M-4S R/B
Satellite information M-4S R/B
| Spacetrack Directory Name | M-4S R/B |
| Orbit launches |
1971-02-16 |
| Deorbitation |
|
| Country/organisation of origin | Japonia (JPN) |
| Starting point | KSCUT (Uchinoura Space Center, Japan) |
| Perigee | 969 km |
| Apogee | 987 km |
| Height M-4S R/B | 977.91 km |
Additional information M-4S R/B
M-4S R/B, 5126 is space debris in LEO originally from a launch on Tue, 16 Feb 1971 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-4S R/B Date of exalting 16.02.1971y. Average height of ISS M-4S R/B hundred 977.91 km. Average velocity M-4S R/B is 26515 km/h. Inclination M-4S R/B satellite 29.68°.Average velocity M-4S R/B
Average inclination M-4S R/B
Mean right ascension of the ascending node (RAAN) M-4S R/B
Mean argument of perigee M-4S R/B
Mean semi-major axis of the orbit M-4S R/B
Mean orbital eccentricity M-4S R/B
ISS
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