THOR AGENA D R/B
Satellite information THOR AGENA D R/B - HAYLOFT
| Spacetrack Directory Name | THOR AGENA D R/B |
| Alternative name | HAYLOFT |
| Follow THOR AGENA D R/B | THOR AGENA D R/B Tracker |
| Pass predictions THOR AGENA D R/B | Pass predictions THOR AGENA D R/B |
| Orbit launches |
1964-01-11 (62 years ago)
|
| Days in orbit | 22932 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Rocket body |
| Perigee | 902 km |
| Apogee | 917 km |
| Orbit slope (inclination) | 69.91° |
| Laps per day | 14 |
| Height THOR AGENA D R/B | 918.79 km |
Additional information THOR AGENA D R/B
THOR AGENA D R/B, 727 is space debris in LEO originally from a launch on Sat, 11 Jan 1964 UTC via a THOR SLV-2A AGENA D launch vehicle 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 D R/B Date of exalting 11.01.1964y. Average height of ISS THOR AGENA D R/B hundred 918.79 km. Average velocity THOR AGENA D R/B is 26619.24 km/h. Inclination THOR AGENA D R/B satellite 69.91°.TLE
Average velocity THOR AGENA D R/B
Average inclination THOR AGENA D R/B
Mean right ascension of the ascending node (RAAN) THOR AGENA D R/B
Mean argument of perigee THOR AGENA D R/B
Mean semi-major axis of the orbit THOR AGENA D R/B
Mean orbital eccentricity THOR AGENA D R/B
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