| Orbit | 800 km circular sun-synchronous orbit (inclination 98.57°) |
| Dimension | 352×356×670 mm |
| Mass | 47.5 kg |
| Maximum supply voltage | Max 30 W |
| Attitude control method | Gravity-gradient stabilization, magnetic torquer < 5 deg pointing accuracy |
| Communication (Tx speed) | Uplink (145 MHz frequency band): 9,600 bpsDownlink (436 MHz frequency band): 9,600 bps |
| On board computer | OBC186 (80C186) |
| Payload | CCD Earth imaging system (CEIS)Next generation small satellite computerHigh speed modulation experiment deviceDigital store and forward communication experiment (DSFCE)Low energy electron detector (LEED) |