| 1 | Mission orbit | 500–600 km Sun-Synchronous Orbit | |
| 2 | Mission lifetime | 6 month | Designed for 1 year |
| 3 | Total mass | Max. 9 kg | |
| 4 | Propellant mass | 1,314 g | R-236fa |
| 5 | Size | 100 × 226.3 × 366 mm | 6U cubesat standar. |
| 6 | Solar array type | 2 wings (about 200 × 300 m. for each wing) | |
| 7 | Solar cell | Triple Junction Solar Cel. (8 × 4 cm) × 50 | AzureSpac. |
| 8 | S/A power generation | 20.38 W (@EOL) | Orbit average |
| 9 | Battery | 40 Wh | ClydeSpace |
| 10 | Bus supply voltage | 3.3 V, 5 V, 12 V, BAT | |
| 11 | Battery DOD | 30% | |
| 12 | Thruster total delta-V | ≥ 50 m/s | |
| 13 | On-board time accuracy | ~100 ms | |
| 14 | UHF uplink frequency | 436.50 MHz | |
| 15 | UHF downlink frequency | 436.50 MHz | |
| 16 | UHF uplink rate | 9.6 kbps | |
| 17 | UHF downlink frequency | 9.6 kbps | |
| 18 | S-band uplink frequency | 2,097.50 MHz | |
| 19 | S-band downlink frequency | 2,240.84 MHz | |
| 20 | S-band uplink rate | 1 Mbps | |
| 21 | S-band downlink frequency | 1 Mbps | |
| 22 | S/C RF power | 1 W (UHF) / 1 W (S-band) | |
| 23 | Mass memory | ~16 GB | |
| 24 | Pointing accuracy | Less than ± 3 deg (3σ) | |
| 25 | Pointing knowledge accuracy | Less than ± 0.01 deg (3σ. for Roll & Yaw ± 0.05 deg (3σ) for Pitch | |
| 26 | Sensor | MEMS Gyro (1 EA),MEMS Mag (1 EA),ASS (3 EA), ST (1 EA) | |
| 27 | Momentum dumping | Within 20 min , Period: 1 day | Normal mode |