M-3H R/B
Satellite information M-3H R/B
| Spacetrack Directory Name | M-3H R/B |
| Follow M-3H R/B | M-3H R/B Tracker |
| Pass predictions M-3H R/B | Pass predictions M-3H R/B |
| Orbit launches |
1978-09-16 (48 years ago)
|
| Days in orbit | 17552 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | KSCUT (Uchinoura Space Center, Japan) |
| Perigee | 252 km |
| Apogee | 10564 km |
| Orbit slope (inclination) | 31.26° |
| Laps per day | 8 |
| Height M-3H R/B | 5502.58 km |
Additional information M-3H R/B
M-3H R/B, 11028 is space debris originally from a launch on Sat, 16 Sep 1978 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-3H R/B Date of exalting 16.09.1978y. Average height of ISS M-3H R/B hundred 5502.58 km. Average velocity M-3H R/B is 20782.8 km/h. Inclination M-3H R/B satellite 31.24°.TLE
Average velocity M-3H R/B
Average inclination M-3H R/B
Mean right ascension of the ascending node (RAAN) M-3H R/B
Mean argument of perigee M-3H R/B
Mean semi-major axis of the orbit M-3H R/B
Mean orbital eccentricity M-3H R/B
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