THOR ABLESTAR R/B
Satellite information THOR ABLESTAR R/B - Ablestar 005
| Spacetrack Directory Name | THOR ABLESTAR R/B |
| Alternative name | Ablestar 005 |
| Follow THOR ABLESTAR R/B | THOR ABLESTAR R/B Tracker |
| Pass predictions THOR ABLESTAR R/B | Pass predictions THOR ABLESTAR R/B |
| Orbit launches |
1960-10-04 (65 years ago)
|
| Days in orbit | 24061 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Rocket body |
| Perigee | 920 km |
| Apogee | 1202 km |
| Orbit slope (inclination) | 28.25° |
| Laps per day | 14 |
| Height THOR ABLESTAR R/B | 1062.63 km |
Additional information THOR ABLESTAR R/B
THOR ABLESTAR R/B, 59 is space debris in LEO originally from a launch on Tue, 04 Oct 1960 UTC launched from the Air Force Eastern Test Range (AFETR). 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 04.10.1960y. Average height of ISS THOR ABLESTAR R/B hundred 1062.63 km. Average velocity THOR ABLESTAR R/B is 26363.29 km/h. Inclination THOR ABLESTAR R/B satellite 28.25°.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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