THOR BURNER 2 R/B
Satellite information THOR BURNER 2 R/B
| Spacetrack Directory Name | THOR BURNER 2 R/B |
| Follow THOR BURNER 2 R/B | THOR BURNER 2 R/B Tracker |
| Pass predictions THOR BURNER 2 R/B | Pass predictions THOR BURNER 2 R/B |
| Orbit launches |
1969-07-23 (57 years ago)
|
| Days in orbit | 20861 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 759 km |
| Apogee | 818 km |
| Orbit slope (inclination) | 98.35° |
| Laps per day | 14 |
| Height THOR BURNER 2 R/B | 796.09 km |
Additional information THOR BURNER 2 R/B
THOR BURNER 2 R/B, 4048 is space debris in SSO originally from a launch on Wed, 23 Jul 1969 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 2 R/B Date of exalting 23.07.1969y. Average height of ISS THOR BURNER 2 R/B hundred 796.09 km. Average velocity THOR BURNER 2 R/B is 26845.41 km/h. Inclination THOR BURNER 2 R/B satellite 98.35°.TLE
Average velocity THOR BURNER 2 R/B
Average inclination THOR BURNER 2 R/B
Mean right ascension of the ascending node (RAAN) THOR BURNER 2 R/B
Mean argument of perigee THOR BURNER 2 R/B
Mean semi-major axis of the orbit THOR BURNER 2 R/B
Mean orbital eccentricity THOR BURNER 2 R/B
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