THOR ALTAIR DEB
Satellite information THOR ALTAIR DEB
| Spacetrack Directory Name | THOR ALTAIR DEB |
| Follow THOR ALTAIR DEB | THOR ALTAIR DEB Tracker |
| Pass predictions THOR ALTAIR DEB | Pass predictions THOR ALTAIR DEB |
| Orbit launches |
1965-09-10 (60 years ago)
|
| Days in orbit | 22273 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 613 km |
| Apogee | 978 km |
| Orbit slope (inclination) | 99° |
| Laps per day | 14 |
| Height THOR ALTAIR DEB | 787.77 km |
Additional information THOR ALTAIR DEB
THOR ALTAIR DEB, 1931 is space debris in SSO originally from a launch on Fri, 10 Sep 1965 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite THOR ALTAIR DEB Date of exalting 10.09.1965y. Average height of ISS THOR ALTAIR DEB hundred 787.77 km. Average velocity THOR ALTAIR DEB is 26861.37 km/h. Inclination THOR ALTAIR DEB satellite 99°.TLE
Average velocity THOR ALTAIR DEB
Average inclination THOR ALTAIR DEB
Mean right ascension of the ascending node (RAAN) THOR ALTAIR DEB
Mean argument of perigee THOR ALTAIR DEB
Mean semi-major axis of the orbit THOR ALTAIR DEB
Mean orbital eccentricity THOR ALTAIR DEB
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