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Observation
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ALOS |
Client |
JAXA |
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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. |
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