NSS-6 |
Netherlands |
Spacecraft n°: |
Netherlands spacecraft n°: 4 |
| Designation | 27603 / 02057A |
| Launch date | 17 Dec 2002 - 23:04 UT |
| Launch site | Ko, ELA-2 |
| Launch vehicle | Ariane-44L (V156) |
| Mission | Communications |
| Geostationary orbit on: | |
| Perigee / Apogee | km |
| Eccentricity | |
| Inclination | ° |
| Period | min |
| Location | 95°E |
| Prime contractor | Lockheed martin |
| Platform | A2100AX |
| Mass at launch | |
| Mass in orbit | |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | EOL: 10000 W |
| Design lifetime | 14 years |
| Main transponders | 50 |
| Backup transponders | |
| Power | |
| Bandwidth | 36 MHz |
| Coverage |
6
beams: India China the Middle East (+ Cyprus and South Africa) Australia Southeast Asia Northeast Asia |
| EIRP max | 51 dBW |
| G/T max | +5 dB/K |
| Polarization | |
| Frequencies |
Uplink:
13.78-14.48 GHz Downlink: 10.95-11.20 (India or Middle East), 11.45-11.70 (NEA or Middle East), 12.50-12.75 (Australia) GHz |
| Main transponders | 12 |
| Backup transponders | |
| Power | |
| Bandwidth | |
| Coverage | spot beams (each spot covers 650 km) |
| EIRP max | |
| G/T max | +14 dB/K |
| Polarization | |
| Frequencies |
Uplink:
29.50-30 GHz Downlink: |
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| Ref.: #7, #15, #415 - update: 04.11.19 | Home |