EPSILON R/B
Satellite information EPSILON R/B
| Spacetrack Directory Name | EPSILON R/B |
| Follow EPSILON R/B | EPSILON R/B Tracker |
| Pass predictions EPSILON R/B | Pass predictions EPSILON R/B |
| 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 | 807 km |
| Apogee | 973 km |
| Orbit slope (inclination) | 29.75° |
| Laps per day | 14 |
| Height EPSILON R/B | 889.27 km |
Additional information EPSILON R/B
EPSILON R/B, 39255 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 R/B Date of exalting 14.09.2013y. Average height of ISS EPSILON R/B hundred 889.27 km. Average velocity EPSILON R/B is 26676.66 km/h. Inclination EPSILON R/B satellite 29.75°.TLE
Average velocity EPSILON R/B
Average inclination EPSILON R/B
Mean right ascension of the ascending node (RAAN) EPSILON R/B
Mean argument of perigee EPSILON R/B
Mean semi-major axis of the orbit EPSILON R/B
Mean orbital eccentricity EPSILON R/B
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