| Name of Satellite, Alternate Names | ShindaiSat (Shinshu University Satellite) |
| Country of Operator/Owner | Japan |
| Operator/Owner | Shinshu University |
| Users | Civil |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Circular |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 384 |
| Apogee (km) | 401 |
| Eccentricity | 0.00125693160813309 |
| Inclination (degrees) | 65.01 |
| Period (minutes) | 92.4 |
| Launch Mass (kg.) | 35 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 27-02-2014 |
| Expected Lifetime | |
| Contractor | Shinshu University |
| Country of Contractor | Japan |
| Launch Site | Tanegashima Space Center |
| Launch Vehicle | H-2A |
| COSPAR Number | 2014-009A |
| NORAD Number | 39572 |
| Comments | Equipped with an LED to drive an optical communications ground station link at distances up to 400 kilometres. |