OBJECT E
Satellite information OBJECT E
| Spacetrack Directory Name | OBJECT E |
| Follow OBJECT E | OBJECT E Tracker |
| Pass predictions OBJECT E | Pass predictions OBJECT E |
| Orbit launches |
2026-10-20 (15 days ago)
|
| Days in orbit | 15 |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 583 km |
| Apogee | 593 km |
| Orbit slope (inclination) | 52.99° |
| Laps per day | 15 |
| Height OBJECT E | 594.69 km |
Additional information OBJECT E
OBJECT E, 101115 is a satellite in LEO that was launched on Tue, 20 Oct 2026 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Unknown objects in Earths orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earths gravity.
satellite OBJECT E Date of exalting 20.10.2026y. Average height of ISS OBJECT E hundred 594.69 km. Average velocity OBJECT E is 27232.84 km/h. Inclination OBJECT E satellite 52.99°.TLE
Average velocity OBJECT E
Average inclination OBJECT E
Mean right ascension of the ascending node (RAAN) OBJECT E
Mean argument of perigee OBJECT E
Mean semi-major axis of the orbit OBJECT E
Mean orbital eccentricity OBJECT E
ISS
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