Attachment Schedule S document

This document pretains to SAT-LOA-20090227-00029 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2009022700029_698082

                             EXHIBIT 12: GALAXY KA LINK BUDGETS




Notes:
1) Carrier modulation is QPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).


                    EXHIBIT 12: GALAXY KA LINK BUDGETS (continued)




Notes:
1) Carrier modulation is QPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).


                    EXHIBIT 12: GALAXY KA LINK BUDGETS (continued)




Notes:
1) Carrier modulation is QPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).


                    EXHIBIT 12: GALAXY KA LINK BUDGETS (continued)




Notes:
1) Carrier modulation is BPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).


                    EXHIBIT 12: GALAXY KA LINK BUDGETS (continued)




Notes:
1) Carrier modulation is BPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).


                    EXHIBIT 12: GALAXY KA LINK BUDGETS (continued)




Notes:
1) Carrier modulation is QPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).


                    EXHIBIT 12: GALAXY KA LINK BUDGETS (continued)




Notes:
1) Carrier modulation is QPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).


                    EXHIBIT 12: GALAXY KA LINK BUDGETS (continued)




Notes:
1) Carrier modulation is QPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).


                    EXHIBIT 12: GALAXY KA LINK BUDGETS (continued)




Notes:
1) Carrier modulation is BPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).


                    EXHIBIT 12: GALAXY KA LINK BUDGETS (continued)




Notes:
1) Carrier modulation is BPSK
2) Link calculations apply to all combinations of the Conus and South America uplink and downlink beams.
3) The orbital location listed for each adjacent satellite corresponds to the topocentric location corresponding to a 2 degree
   geocentric separation with respect to Galaxy Ka and incorporating 0.05 degrees of stationkeeping accuracy as well as
   0.05 degrees of receive antenna mispointing towards one of the adjacent satellites (and 0.05 degree of mispointing away
   from the other adjacent satellite).



Document Created: 2009-03-03 15:17:55
Document Modified: 2009-03-03 15:17:55

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