ADEOS 2
Satellite information ADEOS 2 - MIDORI II (ADEOS-II)
| Spacetrack Directory Name | ADEOS 2 |
| Alternative name | MIDORI II (ADEOS-II) |
| Follow ADEOS 2 | ADEOS 2 Tracker |
| Pass predictions ADEOS 2 | Pass predictions ADEOS 2 |
| Orbit launches |
2002-12-14 (23 years ago)
|
| Days in orbit | 8665 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Categories | |
| Perigee | 799 km |
| Apogee | 801 km |
| Orbit slope (inclination) | 98.8° |
| Laps per day | 14 |
| Height ADEOS 2 | 805.72 km |
Additional information ADEOS 2
ADEOS II (Advanced Earth Observing Satellite 2) was an Earth observation satellite launched by NASDA, with contributions from NASA and CNES, in December 2002. Its Japanese name was Midori 2, and it was the successor to the 1996 mission ADEOS I. The mission ended in October 2003 after the satellite's solar panels failed.
satellite ADEOS 2 Date of exalting 14.12.2002y. Average height of ISS ADEOS 2 hundred 805.72 km. Average velocity ADEOS 2 is 26827.42 km/h. Inclination ADEOS 2 satellite 98.79°.TLE
Average velocity ADEOS 2
Average inclination ADEOS 2
Mean right ascension of the ascending node (RAAN) ADEOS 2
Mean argument of perigee ADEOS 2
Mean semi-major axis of the orbit ADEOS 2
Mean orbital eccentricity ADEOS 2
ISS
Buy us a coffee!
