M-5 DEB
Satellite information M-5 DEB - M-V-1 DEB
| Spacetrack Directory Name | M-5 DEB |
| Alternative name | M-V-1 DEB |
| Follow M-5 DEB | M-5 DEB Tracker |
| Pass predictions M-5 DEB | Pass predictions M-5 DEB |
| Orbit launches |
1997-02-12 (29 years ago)
|
| Days in orbit | 10828 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | KSCUT (Uchinoura Space Center, Japan) |
| Perigee | 266 km |
| Apogee | 12817 km |
| Orbit slope (inclination) | 31.45° |
| Laps per day | 7 |
| Height M-5 DEB | 6925.84 km |
Additional information M-5 DEB
M-5 DEB, 27489 is space debris in HEO originally from a launch on Wed, 12 Feb 1997 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 M-5 DEB Date of exalting 12.02.1997y. Average height of ISS M-5 DEB hundred 6925.84 km. Average velocity M-5 DEB is 19592.54 km/h. Inclination M-5 DEB satellite 31.44°.TLE
Average velocity M-5 DEB
Average inclination M-5 DEB
Mean right ascension of the ascending node (RAAN) M-5 DEB
Mean argument of perigee M-5 DEB
Mean semi-major axis of the orbit M-5 DEB
Mean orbital eccentricity M-5 DEB
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