Jumpseat 4 |
USA |
Spacecraft n°: |
USA satellite n°: |
| Designation | 75017A |
| Launch date | 10 Mar 1975 |
| Launch site | Va, SLC-4W |
| Launch vehicle | Titan-3(34)B Agena-D |
| Mission | NRO signals intelligence |
| HEO Earth orbit on: | |
| Perigee / Apogee | 295 x 39338 km |
| Eccentricity | |
| Inclination | 63.5 deg |
| Period | min |
| Prime contractor | |
| Operator | |
| Platform | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |