Akebono

Launch Success

Liftoff Time (GMT)

23:30:00

Tuesday February 21, 1989

Mission Details

Akebono

Wiki

The purpose of the Exos D or Akebono mission was to investigate the particle acceleration regions above the auroral region in order to develop a better understanding of the acceleration mechanism and its relation to substorm phenomena. The spacecraft was spin-stabilized with a rotation rate of 7.5 rpm. The attitude was magnetically controlled with the spacecraft axis pointing to the sun. All onboard operations such as command and data acquisition were controlled by an onboard computer permitting automatic operations for a full week. JAXA stopped sending and receiving signals to and from EXOS-D on April 23, 2015, to terminate its operation after more than 26 years in orbit.

Medium Earth Orbit

1 Payload

294 kilograms

Rocket

Retired
Mu-III S2

Active 1985 to 1995

Institute of Space and Aeronautical Science logo

Agency

ISAS

Payload to Orbit

LEO: 770 kg

Stages

4

Strap-ons

2

Launch Site

Mu Pad

Uchinoura Space Center, Japan

Fastest Turnaround

143 days 23 hours

Stats

Mu-III


15th

Mission

1st

Mission of 1989

Institute of Space and Aeronautical Science


19th

Mission

1st

Mission of 1989

1989


16th

Orbital launch attempt