N-1 DEB
Satellite information N-1 DEB
| Spacetrack Directory Name | N-1 DEB |
| Follow N-1 DEB | N-1 DEB Tracker |
| Pass predictions N-1 DEB | Pass predictions N-1 DEB |
| Orbit launches |
1982-09-03 (44 years ago)
|
| Days in orbit | 16072 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 927 km |
| Apogee | 1172 km |
| Orbit slope (inclination) | 44.58° |
| Laps per day | 14 |
| Height N-1 DEB | 1043.45 km |
Additional information N-1 DEB
N-1 DEB, 13510 is space debris in LEO originally from a launch on Fri, 03 Sep 1982 UTC launched from the Tanegashima Space Center (TNSTA). 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 N-1 DEB Date of exalting 03.09.1982y. Average height of ISS N-1 DEB hundred 1043.45 km. Average velocity N-1 DEB is 26396.26 km/h. Inclination N-1 DEB satellite 44.58°.TLE
Average velocity N-1 DEB
Average inclination N-1 DEB
Mean right ascension of the ascending node (RAAN) N-1 DEB
Mean argument of perigee N-1 DEB
Mean semi-major axis of the orbit N-1 DEB
Mean orbital eccentricity N-1 DEB
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