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 |