Mentor 3 |
USA |
Spacecraft n°: |
USA satellite n°: |
| Designation | 27937 / 03041A |
| Launch date | 09 Sept 2003 - 04:29 UT |
| Launch site | CC, SLC-40 |
| Launch vehicle | Titan-401B/Centaur-T (4B-36/TC-20) |
| Mission | SIGINT (Mentor = Advanced Magnum) |
| Geostationary orbit: | |
| Perigee / Apogee | km |
| Inclination | ° |
| Period | min |
| Location | 95.5°E |
| Prime contractor | |
| Customer | |
| Platform | |
| Mass at launch | 4500 kg? |
| Dry Mass | kg |
| Dimension | |
| Basic shape | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |