Asiasat 1 |
China (PR) |
Spacecraft nº: |
Chinese satellite nº: 33 |
Launch data:
|
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| Begin | End | Position |
| L: 7 Apr 1990 | Jun 1999 | 105.5°E |
| Aug 1999 | 122°E, inclined |
| Prime contractor | Hughes |
| Platform | HS-376 |
| Mass at launch | 1244 kg |
| Mass in orbit | 620 kg |
| Diameter | 2.16 m |
| Height | 6.6 m (2.84 m stowed) |
| Stabilization | Spin stabilized |
| DC power | BOL: 850 W |
| Design lifetime | 9 years |
| Main transponders | 24 |
| Backup transponders | 6 |
| Power | 8.5 W (TWTA) |
| Bandwidth | 36 MHz |
|
Coverage
and EIRP max | North beam: 36 dBW South beam: 37 dBW |
| G/T max | 3 dB/K |
| SFD | -81 to -90 dBW/m² |
| Polarization | linear H/V |
|
Horizontal
Uplink |
Horizontal
Downlink | Transponder |
Vertical
Downlink |
Vertical
Uplink |
| 3.720 | 1H | 5.945 | ||
| 5.965 | 1V | 3.740 | ||
| 3.760 | 2H | 5.985 | ||
| 6.005 | 2B | 3.780 | ||
| 3.800 | 3H | 6.025 | ||
| 6.045 | 3V | 3.820 | ||
| 3.840 | 4H | 6.065 | ||
| 6.085 | 4V | 3.860 | ||
| 3.880 | 5H | 6.105 | ||
| 6.125 | 5V | 3.900 | ||
| 3.920 | 6H | 6.145 | ||
| 6.165 | 6V | 3.940 | ||
| 3.960 | 7H | 6.185 | ||
| 6.205 | 7V | 3.980 | ||
| 4.000 | 8H | 6.225 | ||
| 6.245 | 8V | 4.020 | ||
| 4.040 | 9H | 6.265 | ||
| 6.285 | 9V | 4.060 | ||
| 4.080 | 10H | 6.305 | ||
| 6.325 | 10V | 4.100 | ||
| 4.120 | 11H | 6.345 | ||
| 6.365 | 11V | 4.140 | ||
| 4.160 | 12H | 6.385 | ||
| 6.405 | 12V | 4.180 |
| Ref.: #15, #77 - update: 27.03.17 | Home |