HIMAWARI 4 AKM
Satellite information HIMAWARI 4 AKM
| Spacetrack Directory Name | HIMAWARI 4 AKM |
| Follow HIMAWARI 4 AKM | HIMAWARI 4 AKM Tracker |
| Pass predictions HIMAWARI 4 AKM | Pass predictions HIMAWARI 4 AKM |
| Orbit launches |
1989-09-05 (36 years ago)
|
| Days in orbit | 13513 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| WWW | Here |
| Perigee | 35177 km |
| Apogee | 37252 km |
| Orbit slope (inclination) | 12.52° |
| Laps per day | 1 |
| Height HIMAWARI 4 AKM | 36216.16 km |
Additional information HIMAWARI 4 AKM
HIMAWARI 4 AKM, 20317 is space debris in GEO originally from a launch on Tue, 05 Sep 1989 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 HIMAWARI 4 AKM Date of exalting 05.09.1989y. Average height of ISS HIMAWARI 4 AKM hundred 36216.16 km. Average velocity HIMAWARI 4 AKM is 11014.43 km/h. Inclination HIMAWARI 4 AKM satellite 12.53°.TLE
Average velocity HIMAWARI 4 AKM
Average inclination HIMAWARI 4 AKM
Mean right ascension of the ascending node (RAAN) HIMAWARI 4 AKM
Mean argument of perigee HIMAWARI 4 AKM
Mean semi-major axis of the orbit HIMAWARI 4 AKM
Mean orbital eccentricity HIMAWARI 4 AKM
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