SNUGLITE (original) (raw)
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SNUSGLITE [SNU]
SNUGLITE is a South Korean 2U-CubeSat designed by the Seoul National University for technology demonstrations and amateur radio communication.
The mission of SNUGLITE is:
- Space station for amateur radio communication training. Sends beacon signals using UHF band with GMSK modulation. Earth stations that have capability of receiving S-band will be able to receive S-band signals.
- Technology demonstration of an in-house developed dual frequency GPS receiver.
- Technology demonstration of measuring TEC and magnetic field using dual frequency GPS receiver and fine magnetometer with a boom.
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 |
| Operator: | Seoul National University |
| Contractors: | Seoul National University |
| Equipment: | FIPEX |
| Configuration: | CubeSat (2U) |
| Propulsion: | None |
| Power: | 2 deployable fixed solar arrays, solar cells, batteries |
| Lifetime: | 3 months |
| Mass: | 2 kg |
| Orbit: | 572 km × 591 km, 97.77� |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks |
|---|---|---|---|---|---|
| SNUGLITE | 2018-099AC | 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 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, SNUSAT 2, THEA, VESTA, PW-Sat 2, 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 |