THOR DELTA 1 R/B
Satellite information THOR DELTA 1 R/B
| Spacetrack Directory Name | THOR DELTA 1 R/B |
| Follow THOR DELTA 1 R/B | THOR DELTA 1 R/B Tracker |
| Pass predictions THOR DELTA 1 R/B | Pass predictions THOR DELTA 1 R/B |
| Orbit launches |
1981-10-06 (44 years ago)
|
| Days in orbit | 16397 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 550 km |
| Apogee | 2652 km |
| Orbit slope (inclination) | 99.87° |
| Laps per day | 12 |
| Height THOR DELTA 1 R/B | 1675 km |
Additional information THOR DELTA 1 R/B
THOR DELTA 1 R/B, 12889 is space debris in SSO originally from a launch on Tue, 06 Oct 1981 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 DELTA 1 R/B Date of exalting 06.10.1981y. Average height of ISS THOR DELTA 1 R/B hundred 1675 km. Average velocity THOR DELTA 1 R/B is 25328.46 km/h. Inclination THOR DELTA 1 R/B satellite 99.88°.TLE
Average velocity THOR DELTA 1 R/B
Average inclination THOR DELTA 1 R/B
Mean right ascension of the ascending node (RAAN) THOR DELTA 1 R/B
Mean argument of perigee THOR DELTA 1 R/B
Mean semi-major axis of the orbit THOR DELTA 1 R/B
Mean orbital eccentricity THOR DELTA 1 R/B
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