THOR ABLE DEB [YO]
Satellite information THOR ABLE DEB [YO] - Tiros 1 despin weight
| Spacetrack Directory Name | THOR ABLE DEB [YO] |
| Alternative name | Tiros 1 despin weight |
| Follow THOR ABLE DEB [YO] | THOR ABLE DEB [YO] Tracker |
| Pass predictions THOR ABLE DEB [YO] | Pass predictions THOR ABLE DEB [YO] |
| Orbit launches |
1960-04-01 (66 years ago)
|
| Days in orbit | 24247 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Debris |
| Perigee | 594 km |
| Apogee | 642 km |
| Orbit slope (inclination) | 48.16° |
| Laps per day | 15 |
| Height THOR ABLE DEB [YO] | 577.13 km |
Additional information THOR ABLE DEB [YO]
THOR ABLE DEB (YO), 115 is space debris in LEO originally from a launch on Fri, 01 Apr 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 ABLE DEB [YO] Date of exalting 01.04.1960y. Average height of ISS THOR ABLE DEB [YO] hundred 577.13 km. Average velocity THOR ABLE DEB [YO] is 27267.75 km/h. Inclination THOR ABLE DEB [YO] satellite 48.16°.TLE
Average velocity THOR ABLE DEB [YO]
Average inclination THOR ABLE DEB [YO]
Mean right ascension of the ascending node (RAAN) THOR ABLE DEB [YO]
Mean argument of perigee THOR ABLE DEB [YO]
Mean semi-major axis of the orbit THOR ABLE DEB [YO]
Mean orbital eccentricity THOR ABLE DEB [YO]
ISS
Buy us a coffee!
