SNUSAT 2 (original) (raw)
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SNUSAT 21 [SNU]
SNUSAT 2 (Seoul National University Satellite 2), is a South Korean 3U-CubeSat designed by the Seoul National University for early point of interest scanning for disaster monitoring using wide angle and high resolution cameras. Also testing in house developed star tracker and earth sensor.
The satellite was launched on Spaceflight Industry's SSO-A multi-satellite launch on a Falcon-9 v1.2 (Block 5) rocket.
| Nation: | South Korea |
|---|---|
| Type / Application: | Technology, earth observation |
| Operator: | Seoul National University |
| Contractors: | Seoul National University |
| Equipment: | FIPEX |
| Configuration: | CubeSat (3U) |
| Propulsion: | None |
| Power: | 4 deployable fixed solar arrays, solar cells, batteries |
| Lifetime: | |
| Mass: | |
| Orbit: | 572 km × 588 km, 97.76� |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks |
|---|---|---|---|---|---|
| SNUSAT 2 | 2018-099AA | 03.12.2018 | Va SLC-4E | Falcon-9 v1.2 (Block 5) | with SkySat 14, 15, Eu:CROPIS, STPSat 5, FalconSat 6, NEXTSat 1, KazSTSAT, eXCITe, SeeMe, ICEYE X2, BlackSky Global 2, ESEO, Hawk A, B, C, Capella 1, AISTECHSAT 2, CSIM-FD, Hiber 2, ITASAT 1, Landmapper-BC 4, ORS 7A, 7B, Al-Farabi 2, Astrocast 0.1, Audacy 0, BRIO, Centauri 1, Eaglet 1, Enoch, Flock-3s 1, 2, 3, K2SAT, KazSciSat 1, MinXSS 2, Orbital Reflector, RAAF M1, SeaHawk 1, THEA, VESTA, PW-Sat 2, SNUGLITE, VisionCube, RANGE A, B, Elysium-Star 2, ExseedSat 1, Fox 1C, Irvine 02, JY1-Sat, KNACKSAT, MOVE 2, SpaceBEE 5, 6, 7, Suomi-100, WeissSat 1, Sirion Pathfinder 2, OrbWeaver 1, 2, SPAWAR-CAL O, OR, R |