| Prime contractor | Airbus Defence and Space |
| Platform | Eurostar 3000e (electric orbit raising) |
| Mass at launch | 5740 kg |
| Dry mass | |
| Mass in orbit | 5500 kg |
| Payload mass | |
| Dimension | |
| Solar array | |
| Stabilization | 3-axis |
| DC power | 21 kW |
| Payload power | |
| Design lifetime | 15 years |