DSCS 3-06 |
USA |
Spacecraft n°: |
USA satellite n°: |
Designation | 22009 / 92037A |
Launch date | 02 Jul 1992 - 21:54:01 UT |
Launch site | CC, LC-36A |
Launch vehicle | Atlas-2 (AC-103) |
Mission | Military: Communications |
Geostationary orbit on: | |
Perigee / Apogee | 35718 x 35855 km |
Eccentricity | 1,62E-03 |
Inclination | 0.05 deg |
Period | 1436.1 min |
Location | 12,09 deg W |
Prime contractor | Lockheed Martin Missiles and Space |
Platform | |
Operator | US Air Force |
Mass at launch | 1156 kg |
Dry Mass | 884 kg |
Basic shape | |
Dimension (m) | |
Solar array | |
Stabilization | |
DC power | 1240 W |
Design lifetime | 10 yrs - No more active end 2019 |
Main transponders | 6 |
Backup | two 40 W and two 10 W amplifiers |
Power |
channels
1 & 2: 40 W (TWTA) channels 3 to 6: 10 W (SSPA) |
Coverage and EIRP max |
2
Global beams: 29 dBW 2 Spot beams: 34 dBW Gimballed dish: 44 dBW |
Channel | Bandwidth (MHz) | Frequency |
1 | 50 | ? |
2 | 75 | ? |
3 | 85 | ? |
4 | 85 | ? |
5 | 60 | ? |
6 | 50 | ? |
Ref.: #7, #15, #226 - update: 29.12.19 | Home |