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 |
1978-02-16 (48 years ago)
|
| Days in orbit | 17732 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 974 km |
| Apogee | 1283 km |
| Orbit slope (inclination) | 69.21° |
| Laps per day | 13 |
| Height N-1 DEB | 1139.99 km |
Additional information N-1 DEB
N-1 DEB, 13132 is space debris in LEO originally from a launch on Thu, 16 Feb 1978 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 16.02.1978y. Average height of ISS N-1 DEB hundred 1139.99 km. Average velocity N-1 DEB is 26224.59 km/h. Inclination N-1 DEB satellite 69.21°.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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