THOR AGENA B R/B
Satellite information THOR AGENA B R/B - TAVE
| Spacetrack Directory Name | THOR AGENA B R/B |
| Alternative name | TAVE |
| Follow THOR AGENA B R/B | THOR AGENA B R/B Tracker |
| Pass predictions THOR AGENA B R/B | Pass predictions THOR AGENA B R/B |
| Orbit launches |
1962-09-29 (64 years ago)
|
| Days in orbit | 23408 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Rocket body |
| Perigee | 992 km |
| Apogee | 1018 km |
| Orbit slope (inclination) | 80.47° |
| Laps per day | 14 |
| Height THOR AGENA B R/B | 1015.78 km |
Additional information THOR AGENA B R/B
THOR AGENA B R/B, 426 is space debris in LEO originally from a launch on Sat, 29 Sep 1962 UTC via a THOR AGENA B launch vehicle 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 AGENA B R/B Date of exalting 29.09.1962y. Average height of ISS THOR AGENA B R/B hundred 1015.78 km. Average velocity THOR AGENA B R/B is 26443.53 km/h. Inclination THOR AGENA B R/B satellite 80.47°.TLE
Average velocity THOR AGENA B R/B
Average inclination THOR AGENA B R/B
Mean right ascension of the ascending node (RAAN) THOR AGENA B R/B
Mean argument of perigee THOR AGENA B R/B
Mean semi-major axis of the orbit THOR AGENA B R/B
Mean orbital eccentricity THOR AGENA B R/B
ISS
Buy us a coffee!
