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Observation

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ALOS

Client JAXA
Launch date January 24, 2006
Launch vehicle H-IIA
Launch site Tanegashima Space Center
Orbit Sun-synchronous subrecurrent orbit
Mass 4000 kg (at launch)
Electrical power 7000 W (EOL)
Design life 3 to 5 years
Responsibilities Sub contractor
Outline ALOS is a satellite following JERS-1 and ADEOS, which utilizes advanced land observing technology.
ALOS is used for cartography, regional observation, disaster monitoring and resource surveying.