THOR ABLESTAR R/B
Satellite information THOR ABLESTAR R/B
| Spacetrack Directory Name | THOR ABLESTAR R/B |
| Follow THOR ABLESTAR R/B | THOR ABLESTAR R/B Tracker |
| Pass predictions THOR ABLESTAR R/B | Pass predictions THOR ABLESTAR R/B |
| Orbit launches |
1964-10-06 (61 years ago)
|
| Days in orbit | 22613 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1032 km |
| Apogee | 1068 km |
| Orbit slope (inclination) | 90.23° |
| Laps per day | 14 |
| Height THOR ABLESTAR R/B | 1061.34 km |
Additional information THOR ABLESTAR R/B
THOR ABLESTAR R/B, 893 is space debris in LEO originally from a launch on Tue, 06 Oct 1964 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 ABLESTAR R/B Date of exalting 06.10.1964y. Average height of ISS THOR ABLESTAR R/B hundred 1061.34 km. Average velocity THOR ABLESTAR R/B is 26362.33 km/h. Inclination THOR ABLESTAR R/B satellite 90.23°.TLE
Average velocity THOR ABLESTAR R/B
Average inclination THOR ABLESTAR R/B
Mean right ascension of the ascending node (RAAN) THOR ABLESTAR R/B
Mean argument of perigee THOR ABLESTAR R/B
Mean semi-major axis of the orbit THOR ABLESTAR R/B
Mean orbital eccentricity THOR ABLESTAR R/B
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