ASTRA 1E
Satellite information ASTRA 1E
| Spacetrack Directory Name | ASTRA 1E |
| Follow ASTRA 1E | ASTRA 1E Tracker |
| Pass predictions ASTRA 1E | Pass predictions ASTRA 1E |
| Orbit launches |
1995-10-19 (30 years ago)
|
| Days in orbit | 11288 |
| Country/organisation of origin | SES |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36167 km |
| Apogee | 36245 km |
| Orbit slope (inclination) | 11.69° |
| Laps per day | 1 |
| Height ASTRA 1E | 36206.61 km |
Additional information ASTRA 1E
ASTRA 1E, 23686 is a payload satellite owned by SES (LU) in GEO that was launched on Thu, 19 Oct 1995 UTC via an ARIANE 42L 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 ASTRA 1E Date of exalting 19.10.1995y. Average height of ISS ASTRA 1E hundred 36206.61 km. Average velocity ASTRA 1E is 11014.21 km/h. Inclination ASTRA 1E satellite 11.66°.TLE
Average velocity ASTRA 1E
Average inclination ASTRA 1E
Mean right ascension of the ascending node (RAAN) ASTRA 1E
Mean argument of perigee ASTRA 1E
Mean semi-major axis of the orbit ASTRA 1E
Mean orbital eccentricity ASTRA 1E
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