| Structure | 6 U CubeSat, Mass - 14 kg |
| Payload (PL) | 40° and 2.5° Field of View (FOV) cameras |
| Rangefinder (RF) | Laser ranging (up to 5 km), supporting navigation |
| Electric Power System (EPS) | 80 W (maximum) solar panel arrays (SPAs) with 120 Wh batteries |
| Propulsion System (PS) | Monopropellant, four cold gas thrusters |
| Attitude Determination and Control System (ADCS) | 3-axis stabilization, star tracker, sun sensors, reaction wheel |
| Communication (COMM) | Four patch antennasReceiving (RX): 6.2 dB, 85°Transmitting (TX): 7 dB, 80°with 3-dB beam-width |