THOR BURNER 2A R/B
Satellite information THOR BURNER 2A R/B
| Spacetrack Directory Name | THOR BURNER 2A R/B |
| Follow THOR BURNER 2A R/B | THOR BURNER 2A R/B Tracker |
| Pass predictions THOR BURNER 2A R/B | Pass predictions THOR BURNER 2A R/B |
| 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 | 762 km |
| Apogee | 854 km |
| Orbit slope (inclination) | 99.08° |
| Laps per day | 14 |
| Height THOR BURNER 2A R/B | 816.35 km |
Additional information THOR BURNER 2A R/B
THOR BURNER 2A R/B, 7219 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 R/B Date of exalting 16.03.1974y. Average height of ISS THOR BURNER 2A R/B hundred 816.35 km. Average velocity THOR BURNER 2A R/B is 26807.6 km/h. Inclination THOR BURNER 2A R/B satellite 99.07°.TLE
Average velocity THOR BURNER 2A R/B
Average inclination THOR BURNER 2A R/B
Mean right ascension of the ascending node (RAAN) THOR BURNER 2A R/B
Mean argument of perigee THOR BURNER 2A R/B
Mean semi-major axis of the orbit THOR BURNER 2A R/B
Mean orbital eccentricity THOR BURNER 2A R/B
ISS
Buy us a coffee!
