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 |
1971-04-01 (55 years ago)
|
| Days in orbit | 20242 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1353 km |
| Apogee | 1421 km |
| Orbit slope (inclination) | 88.16° |
| Laps per day | 13 |
| Height THOR DELTA 1 R/B | 1398.49 km |
Additional information THOR DELTA 1 R/B
THOR DELTA 1 R/B, 5106 is space debris in LEO originally from a launch on Thu, 01 Apr 1971 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 01.04.1971y. Average height of ISS THOR DELTA 1 R/B hundred 1398.49 km. Average velocity THOR DELTA 1 R/B is 25784.4 km/h. Inclination THOR DELTA 1 R/B satellite 88.17°.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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