
OPUSAT 2 [OPU]
OPUSAT 2 (Osaka Prefecture University Satellite) or Hirogari is a nanosatellite that was developed by Osaka Prefecture University. It follows the 2U CubeSat form factor.
OPUSAT 2 was developed based on the earlier OPUSAT. It has two main missions:
The satellite was launched on board of Cygnus CRS-15 on an Antares-230+ rocket to be delivered to the ISS, from where it was deployed via the JEM airlock.
| Nation: | Japan |
|---|---|
| Type / Application: | Technology |
| Operator: | Osaka Prefecture University (OPU) |
| Contractors: | Osaka Prefecture University (OPU) |
| Equipment: | |
| Configuration: | CubeSat (1U) |
| Propulsion: | None |
| Power: | 2 deployable fixed solar arrays, solar cells, batteries |
| Lifetime: | |
| Mass: | 1.4 kg |
| Orbit: | 414 km 421 km, 51.64 |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| OPUSAT 2 (Hirogari) | 1998-067SG | 20.02.2021 | WI LC-0A | Antares-230+ | with Cygnus CRS-15, Lawkanat 1, Gunsmoke-J 2, ORCA 6, ORCA 7, IT-SPINS, TAU-SAT 1, MYSAT 2, STARS-EC, RSP 01, WARP 01, Maya 2, Guaranisat 1, Tsuru, ThinSat 2A, ..., 2I |
