SPACEMOBILE-SSR02 DEB
Satellite information SPACEMOBILE-SSR02 DEB - SPACEMOBILE-002 DEB
| Spacetrack Directory Name | SPACEMOBILE-SSR02 DEB |
| Alternative name | SPACEMOBILE-002 DEB |
| Follow SPACEMOBILE-SSR02 DEB | SPACEMOBILE-SSR02 DEB Tracker |
| Pass predictions SPACEMOBILE-SSR02 DEB | Pass predictions SPACEMOBILE-SSR02 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 | 515 km |
| Orbit slope (inclination) | 52.94° |
| Laps per day | 15 |
| Height SPACEMOBILE-SSR02 DEB | 438.02 km |
Additional information SPACEMOBILE-SSR02 DEB
SPACEMOBILE-SSR02 DEB, 62370 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-SSR02 DEB Date of exalting 12.09.2024y. Average height of ISS SPACEMOBILE-SSR02 DEB hundred 438.02 km. Average velocity SPACEMOBILE-SSR02 DEB is 27544.41 km/h. Inclination SPACEMOBILE-SSR02 DEB satellite 52.94°.TLE
Average velocity SPACEMOBILE-SSR02 DEB
Average inclination SPACEMOBILE-SSR02 DEB
Mean right ascension of the ascending node (RAAN) SPACEMOBILE-SSR02 DEB
Mean argument of perigee SPACEMOBILE-SSR02 DEB
Mean semi-major axis of the orbit SPACEMOBILE-SSR02 DEB
Mean orbital eccentricity SPACEMOBILE-SSR02 DEB
ISS
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