Spacecraft data:
| Prime manufacturer | CIFAS/Aerospatiale consortium |
| Platform | |
| Operator | CNES, DFVLR |
| Mass at launch | 400 kg |
| Mass in orbit | 230 kg |
| Basic shape | Hexagonal body |
| Dimension (m) | |
| Equipment | 140 MHz transponder, C-band transponder |
| Solar array | 3 deployable fixed solar arrays |
| Stabilization | 3-axis stabilized |
| Propulsion | S400 |
| DC power | |
|
Location:
|
Begin
|
End
|
Position
|
|
L:
19 Dec 1974
|
1977
|
11.5°W
|
|
1977
|
Aug
1979
|
49°E
(for India, STEP project)
|
|
Aug
1979
|
19
Feb 1983
|
11.5°W
|
|