| System/Bus | Altitude | 500 km → 800 km rising → Earth re-entry |
| Mass | < 500 kg (including payload and propellant) |
| Lifetime | > 1 year |
| Power | ~300 W |
| Attitude control | 3 axis attitude control |
| Payload | Vision sensor | Monitoring/Control the ADR and RD |
| IR sensor | Sensing the target with -40 to 120 degree of temperature |
| Lidar | Precise distance observation (~500 m) |
| Space net | Net for capturing |
| Robotic arm | Arm more than 6 degree of freedom |
| Docking system | Docking device in Rendezvous |
| Transmission | X-band Transmitter (~100 Mbps) |
| Storage capacity | ~128 G |