Intelsat K |
INTELSAT / US |
Spacecraft n°: |
INTELSAT spacecraft n°: 48 |
| Designation: | 21989 / 92032A |
| Launch date | 09 Jun 1992 |
| Launch site | CC, LC-36B |
| Launch vehicle | Atlas-2A (AC-105) |
| Mission | Communications |
| Geostationary orbit on: | |
| Perigee / Apogee | km |
| Eccentricity | |
| Inclination | deg |
| Period | min |
| Location | 21.5°W |
| Out of service | Aug 2002 |
| Cause | Retired |
| Prime contractor | GE Astro Space |
| Platform | GE-5000 |
| Mass at launch | 2836 kg |
| Mass in orbit | 1547 kg |
| Dimension | 2.84 x 2.26 x 2.18 m |
| Solar array | 31.2 m span |
| Stabilization | 3-axis |
| DC power |
BOL:
4800 W EOL: equinox: 3639 W |
| Design lifetime | 10 years |
| Main transponders | 16 |
| Backup transponders | |
| Power | 62.5 W (TWTA) |
| Bandwidth | 54 MHz |
|
Coverage
and EIRP (beam peak to outer edge) |
Europe:
50.5-47 dBW United States: 52.2-47 dBW South America: 47.7-45 dBW North & South America: 45.5-42.7 dBW |
|
G/T (beam peak to outer edge) |
Europe:
+7.3 - +3.0 dB/K United States: +7.3 - +3.0 dB/K South America: +10 - +3.0 dB/K North America + Europe: +4 - -0.3 dB/K |
| Polarization | linear H/V |
| Frequencies |
Uplink:
14.00-14.50 GHz Downlink: 11.45-11.70 GHz (all beams) 11.70-11.95 GHz (Americas) 12.50-12.75 GHz (Europe) |
| Uplink |
Downlink
NAH |
Downlink
EUV |
Downlink
EUH |
Downlink
SAV | Possible combined downlink |
| 14.035 | 11.735 | 12.535 | 11.735 | (NAH + SAV) | |
| 14.095 | 11.795 | 12.595 | 11.795 | (NAH + SAV) | |
| 14.155 | 11.855 | 12.655 | 11.855 | (NAH + SAV) | |
| 14.215 | 11.915 | 12.715 | 11.915 | (NAH + SAV) | |
| 14.285 | 11.485 | 11.485 | 11.485 | 11.485 | (NAH + SAV) (NAH + EUV) (NAH + EUV + SAV) |
| 14.345 | 11.545 | 11.545 | 11.545 | 11.545 | (NAH + SAV) (NAH + EUV) (NAH + EUV + SAV) |
| 14.405 | 11.605 | 11.605 | 11.605 | 11.605 | (NAH + SAV) (NAH + EUV) (NAH + EUV + SAV) |
| 14.465 | 11.665 | 11.665 | 11.665 | 11.665 | (NAH + SAV) (NAH + EUV) (NAH + EUV + SAV) |