EPSILON DEB
Satellite information EPSILON DEB
| Spacetrack Directory Name | EPSILON DEB |
| Follow EPSILON DEB | EPSILON DEB Tracker |
| Pass predictions EPSILON DEB | Pass predictions EPSILON DEB |
| Orbit launches |
2013-09-14 (13 years ago)
|
| Days in orbit | 4770 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | KSCUT (Uchinoura Space Center, Japan) |
| Perigee | 847 km |
| Apogee | 1115 km |
| Orbit slope (inclination) | 29.7° |
| Laps per day | 14 |
| Height EPSILON DEB | 982.03 km |
Additional information EPSILON DEB
EPSILON DEB, 39254 is space debris in LEO originally from a launch on Sat, 14 Sep 2013 UTC launched from the Kagoshima Space Center University Of Tokyo (KSCUT). 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 EPSILON DEB Date of exalting 14.09.2013y. Average height of ISS EPSILON DEB hundred 982.03 km. Average velocity EPSILON DEB is 26507.55 km/h. Inclination EPSILON DEB satellite 29.71°.TLE
Average velocity EPSILON DEB
Average inclination EPSILON DEB
Mean right ascension of the ascending node (RAAN) EPSILON DEB
Mean argument of perigee EPSILON DEB
Mean semi-major axis of the orbit EPSILON DEB
Mean orbital eccentricity EPSILON DEB
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