SENTINEL 1A
Satellite information SENTINEL 1A
| Spacetrack Directory Name | SENTINEL 1A |
| Follow SENTINEL 1A | SENTINEL 1A Tracker |
| Pass predictions SENTINEL 1A | Pass predictions SENTINEL 1A |
| Orbit launches |
2014-04-03 (12 years ago)
|
| Days in orbit | 4528 |
| Country/organisation of origin | European Space Agency (ESA) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| WWW | Here |
| Categories | |
| Perigee | 695 km |
| Apogee | 697 km |
| Orbit slope (inclination) | 98.16° |
| Laps per day | 15 |
| Orbit | LEO (Sun-Synchronous) |
| Height SENTINEL 1A | 707.66 km |
Additional information SENTINEL 1A
SENTINEL 1A, 39634 is a payload satellite owned by ESA (ESA) in SSO that was launched on Thu, 03 Apr 2014 UTC via a SOYUZ-ST-A launch vehicle from the French Guiana (FRGUI). 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 SENTINEL 1A Date of exalting 03.04.2014y. Average height of ISS SENTINEL 1A hundred 707.66 km. Average velocity SENTINEL 1A is 27012.46 km/h. Inclination SENTINEL 1A satellite 98.18°.TLE
Average velocity SENTINEL 1A
Average inclination SENTINEL 1A
Mean right ascension of the ascending node (RAAN) SENTINEL 1A
Mean argument of perigee SENTINEL 1A
Mean semi-major axis of the orbit SENTINEL 1A
Mean orbital eccentricity SENTINEL 1A
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