Official name HIMAWARI 7
Alternative name Himawari 7 (MTSAT 2)
Cospar ID 2006-004A
Norad ID 28937
Launch date 2006-02-18
Launch site TNSTA
Launch vehicle H-2A-2024
Country/Organization Japan
Type application Communication, Meteorology
Operator Japanese Ministry of Transport Civil Aviation Bureau & Meteorological Agency
RCS size LARGE
Decay date ON ORBIT
Period (min) 1453.4
Inclination (deg) 3.79
Perigee (km) 36106
Apogee (km) 36143
Eccentricity 0.000512117814779443
Mean motion (revs. per day) 0.990780239438558
Semi-Major axis (km) 42502.635
Raan (deg) 82.181
Arg of perigee (deg) 138.1998
Shape Box + 1 Pan + 1 Arm
Mass (kg) 4650
Height (m) 6
Width (m) 4
Depth (m) 4
Span (m^2) 30
Lifetime 10 years
Contractors Mitsubishi Electric (prime), Boeing
Equipment IMAGER
Propulsion R-4D-11-164
Configuration DS-2000
Power Deployable solar array, batteries

The MTSAT-2 (Multifunctional Transport Satellite) is a multi-functional satellite with a dual purpose:

On the one hand, it is an integral part of a next-generation global-scale air traffic safety system comprised of communications, navigation, tracking and air traffic control. The purpose is to improve traffic congestion and safety in the Asia Pacific region.

On the other hand, the MTSAT-2 is designed to take on a meteorological mission to capture, collect and deliver meteorological images and/or data. In this capacity it inherits and expands the mission of a previous satellite.

The satellite carries IMAGER, an imaging telescope, backed by detectors for five wavelength channels:

  1. Visible band at 0.55-0.80 microns, detected by silicon photovoltaic detectors at a spatial resolution of 1.25 km;
  2. 10.3-11.3 micron infrared channel (IR1) with a HgCdTe photoconductive detector.
  3. 11.5-12.5 micron channel (IR2) with a HgCdTe detector;
  4. 6.5-7.0 micron water vapor channel (IR3) with a HgCdTe detector; and,
  5. 3.5-4.0 micron near-infrared channel with an InSb photovoltaic detector.

All infrared channels provide a spatial resolution of 5.0 km.

For the meteorological mission, MTSAT-2 will play a role of a back-up satellite while MTSAT-1R is in operation until 2008. After the commencement of MTSAT-2 operations, MTSAT-1R will be used as a stand-by satellite for the meteorological mission.

MTSat 2 was renamed Himawari 7 after launch.

In May 2020, MTSat 2 was moved to a graveyard orbit above GEO.

Satellite COSPAR Date LS Launch Vehicle Remarks
HIMAWARI 7 2006-004A 2006-02-18 TNSTA H-2A-2024