SPACEMOBILE-SSR01 DEB
Satellite information SPACEMOBILE-SSR01 DEB - SPACEMOBILE-001 DEB
| Spacetrack Directory Name | SPACEMOBILE-SSR01 DEB |
| Alternative name | SPACEMOBILE-001 DEB |
| Follow SPACEMOBILE-SSR01 DEB | SPACEMOBILE-SSR01 DEB Tracker |
| Pass predictions SPACEMOBILE-SSR01 DEB | Pass predictions SPACEMOBILE-SSR01 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 | 517 km |
| Orbit slope (inclination) | 52.99° |
| Laps per day | 15 |
| Height SPACEMOBILE-SSR01 DEB | 464.81 km |
Additional information SPACEMOBILE-SSR01 DEB
SPACEMOBILE-SSR01 DEB, 62369 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-SSR01 DEB Date of exalting 12.09.2024y. Average height of ISS SPACEMOBILE-SSR01 DEB hundred 464.81 km. Average velocity SPACEMOBILE-SSR01 DEB is 27490.4 km/h. Inclination SPACEMOBILE-SSR01 DEB satellite 52.99°.TLE
Average velocity SPACEMOBILE-SSR01 DEB
Average inclination SPACEMOBILE-SSR01 DEB
Mean right ascension of the ascending node (RAAN) SPACEMOBILE-SSR01 DEB
Mean argument of perigee SPACEMOBILE-SSR01 DEB
Mean semi-major axis of the orbit SPACEMOBILE-SSR01 DEB
Mean orbital eccentricity SPACEMOBILE-SSR01 DEB
ISS
Buy us a coffee!
