Official name SPRINT A
Alternative name Hisaki (Sprint-A, Exceed)
Cospar ID 2013-049A
Norad ID 39253
Launch date 2013-09-14
Launch site KSCUT
Launch vehicle Epsilon CLPS
Country/Organization Japan
Type application Astronomy
Operator JAXA
RCS size LARGE
Decay date ON ORBIT
Period (min) 106.24
Inclination (deg) 29.72
Perigee (km) 951
Apogee (km) 1154
Eccentricity 0.096437054631829
Mean motion (revs. per day) 13.5542168674699
Semi-Major axis (km) 7430.635
Raan (deg) 184.5208
Arg of perigee (deg) 238.7448
Shape Box + 2 Pan
Mass (kg) 340
Height (m) 4
Width (m) 1
Depth (m) 1
Span (m^2) 6
Contractors NEC
Equipment EUV spectrometer, guiding camera
Configuration NEXTAR NX-300L
Power 2 deployable solar arrays, batteries

JAXA developed the small scientific satellite SPRINT-A (EXCEED or Hisaki) to design and verify the standard bus that can support a series of small scientific satellites. The SPRINT-A is a space telescope that remotely observes Venus, Mars, Jupiter and other planets from its earth orbit. By monitoring Venus, Mars, and Jupiter with extreme ultraviolet (EUV) rays, it will observe the plasma region defused from Jupiter I (Io) to study how energy is provided. It will also investigate the mechanism of how the atmosphere of some earth-type planets including Venus and Mars has escaped to space.

The mission payload contains an EUV spectrometer, and a guiding camera which maintains the pointing accuracy of the mission. SPRINT-A/EXCEED employs a new standard and flexible satellite bus module developed for the series in JAXA.

This mission replaces the cancelled TOPS satellite. It was launched on the maiden flight of the Epsilon launch vehicle.

Satellite COSPAR Date LS Launch Vehicle Remarks
SPRINT A 2013-049A 2013-09-14 KSCUT Epsilon CLPS