Hayato (satellite)
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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
Launch
The launch was conducted by
cryogenic propellant into the rocket's first and second stages had been completed.[6] The launch attempt was scrubbed a few minutes before liftoff due to bad weather, but took place successfully at 21:58:22 UTC
on 20 May 2010.
Mission
Hayato was deployed from a
See also
References
- ^ a b "KSAT (Hayato) Project". Kagoshima University. 6 September 2011. Archived from the original on 14 April 2014. Retrieved 24 October 2021.
- ^ "Information furnished in conformity with the Convention on Registration of Objects Launched into Outer Space" (PDF). Committee on the Peaceful Uses of Outer Space. 25 July 2011. Retrieved 24 October 2021.
- ^ "Launch Log". Jonathan's Space Report. 21 July 2021. Retrieved 24 October 2021.
- ^ a b Krebs, Gunter (11 December 2017). "KSAT (Hayato)". Gunter's Space Page. Retrieved 24 October 2021.
- ^ "鹿児島人工衛星開発部会 プロジェクト". Kagoshima University. Archived from the original on 15 May 2010. Retrieved 24 October 2021.
- ^ a b "Countdown Report". H-IIA Launch Services Flight 17. Mitsubishi Heavy Industries. Archived from the original on 9 August 2016. Retrieved 17 May 2010.
- ^ "Overview of Secondary Payloads". Akatsuki Special Site. JAXA. Retrieved 17 May 2010.