THOR BURNER 2A DEB
Satellite information THOR BURNER 2A DEB
| Spacetrack Directory Name | THOR BURNER 2A DEB |
| Follow THOR BURNER 2A DEB | THOR BURNER 2A DEB Tracker |
| Pass predictions THOR BURNER 2A DEB | Pass predictions THOR BURNER 2A DEB |
| Orbit launches |
1974-03-16 (52 years ago)
|
| Days in orbit | 19161 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 739 km |
| Apogee | 830 km |
| Orbit slope (inclination) | 99.06° |
| Laps per day | 14 |
| Height THOR BURNER 2A DEB | 769.32 km |
Additional information THOR BURNER 2A DEB
THOR BURNER 2A DEB, 28593 is space debris in SSO originally from a launch on Sat, 16 Mar 1974 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 BURNER 2A DEB Date of exalting 16.03.1974y. Average height of ISS THOR BURNER 2A DEB hundred 769.32 km. Average velocity THOR BURNER 2A DEB is 26895.77 km/h. Inclination THOR BURNER 2A DEB satellite 99.07°.TLE
Average velocity THOR BURNER 2A DEB
Average inclination THOR BURNER 2A DEB
Mean right ascension of the ascending node (RAAN) THOR BURNER 2A DEB
Mean argument of perigee THOR BURNER 2A DEB
Mean semi-major axis of the orbit THOR BURNER 2A DEB
Mean orbital eccentricity THOR BURNER 2A DEB
ISS
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