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 |