HIMAWARI 1 AKM
Satellite information HIMAWARI 1 AKM - 0 HIMAWARI 1 AKM
| Spacetrack Directory Name | HIMAWARI 1 AKM |
| Alternative name | 0 HIMAWARI 1 AKM |
| Follow HIMAWARI 1 AKM | HIMAWARI 1 AKM Tracker |
| Pass predictions HIMAWARI 1 AKM | Pass predictions HIMAWARI 1 AKM |
| Orbit launches |
1977-07-14 (49 years ago)
|
| Days in orbit | 17954 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 34394 km |
| Apogee | 36707 km |
| Orbit slope (inclination) | 4° |
| Laps per day | 1 |
| Height HIMAWARI 1 AKM | 35569.15 km |
Additional information HIMAWARI 1 AKM
HIMAWARI 1 AKM, 59985 is space debris in GEO originally from a launch on Thu, 14 Jul 1977 UTC launched from the Air Force Eastern Test Range (AFETR). 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 1 AKM Date of exalting 14.07.1977y. Average height of ISS HIMAWARI 1 AKM hundred 35569.15 km. Average velocity HIMAWARI 1 AKM is 11097.04 km/h. Inclination HIMAWARI 1 AKM satellite 4.03°.TLE
Average velocity HIMAWARI 1 AKM
Average inclination HIMAWARI 1 AKM
Mean right ascension of the ascending node (RAAN) HIMAWARI 1 AKM
Mean argument of perigee HIMAWARI 1 AKM
Mean semi-major axis of the orbit HIMAWARI 1 AKM
Mean orbital eccentricity HIMAWARI 1 AKM
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