Official name GCOM-C
Alternative name Shikisai
Cospar ID 2017-082A
Norad ID 43065
Launch date 2017-12-23
Launch site TNSTA
Launch vehicle H-2A-202
Country/Organization Japan
Type application Earth observation
Operator JAXA
RCS size LARGE
Decay date ON ORBIT
Period (min) 100.89
Inclination (deg) 98.67
Perigee (km) 800
Apogee (km) 802
Eccentricity 0.00124843945068664
Mean motion (revs. per day) 14.2729705619982
Semi-Major axis (km) 7179.135
Raan (deg) 218.8181
Arg of perigee (deg) 109.3547
Shape Box + 2 Pan + 1 Dish
Mass (kg) 2093
Height (m) 4.6
Width (m) 2.5
Depth (m) 2.5
Span (m^2) 16.5
Lifetime 5 years
Equipment SGLI
Power 2 deployable solar arrays, batteries

The GCOM-C (Global Change Observation Mission - Carbon cycle) aims to contribute to surface and atmospheric measurements related to the carbon cycle and the radiation budget. The payload consists of a second-generation GLI (SGLI) instrument.

SGLI (Second Generation Global Imager). SGLI is an advanced multi-purpose visible/infrared (VNIR) imager of GLI heritage, flown on ADEOS-II. The objective is to measure ocean color, land use and vegetation, snow and ice, clouds, aerosols and water vapor, etc.

  • The largest target of SGLI is to retrieve global aerosol distributions. To achieve this target, SGLI will have 2 polarization channels with 3 directions
  • SGLI is mainly focused to land and coastal areas. There are 11 channels with an IFOV of 250 m. GLI on ADEOS-II had only 6 channels of 250 m resolution.
  • SGLI is a pushbroom instrument providing 29 channels in the VNIR (Visible Near Infrared) spectral region. In addition, there are 6 channels in the SWIR (Shortwave Infrared) and TIR (Thermal Infrared) regions being served by a whiskbroom scanner (mechanical method).
Satellite COSPAR Date LS Launch Vehicle Remarks
GCOM-C 2017-082A 2017-12-23 TNSTA H-2A-202 with SLATS