H-2 R/B
Satellite information H-2 R/B
| Spacetrack Directory Name | H-2 R/B |
| Follow H-2 R/B | H-2 R/B Tracker |
| Pass predictions H-2 R/B | Pass predictions H-2 R/B |
| Orbit launches |
1996-08-17 (30 years ago)
|
| Days in orbit | 10975 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 859 km |
| Apogee | 1306 km |
| Orbit slope (inclination) | 98.76° |
| Laps per day | 13 |
| Height H-2 R/B | 1096.79 km |
Additional information H-2 R/B
H-2 R/B, 24279 is space debris in SSO originally from a launch on Sat, 17 Aug 1996 UTC launched 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-2 R/B Date of exalting 17.08.1996y. Average height of ISS H-2 R/B hundred 1096.79 km. Average velocity H-2 R/B is 26299.68 km/h. Inclination H-2 R/B satellite 98.76°.TLE
Average velocity H-2 R/B
Average inclination H-2 R/B
Mean right ascension of the ascending node (RAAN) H-2 R/B
Mean argument of perigee H-2 R/B
Mean semi-major axis of the orbit H-2 R/B
Mean orbital eccentricity H-2 R/B
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