M-4S R/B
Satellite information M-4S R/B
| Spacetrack Directory Name | M-4S R/B |
| Follow M-4S R/B | M-4S R/B Tracker |
| Pass predictions M-4S R/B | Pass predictions M-4S R/B |
| Orbit launches |
1971-09-28 (55 years ago)
|
| Days in orbit | 20097 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | KSCUT (Uchinoura Space Center, Japan) |
| Perigee | 867 km |
| Apogee | 1749 km |
| Orbit slope (inclination) | 32.03° |
| Laps per day | 13 |
| Height M-4S R/B | 1321.17 km |
Additional information M-4S R/B
M-4S R/B, 5498 is space debris in LEO originally from a launch on Tue, 28 Sep 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 28.09.1971y. Average height of ISS M-4S R/B hundred 1321.17 km. Average velocity M-4S R/B is 25916.64 km/h. Inclination M-4S R/B satellite 32.03°.TLE
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
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