| Prime contractor | Aerospatiale |
| Platform | Spacebus-2000 |
| Mass at launch | 1775 kg |
| Mass in orbit | 1078 kg |
| Dimension | 2.8 x 2.2 x 2.5 m |
| Solar array | 22.4 m span |
| Stabilization | 3 axis |
| DC power | EOL equinox: 2900 W |
| Design lifetime | 12 years |
| Apogee motor | MBB S400 (liquid fuel) |