Intelsat 806 |
INTELSAT / US |
Spacecraft n°: |
INTELSAT spacecraft n°: 62 |
| Designation: | 25239 / 98014A |
| Launch date | 28 Feb 1998 |
| Launch site | CC, LC-36B |
| Launch vehicle | Atlas-2AS (AC-151 #114) |
| Mission: | Telecommunications |
| Geostationary orbit on: | |
| Perigee / Apogee | km |
| Eccentricity | |
| Inclination | deg |
| Period | min |
| Location | 40.5°W |
| Prime manufacturer | Lockheed Martin |
| Platform | LM-3000 |
| Operator | Intelsat, Ltd |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| slot # | Uplink (GHz) | Downlink (GHz) | Hemi A | Hemi B | Bandwidth (MHz) |
| 5'-6' | 6.527 | 3.502 | 12' | 22' | 72 |
| 3'-4' | 6.607 | 3.582 | 11' | 21' | 72 |
| 1'-2' | 5.888 | 3.663 | 10 | 20 | 72 |
| 1-2 | 5.968 | 3.743 | 11 | 21 | 72 |
| 3 | 6.028 | 3.803 | 12A | 22A | 36 |
| 4 | 6.068 | 3.843 | 12B | 22B | 36 |
| 5 | 6.108 | 3.883 | 13A | 23A | 36 |
| 6 | 6.148 | 3.923 | 13B | 23B | 36 |
| 7 | 6.201 | 3.976 | 14A | 24A | 36 |
| 8 | 6.240 | 4.014 | 14B | 24B | 36 |
| 9 | 6.280 | 4.055 | 15 | 25 | 36 |
| 10 | 6.320 | 4.095 | 16 | 26 | 36 |
| 11 | 6.360 | 4.135 | 17 | 27 | 36 |
| 12 | 6.4025 | 4.1775 | 18 | 28 | 41 |
| Pol.: | A | B |
| Uplink beam | slot # | Downlink beam | Band |
| hemi A | 1'-2', 1-2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 3'-4', 5'-6' | hemi A | C |
| hemi A | 1-2, 4/3-4, 6/5-6 | spot 1 | Ku |
| hemi B | 1'-2', 1-2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 3'-4', 5'-6' | hemi B | C |
| slot # | Uplink (GHz) | Downlink (GHz) | Spot 1 | Bandwith (MHz) |
| 1-2 | 14.0425 | 11.7475 | 261 | 77 |
| 3-4 | 14.125 | 11.830 | 262 | 72 |
| 5-6 | 14.205 | 11.910 | 263 | 72 |
| Pol: | V | H |
| Uplink beam | slot # | Downlink beam | Band |
| spot 1 | 1-2, 3-4, 5-6 | spot 1 | Ku |
| spot 1 | 1-2, 3-4/4, 5-6/6 | hemi A | C |