KSAT-2
Japanese satellite
Names | Hayato-2 |
---|---|
Mission type | Technology demonstration Atmospheric research |
Operator | Kagoshima University |
COSPAR ID | 2014-009G ![]() |
SATCAT no. | 39578 |
Website | leo |
Mission duration | 80 days (achieved) |
Spacecraft properties | |
Spacecraft | CubeSat |
Bus | 1U CubeSat |
Manufacturer | Kagoshima University |
Launch mass | 1.5 kg (3.3 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 | 27 February 2014, 18:37 UTC[1] |
Rocket | H-IIA (202) |
Launch site | Tanegashima, Yoshinobu 1 |
Contractor | Mitsubishi Heavy Industries |
End of mission | |
Decay date | 18 May 2014 |
Orbital parameters | |
Reference system | Geocentric orbit[2] |
Regime | Low Earth orbit |
Perigee altitude | 382 km (237 mi) |
Apogee altitude | 389 km (242 mi) |
Inclination | 65.01° |
Period | 92.26 minutes |
KSAT-2, also known as Hayato-2 was a Japanese satellite constructed by Kagoshima University as a reflight of its KSAT mission. It has a size of 10 x 10 x 10 cm (without extendible antenna boom) and is built around a standard 1U CubeSat satellite bus. The primary satellite payload is a radio-frequency water vapor detector for climatology research.
See also
- List of CubeSats
- KSAT page (KSAT launched 20 May 2010, contact lost 12 days after launch)
References
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Report. Retrieved 1 January 2015.
- ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 1 January 2015.
External links
- Gunters space KSAT-2 page
- KSAT-2 tracking page
- v
- t
- e
- Progress M-22M
- ABS-2, Athena-Fidus
- Türksat 4A
- USA-248
- GPM Core, Ginrei, KSAT-2, INVADER, OPUSAT, STARS-II, TeikyoSat-3, ITF-1
- Kosmos 2495
- Ekspress AM4R
- USA-251
- USA-252
- Kosmos 2496, Kosmos 2497, Kosmos 2498, Kosmos 2499
- ALOS-2, Raijin-2, UNIFORM-1, SOCRATES, SPROUT
- Eutelsat 3B
- Soyuz TMA-13M
- Kosmos 2500 / GLONASS-M 755
- AprizeSat 9, AprizeSat 10, BRITE-Montreal, BRITE-Toronto, BugSat 1, Deimos-2, Hodoyoshi 3, Hodoyoshi 4, KazEOSat 2, Perseus-M1, Perseus-M2, SaudiSat-4, TabletSat-Aurora, UniSat-6 (Lemur-1, Tigrisat), Flock-1c × 11
- SPOT 7, CanX-4, CanX-5
- OCO-2
- Gonets-M × 3
- Meteor-M No.2
- O3b × 4
- CRS Orb-2 (Flock-1b × 28, TechEdSat-4)
- Orbcomm-OG2 × 6
- Foton-M No.4
- Progress M-24M
- USA-253 / GSSAP 1, USA-254 / GSSAP 2, USA-255 / ANGELS
- Georges Lemaître ATV
- USA-256
- AsiaSat 8
- Yaogan 20 A, B, C
- WorldView-3
- Gaofen 2, Heweliusz
- Galileo FOC-1, Galileo FOC-2
- Chuangxin 1-04, Lingqiao
- AsiaSat 6
- Yaogan 21, Tiantuo 2
- MEASAT 3b, Optus 10
- USA-257
- SpaceX CRS-4
- Soyuz TMA-14M
- Olimp-K
- Shijian XI-07
- Himawari 8
- IRNSS-1C
- ARSAT-1, Intelsat 30
- Yaogan 22
- Ekspress AM6
- Chang'e 5-T1, 4M
- Shijian 11-08
- Cygnus CRS Orb-3† (Arkyd-3†, Flock-1d × 26†)
- Progress M-25M
- USA-258 / GPS IIF 8
- Meridian 7
- Sasuke, Hodoyoshi 1, Kinshachi 1, Tsukushi, TSUBAME
- Yaogan 23
- Yaogan 24
- Kuaizhou 2
- Soyuz TMA-15M
- Kosmos 2501
- Hayabusa2, PROCYON, Shinen 2, DESPATCH
- Orion EFT-1
- DirecTV-14, GSAT-16
- CBERS-4
- Yaogan 25 A, B, C
- USA-259
- Yamal-401
- O3b × 4 (FM9 to FM12)
- Kondor-E No.2
- IPM
- Kosmos 2502
- Resurs-P No.2
- Yaogan 26
- Astra 2G
- Fengyun 2-08
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).