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 |