Mercury F/O 1 (NROL-67, USA 250) |
USA |
Spacecraft nº: |
US spacecraft nº: |
Designation | 39652 / 14020A |
Launch date | 10 April 2014 - 17:45 UT |
Launch site | CC, SLC-41 |
Launch vehicle | Atlas-5/541 (AV-045) |
Mission | ELINT (Sigint) |
Geosynchronous orbit: | |
Perigee / Apogee | km |
Eccentricity | |
Inclination | ° |
Period | min |
Prime manufacturer | |
Platform | |
Operator | USAF |
Mass at launch | 3400 - 3850 kg |
Dry Mass | kg |
Basic shape | |
Dimension (m) | |
Equipment | Large Dish Antenna |
Solar array | |
Stabilization | 3-Axis-Stabilization |
Propulsion | |
DC power | |
Design lifetime |
Ref.: #7(JR696), #14, #228 - update: 02.12.14 | Home |