SPACEMOBILE-SSR03 DEB
Satellite information SPACEMOBILE-SSR03 DEB - SPACEMOBILE-SSR03
| Spacetrack Directory Name | SPACEMOBILE-SSR03 DEB |
| Alternative name | SPACEMOBILE-SSR03 |
| Follow SPACEMOBILE-SSR03 DEB | SPACEMOBILE-SSR03 DEB Tracker |
| Pass predictions SPACEMOBILE-SSR03 DEB | Pass predictions SPACEMOBILE-SSR03 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 | 500 km |
| Apogee | 512 km |
| Orbit slope (inclination) | 52.97° |
| Laps per day | 15 |
| Height SPACEMOBILE-SSR03 DEB | 444.78 km |
Additional information SPACEMOBILE-SSR03 DEB
SPACEMOBILE-SSR03 DEB, 62371 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-SSR03 DEB Date of exalting 12.09.2024y. Average height of ISS SPACEMOBILE-SSR03 DEB hundred 444.78 km. Average velocity SPACEMOBILE-SSR03 DEB is 27530.69 km/h. Inclination SPACEMOBILE-SSR03 DEB satellite 52.97°.TLE
Average velocity SPACEMOBILE-SSR03 DEB
Average inclination SPACEMOBILE-SSR03 DEB
Mean right ascension of the ascending node (RAAN) SPACEMOBILE-SSR03 DEB
Mean argument of perigee SPACEMOBILE-SSR03 DEB
Mean semi-major axis of the orbit SPACEMOBILE-SSR03 DEB
Mean orbital eccentricity SPACEMOBILE-SSR03 DEB
ISS
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