Attachment Sched S Tech Report

This document pretains to SAT-MOD-20100421-00081 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2010042100081_812075

FCC 312 FEDERAL COMMUNICATIONS COMMISSION Page 1: General, Schedule S SATELLITE SPACE STATION AUTHORIZATIONS Frequency Bands, (Technical and Operational Description) and GSO Orbit S1. GENERAL INFORMATION Complete for all satellite applications. a. Space Station or Satellite Network Name: e. Estimated Date of Placement into Service: i Will the space station(s) operate on a Common Carrier Basis: AMC-4 12/22/1999 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 52 0 MHz d1. Est Launch Date Begin: d2. Est Launch Date End: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply: 11/13/1999 11/13/1999 2016 MHz GSO NGSO X S2. OPERATING FREQUENCY BANDS Identify the frequency range and transmit/receive mode for all frequency bands in which this station will oper Also indicate the nature of service(s) for each frequency band. Frequency Band Limits Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode f. Nature of Service(s): List all that apply to this band a. Numeric b. Unit c. Numeric d. Unit (K/M/G) (K/M/G) 14.0 G 14.5 G R Fixed Satellite Service 14.0 G 14.5 G R Direct to Home in the Fixed Fixed Satellite Service 11.7 G 12.2 G T Fixed Satellite Service 11.7 G 12.2 G T Direct to Home in the Fixed Fixed Satellite Service 5925 M 6425 M R Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 13.75 G 14.0 G R Fixed Satellite Service 11.45 G 11.7 G T Fixed Satellite Service S3. ORBITAL INFORMATION FOR GEOSTATIONARY SATELLITES ONLY: a. Nominal Orbital Longitude (Degrees E/W): b. Alternate Orbital Longitude (Degrees E/W): c. Reason for orbital location selection: 67 W Availability of the orbital location with good elevation Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be angles for South and North American coverage N/S Station-Keeping provided (Optional): d. Toward West: Degrees E/W 0.05 Degrees Tolerance: g. Westernmost: e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: i. Reason for service are selection (Optional):

FEDERAL COMMUNICATIONS COMMISSION Page 2: NGSO Orbits SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S4. ORBITAL INFORMATION FOR NON-GEOSTATIONARY SATELLITES ONLY S4a. Total Number of Satellites in Network or System: S4c. Celestial Reference Body (Earth, Sun, Moon, etc.): S4b. Total Number of Orbital Planes in Network or System: S4d. Orbit Epoch Date: For each Orbital Plane Provide: (e) Orbital (f) No. of (g) Inclination (h) Orbital (i) Apogee (km) (j) Perigee (km) (k) Right Ascension (l) Argument of Active Service Arc Range (Degrees) Plane No. Satellites in Angle (degrees) Period of the Ascending Perigee (m) Begin (n) End (o) Other Plane (Seconds) Node (Deg.) (Degrees) Angle Angle S5. INITIAL SATELLITE PHASE ANGLE For each satellite in each orbital plane, provide the intital phase angle. (a) Orbital (b) Satellite (c) Initial Plane No. Number Phase Angle (Degrees) NO NGSO DATA FILED

FEDERAL COMMUNICATIONS COMMISSION Page 3: Service Areas SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S6. SERVICE AREA CHARACTERISTICS for each service area provide: (a) Service Area (b) Type of Associated (c) Service Area Diagram (d) Service Area Description. Provide list of geographic areas (state postal codes or ITU 3-ltr codes), satellites or Figure No. of ID Station (Earth or File Name (GXT File) Service Area Diagram. Space) KNUL S North America and the Caribbean, -6 dB contour KNDL S North America and the Caribbean, -6 dB contour KSUL S South America and parts of the Caribbean, -6 dB contour KSDL S South America and parts of the Caribbean, -6 dB contour CUL S C-band payload off (If on, coverage would be North America), -6 dB contour CDL S C-band payload off (if on, coveage would be North America), -6 dB contour GBL S Hemispherical coverage

FEDERAL COMMUNICATIONS COMMISSION Page 4: Antenna Beams SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S7. SPACE STATION ANTENNA BEAM CHARACTERISTICS For each antenna beam provide: (a) (b) Isotropic Antenna (e) (f) (g) Min. (h) Polar- (i) Polarization (j) Service Transmit Receive Beam T/R Gain Pointing Rotational Cross- ization Alignment Rel. Area ID (k) (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Input Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) Losses Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) (db/K) (dBW/m2) KNR R 33.6 27.6 0.15 0 30 Y 90 KNUL 632 5.59 -98.6 18 1 KNR R 33.87 27.87 0.15 0 30 Y 0 KNUL 624 5.92 -98.9 18 1 KNT T 33.47 27.47 0.15 0 30 Y 90 KNDL 1.48 78 52.39 KNT T 33.6 27.6 0.15 0 30 Y 0 KNDL 1.53 77.1 52.47 KSR R 33.8 27.8 0.15 0 30 Y 90 KSUL 731 5.16 -98.2 18 1 KSR R 33.51 27.51 0.15 0 30 Y 0 KSUL 734 4.85 -97.8 18 1 KSTV T 32.43 26.43 0.15 0 30 Y 90 KSDL 1.62 75.5 51.21 KST T 32.35 26.35 0.15 0 30 Y 0 KSDL 1.84 71.8 50.91 CRV R 33 27 0.15 0 30 Y 90 CUL 567 5.46 -101.2 18 1 CRH R 32.66 26.66 0.15 0 30 Y 0 CUL 479 5.86 -101.6 18 1 CTV T 29.83 23.83 0.15 0 30 Y 90 CDL 1.11 15.5 41.72 CTH T 29.87 23.87 0.15 0 30 Y 0 CDL 1.35 14.6 41.52 GBL R 10 6.5 0.15 0 30 Y 90 GBL 600 -17 GBL R 10 6.5 0.15 0 30 Y 0 GBL 600 -17

