HELLAS-SAT 1 (DFS 3)
Satellite information HELLAS-SAT 1 (DFS 3)
| Spacetrack Directory Name | HELLAS-SAT 1 (DFS 3) |
| Follow HELLAS-SAT 1 (DFS 3) | HELLAS-SAT 1 (DFS 3) Tracker |
| Pass predictions HELLAS-SAT 1 (DFS 3) | Pass predictions HELLAS-SAT 1 (DFS 3) |
| Orbit launches |
1992-10-12 (33 years ago)
|
| Days in orbit | 12384 |
| Country/organisation of origin | Grecja (GREC) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35925 km |
| Apogee | 35953 km |
| Orbit slope (inclination) | 14.29° |
| Laps per day | 1 |
| Height HELLAS-SAT 1 (DFS 3) | 35939.25 km |
Additional information HELLAS-SAT 1 (DFS 3)
HELLAS-SAT 1 (DFS 3), 22175 is a payload satellite owned by Bundespost (GR) in GEO that was launched on Mon, 12 Oct 1992 UTC via a DELTA 7925 launch vehicle from the Air Force Eastern Test Range (AFETR). 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 HELLAS-SAT 1 (DFS 3) Date of exalting 12.10.1992y. Average height of ISS HELLAS-SAT 1 (DFS 3) hundred 35939.25 km. Average velocity HELLAS-SAT 1 (DFS 3) is 11048.99 km/h. Inclination HELLAS-SAT 1 (DFS 3) satellite 14.28°.TLE
Average velocity HELLAS-SAT 1 (DFS 3)
Average inclination HELLAS-SAT 1 (DFS 3)
Mean right ascension of the ascending node (RAAN) HELLAS-SAT 1 (DFS 3)
Mean argument of perigee HELLAS-SAT 1 (DFS 3)
Mean semi-major axis of the orbit HELLAS-SAT 1 (DFS 3)
Mean orbital eccentricity HELLAS-SAT 1 (DFS 3)
ISS
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