SPACEMOBILE-SSR04 DEB
Satellite information SPACEMOBILE-SSR04 DEB - SPACEMOBILE-SSR04
| Spacetrack Directory Name | SPACEMOBILE-SSR04 DEB |
| Alternative name | SPACEMOBILE-SSR04 |
| Follow SPACEMOBILE-SSR04 DEB | SPACEMOBILE-SSR04 DEB Tracker |
| Pass predictions SPACEMOBILE-SSR04 DEB | Pass predictions SPACEMOBILE-SSR04 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 | 497 km |
| Apogee | 508 km |
| Orbit slope (inclination) | 52.98° |
| Laps per day | 15 |
| Height SPACEMOBILE-SSR04 DEB | 448.06 km |
Additional information SPACEMOBILE-SSR04 DEB
SPACEMOBILE-SSR04 DEB, 62372 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-SSR04 DEB Date of exalting 12.09.2024y. Average height of ISS SPACEMOBILE-SSR04 DEB hundred 448.06 km. Average velocity SPACEMOBILE-SSR04 DEB is 27524.14 km/h. Inclination SPACEMOBILE-SSR04 DEB satellite 52.99°.TLE
Average velocity SPACEMOBILE-SSR04 DEB
Average inclination SPACEMOBILE-SSR04 DEB
Mean right ascension of the ascending node (RAAN) SPACEMOBILE-SSR04 DEB
Mean argument of perigee SPACEMOBILE-SSR04 DEB
Mean semi-major axis of the orbit SPACEMOBILE-SSR04 DEB
Mean orbital eccentricity SPACEMOBILE-SSR04 DEB
ISS
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