Prime contractor | Matra Marconi Espace |
Platform | ECS |
Mass at launch | 1210 kg |
Mass in orbit | 653 kg |
Payload mass | 134.4 kg: transponders: 107 kg, antennas: 27.4 kg |
Dimension | 2.06 x 1.9 x 2.2 m |
Solar array | 16 m span |
Stabilization | 3 axis |
DC power | EOL: equinox: 1483 W, solstice: 1450 W |
Payload power | 717.3 W |
Design lifetime | 7 years |