16C (SESAT 1) hundred 36159.67 km. Average velocity EUTE 16C (SESAT 1) is 11020.29 km/h. Inclination EUTE 16C (SESAT 1) satellite 11.02°.TLE
Average velocity EUTE 16C (SESAT 1)
Average inclination EUTE 16C (SESAT 1)
Mean right ascension of the ascending node (RAAN) EUTE 16C (SESAT 1)
Mean argument of perigee EUTE 16C (SESAT 1)
Mean semi-major axis of the orbit EUTE 16C (SESAT 1)
Mean orbital eccentricity EUTE 16C (SESAT 1)
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