H-1 R/B(MABES)
Satellite information H-1 R/B(MABES)
| Spacetrack Directory Name | H-1 R/B(MABES) |
| Follow H-1 R/B(MABES) | H-1 R/B(MABES) Tracker |
| Pass predictions H-1 R/B(MABES) | Pass predictions H-1 R/B(MABES) |
| Orbit launches |
1986-08-12 (40 years ago)
|
| Days in orbit | 14633 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 1481 km |
| Apogee | 1595 km |
| Orbit slope (inclination) | 50° |
| Laps per day | 12 |
| Height H-1 R/B(MABES) | 1544.3 km |
Additional information H-1 R/B(MABES)
H-1 R/B(MABES), 16910 is space debris in LEO originally from a launch on Tue, 12 Aug 1986 UTC via an H-1 launch vehicle 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 H-1 R/B(MABES) Date of exalting 12.08.1986y. Average height of ISS H-1 R/B(MABES) hundred 1544.3 km. Average velocity H-1 R/B(MABES) is 25547.01 km/h. Inclination H-1 R/B(MABES) satellite 50°.TLE
Average velocity H-1 R/B(MABES)
Average inclination H-1 R/B(MABES)
Mean right ascension of the ascending node (RAAN) H-1 R/B(MABES)
Mean argument of perigee H-1 R/B(MABES)
Mean semi-major axis of the orbit H-1 R/B(MABES)
Mean orbital eccentricity H-1 R/B(MABES)
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