H-2 R/B(2)
Satellite information H-2 R/B(2)
| Spacetrack Directory Name | H-2 R/B(2) |
| Follow H-2 R/B(2) | H-2 R/B(2) Tracker |
| Pass predictions H-2 R/B(2) | Pass predictions H-2 R/B(2) |
| Orbit launches |
1995-03-18 (31 years ago)
|
| Days in orbit | 11493 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 285 km |
| Apogee | 26243 km |
| Orbit slope (inclination) | 25.17° |
| Laps per day | 3 |
| Height H-2 R/B(2) | 16197.7 km |
Additional information H-2 R/B(2)
H-2 R/B(2), 23523 is space debris in HEO originally from a launch on Sat, 18 Mar 1995 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(2) Date of exalting 18.03.1995y. Average height of ISS H-2 R/B(2) hundred 16197.7 km. Average velocity H-2 R/B(2) is 14731.3 km/h. Inclination H-2 R/B(2) satellite 25.21°.TLE
Average velocity H-2 R/B(2)
Average inclination H-2 R/B(2)
Mean right ascension of the ascending node (RAAN) H-2 R/B(2)
Mean argument of perigee H-2 R/B(2)
Mean semi-major axis of the orbit H-2 R/B(2)
Mean orbital eccentricity H-2 R/B(2)
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