CEP 1 |
USA |
Spacecraft n°: |
USA satellite n°: |
| Designation | 04794 / 70106B |
| Launch date | 11 Dec 1970 - 11:35 UT |
| Launch site: | Va, SLC-2W |
| Launch vehicle | Delta-N6 (#546/D81) |
| Mission | |
| Earth orbit on: | |
| Perigee / Apogee | 1429 x 1487 km |
| Eccentricity | |
| Inclination | 102.1 deg |
| Period | 114.9 min |
| Prime contractor | |
| Platform | |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |
| Ref.: # - update: 13.03.09 | Home |