H-3 R/B
Satellite information H-3 R/B
| Spacetrack Directory Name | H-3 R/B |
| Follow H-3 R/B | H-3 R/B Tracker |
| Pass predictions H-3 R/B | Pass predictions H-3 R/B |
| Orbit launches |
2026-08-10 (one month ago)
|
| Days in orbit | 41 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TNSTA |
| Perigee | 210 km |
| Apogee | 35321 km |
| Orbit slope (inclination) | 22.58° |
| Laps per day | 2 |
| Height H-3 R/B | 23859.94 km |
Additional information H-3 R/B
H-3 R/B, 100271 is space debris in HEO originally from a launch on Mon, 10 Aug 2026 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-3 R/B Date of exalting 10.08.2026y. Average height of ISS H-3 R/B hundred 23859.94 km. Average velocity H-3 R/B is 12509.8 km/h. Inclination H-3 R/B satellite 22.67°.TLE
Average velocity H-3 R/B
Average inclination H-3 R/B
Mean right ascension of the ascending node (RAAN) H-3 R/B
Mean argument of perigee H-3 R/B
Mean semi-major axis of the orbit H-3 R/B
Mean orbital eccentricity H-3 R/B
ISS
Buy us a coffee!
