ADEOS-2

Japan


Spacecraft nº:

Japanese satellite nº: 106

Advanced Earth Observing Satellite, also called Midori-2

Launch data:

Designation 27597 / 02056A
Launch date14 Dec 2002 - 01:31 UT
Launch site Tanegashima
Launch vehicle:H-2A 202 (#11)
Mission Remote sensing, Earth observation
Earth orbit on:
Perigee/Apogee 803 km (sun synchronous)
Inclination 98.7°
Period 101 min
Cycle 41 days


Specifications

Prime contractorMitsubishi
OperatorNASDA
Platform  
Mass at launch 3680 kg
Mass in orbit  
Payload pass 1230 kg
Dimension 4 x 4 x 6 m
Solar array 3 x 24 m
Stabilization 3-axis
DC power BOL: 6200 W
EOL: 5350 W
Design lifetime 3 years

Photo of the ADEOS-II spacecraft during integration - Credit: JAXA



Downlink: 465.9875 or 468.875 MHz (EIRP > 27.1 dBm)
Uplink: 401.65 MHz

Payloads

Global Imager (GLI): observes solar radiation reflected from Earth surface. 23 visible + near-IR and 13 far-IR channels. 1 km resolution.
Advanced Microwave Scanning Radiometer (AMSR): 8 frequency bands covering 6.9 to 89 GHz.

Improved Limb Atmospheric Spectrometer (ILAS 2): maps distribution of gases in the stratosphere
Polarization and Directionality of the Earth's reflectances (POLDER): measures the reflection of solar light by aerosols, clouds, oceans and land surfaces.
Seawinds: scatterometer that monitors wind speed and direction. 2 m/s accuracy.

Mission details:

Illustration of the ADEOS-II spacecraft (image credit: JAXA)

External links:


Ref.: #7, #14, #235, #242 - update: 06.01.15 Home