THOR AGENA B R/B
Satellite information THOR AGENA B R/B
| Spacetrack Directory Name | THOR AGENA B R/B |
| 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 |
1965-11-29 (60 years ago)
|
| Days in orbit | 22193 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 502 km |
| Apogee | 2650 km |
| Orbit slope (inclination) | 79.84° |
| Laps per day | 12 |
| Height THOR AGENA B R/B | 1638.08 km |
Additional information THOR AGENA B R/B
THOR AGENA B R/B, 1807 is space debris in LEO originally from a launch on Mon, 29 Nov 1965 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 AGENA B R/B Date of exalting 29.11.1965y. Average height of ISS THOR AGENA B R/B hundred 1638.08 km. Average velocity THOR AGENA B R/B is 25393.22 km/h. Inclination THOR AGENA B R/B satellite 79.84°.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
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