SPACEMOBILE-SSR05 DEB
Satellite information SPACEMOBILE-SSR05 DEB - SPACEMOBILE-SSR05
| Spacetrack Directory Name | SPACEMOBILE-SSR05 DEB |
| Alternative name | SPACEMOBILE-SSR05 |
| Follow SPACEMOBILE-SSR05 DEB | SPACEMOBILE-SSR05 DEB Tracker |
| Pass predictions SPACEMOBILE-SSR05 DEB | Pass predictions SPACEMOBILE-SSR05 DEB |
| Orbit launches |
2024-09-12 (one year ago)
|
| Days in orbit | 714 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 499 km |
| Apogee | 512 km |
| Orbit slope (inclination) | 52.98° |
| Laps per day | 15 |
| Height SPACEMOBILE-SSR05 DEB | 466.94 km |
Additional information SPACEMOBILE-SSR05 DEB
SPACEMOBILE-SSR05 DEB, 62373 is space debris in LEO originally from a launch on Thu, 12 Sep 2024 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 SPACEMOBILE-SSR05 DEB Date of exalting 12.09.2024y. Average height of ISS SPACEMOBILE-SSR05 DEB hundred 466.94 km. Average velocity SPACEMOBILE-SSR05 DEB is 27486.04 km/h. Inclination SPACEMOBILE-SSR05 DEB satellite 52.98°.TLE
Average velocity SPACEMOBILE-SSR05 DEB
Average inclination SPACEMOBILE-SSR05 DEB
Mean right ascension of the ascending node (RAAN) SPACEMOBILE-SSR05 DEB
Mean argument of perigee SPACEMOBILE-SSR05 DEB
Mean semi-major axis of the orbit SPACEMOBILE-SSR05 DEB
Mean orbital eccentricity SPACEMOBILE-SSR05 DEB
ISS
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