Arase (satellite)

Arase
Artistic rendering of Arase in orbit.
Mission typeEarth observation
OperatorJAXA
COSPAR ID2016-080A
SATCAT no.41896
Mission duration9 years, 2 months and 26 days (elapsed)
Spacecraft properties
ManufacturerNEC
Launch mass~350 kg
Power≧700 W
Start of mission
Launch date11:00, December 20, 2016 (UTC) (2016-12-20T11:00:00Z)
RocketEpsilon
Launch siteUchinoura
Orbital parameters
Reference systemGeocentric
Perigee altitude~460 km
Apogee altitude~32110 km
Inclination~31 degrees
Period~565 minutes
Instruments
  • Extremely high-energy electron sensor (XEP-e)
  • High-energy particle sensor – electron (HEP-e)
  • Medium-energy particle sensor – electron (MEP-e)
  • Low-energy particle sensor – electron (LEP-e)
  • Medium-energy particle – ion (MEP-i)
  • Low-energy particle – ion (LEP-i)
  • Magnetic Field Experiment (MGF)
  • Plasma Wave Experiment (PWE)
  • Software Wave-Particle Interaction Analyzer (S-WPIA)

Arase, formerly known as Exploration of energization and Radiation in Geospace (ERG), is a scientific satellite to study the Van Allen belts. It was developed by the Institute of Space and Astronautical Science of JAXA. The satellite was named after the Arase River in Kimotsuki, Kagoshima, where the Uchinoura Space Center is located.

It was launched aboard an Epsilon launch vehicle at 11:00:00, 20 December 2016 UTC into apogee height 32250 km, perigee 214 km orbit. Subsequent perigee-up operation moved its orbit to apogee 32110 km, perigee 460 km of 565 minutes period.