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Names | KSAT Kagoshima Satellite |
---|---|
Mission type | Technology demonstration Atmospheric research |
Operator | Kagoshima University |
COSPAR ID | 2010-020A |
SATCAT no. | 36573 |
Mission duration | 55 days (achieved) |
Spacecraft properties | |
Spacecraft | CubeSat |
Bus | 1U CubeSat |
Manufacturer | Kagoshima University |
Launch mass | 1.43 kg (3.2 lb) |
Dimensions | 10 cm × 10 cm × 10 cm (3.9 in × 3.9 in × 3.9 in) |
Power | 2 deployable fixed solar panels, solar cells and batteries |
Start of mission | |
Launch date | 20 May 2010, 21:58:22 UTC |
Rocket | H-IIA (202) (# 17) |
Launch site | Tanegashima, Yoshinobu 1 |
Contractor | Mitsubishi Heavy Industries |
End of mission | |
Last contact | 1 June 2010 [1] |
Decay date | 14 July 2010 [2] |
Orbital parameters | |
Reference system | Geocentric orbit[3] |
Regime | Low Earth orbit |
Perigee altitude | 299.1 km (185.9 mi) |
Apogee altitude | 299.6 km (186.2 mi) |
Inclination | 30.0° |
Period | 90.5 minutes |
Hayato, known before launch as KSAT, or the Kagoshima Satellite, is a Japanese satellite which was launched on 20 May 2010. It is a student-built spacecraft, which is operated by Kagoshima University, and is being used for technology demonstration and atmospheric research.[4] The satellite is a single unit CubeSat, and carries equipment to study water vapour in the Earth's atmosphere, microwave imagery and spacecraft communication.[4][5]
Hayato
was invoked but never defined (see the help page).