S80/T
Satellite information S80/T
| Spacetrack Directory Name | S80/T |
| Follow S80/T | S80/T Tracker |
| Pass predictions S80/T | Pass predictions S80/T |
| Orbit launches |
1992-08-10 (34 years ago)
|
| Days in orbit | 12506 |
| Country/organisation of origin | Francja (FR) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 1309 km |
| Apogee | 1320 km |
| Orbit slope (inclination) | 66.09° |
| Laps per day | 13 |
| Height S80/T | 1323.72 km |
Additional information S80/T
S80/T, 22078 is a payload satellite owned by CNES (FR) in LEO that was launched on Mon, 10 Aug 1992 UTC via an ARIANE 42P 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 S80/T Date of exalting 10.08.1992y. Average height of ISS S80/T hundred 1323.72 km. Average velocity S80/T is 25909.85 km/h. Inclination S80/T satellite 66.09°.TLE
Average velocity S80/T
Average inclination S80/T
Mean right ascension of the ascending node (RAAN) S80/T
Mean argument of perigee S80/T
Mean semi-major axis of the orbit S80/T
Mean orbital eccentricity S80/T
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