NEXT SPACEFLIGHT

Status

Success

Fuji 2 & Midori

Launch Time
Sat Aug 17, 1996 01:53 UTC

Rocket

H-II (2 SSB)
MHI
Status: Retired
Payload to LEO: 10,060 kg
Payload to GTO: 3,930 kg
Stages: 2
Strap-ons: 4
Rocket Height: 49.0 m

Mission Details

Fuji 2

The JAS, also called Fuji 2, satellites were developed and built by the Japan Amateur Radio League. The 26-sided polyhedral satellites weighted 50 kg and were powered by body mounted solar cells, which supplied 10 W. The satellite were 0.44 m in diameter, and 0.47 m long. A turnstile antenna ring at its base received signals and four transmitting antennas extended from the top.

Payloads: 1
Total Mass: 50.0 kg
Low Earth Orbit

Midori

Primary applications of ADEOS (Advanced Earth Observation Satellite), which has been renamed Midori after reaching orbit, include monitoring global environmental changes such as maritime meteorological conditions, atmospheric ozone, and gases that promote global warming. ADEOS was also expected to play a vital role in developing more sophisticated inter-orbit communications and platform technology for the satellite of tomorrow. ADEOS was launched by H-2 Launch Vehicle No.4 on August 1996 and provided a large volume of data containing valuable information about our environment atmosphere, ocean and land for about 10 months until it suddenly got out of control on 30 June 1997 because of the structural damage in its solar array paddle.

Payloads: 1
Total Mass: 3,560.0 kg
Low Earth Orbit

Location

LA-Y1, Tanegashima Space Center, Japan

Stats

1996

50th orbital launch attempt

H-II

4th mission
1st mission of 1996
4th successful mission