FEDERAL COMMUNICATIONS COMMISSION Page 5: Beam Diagrams SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S8. ANTENNA BEAM DIAGRAMS For each beam pattern provide the reference to the graphic image and numerical data: Also provide the power flux density levels in each beam that result from the emission with the highest power flux density. (a) (b) (c) Co-or (d) GSO (e) NGSO Antenna Gain (f) GSO Antenna Max. Power Flux Density (dBW/M2/Hz) Beam T/R Cross Ref. Contour Description Gain Contour Data At Angle of Arrival above horizontal (for emission with highest PFD) ID Mode Polar Orbital (Figure/Table/ Exhibit) (GXT File) (g) 5 Deg (h) 10 Deg (i) 15 Deg (j) 20 Deg (k) 25 Deg Mode ("C" Longitude or" X") (Deg. E/W) KNR R C -67 KNRV.gxt KNR R C -67 KNRH.gxt KNT T C -67 KNTV.gxt -154.2 -153.7 -153.1 -152.5 -151.8 KNT T C -67 KNTH.gxt -154.9 -154.3 -153.6 -152.2 -150.9 KSR R C -67 KSRV.gxt KSR R C -67 KSRH.gxt KSTV T C -67 KSTV.gxt -173.6 -173 -171.1 -170.3 -169.6 KST T C -67 KSTH.gxt -172.2 -173.1 -171.3 -170.6 -169 CRV R C -67 CRV.gxt CRH R C -67 CRH.gxt CTV T C -67 CTV.gxt -163.2 -162.9 -162.5 -161.9 -161.5 CTH T C -67 CTH.gxt -163.8 -163.4 -163 -162.4 -161.8 GBL R C -67 GBL R C -67

FEDERAL COMMUNICATIONS COMMISSION Page 6: Channels and SATELLITE SPACE STATION AUTHORIZATIONS Transponders FCC Form 312 - Schedule S: (Technical and Operational Description) S9. SPACE STATION CHANNELS For each frequency channel provide: S10. SPACE STATION TRANSPONDERS For each transponder provide: (a) (B) Assigned (c) (d) Center (e) (f) TTC (a) (b) Receive Band Transmit Band Channel Bandwidth T/R Frequency Polarization or Comm Transponder Transponder (c) Channel (d) Beam (e) Channel (f) Beam ID No. (kHz) Mode (MHz) (H, V, L, R) Channel ID Gain (dB) No. ID No. (T or C) KNR01 36000 R 14020 H C KNN01 110.4 KNR01 KNRH KNT01 KNTV KNR02 36000 R 14040 V C KNN02 110.4 KNR02 KNRV KNT02 KNTH KNR03 36000 R 14060 H C KNN03 110.4 KNR03 KNRH KNT03 KNTV KNR04 36000 R 14080 V C KNN04 110.4 KNR04 KNRV KNT04 KNTH KNR05 36000 R 14100 H C KNN05 110.4 KNR05 KNRH KNT05 KNTV KNR06 36000 R 14120 V C KNN06 110.4 KNR06 KNRV KNT06 KNTH KNR07 36000 R 14140 H C KNN07 110.4 KNR07 KNRH KNT07 KNTV KNR08 36000 R 14160 V C KNN08 110.4 KNR08 KNRV KNT08 KNTH KNR09 36000 R 14180 H C KNN09 110.4 KNR09 KNRH KNT09 KNTV KNR10 36000 R 14200 V C KNN10 110.4 KNR10 KNRV KNT10 KNTH KNR11 36000 R 14220 H C KNN11 110.4 KNR11 KNRH KNT11 KNTV KNR12 36000 R 14240 V C KNN12 110.4 KNR12 KNRV KNT12 KNTH KNR13 36000 R 14260 H C KNN13 110.4 KNR13 KNRH KNT13 KNTV KNR14 36000 R 14280 V C KNN14 110.4 KNR14 KNRV KNT14 KNTH KNR15 36000 R 14300 H C KNN15 110.4 KNR15 KNRH KNT15 KNTV KNR16 36000 R 14320 V C KNN16 110.4 KNR16 KSRV KNT16 KNTH KNR17 36000 R 14340 H C KNN17 110.4 KNR17 KNRH KNT17 KNTV KNR18 36000 R 14360 V C KNN18 110.4 KNR18 KNRV KNT18 KNTH KNR19 36000 R 14380 H C KNN19 110.4 KNR19 KNRH KNT19 KNTV KNR20 36000 R 14400 V C KNN20 110.4 KNR20 KNRV KNT20 KNTH KNR21 36000 R 14420 H C KNN21 110.4 KNR21 KNRH KNT21 KNTV KNR22 36000 R 14440 V C KNN22 110.4 KNR22 KNRV KNT22 KNTH KNR23 36000 R 14460 H C KNN23 110.4 KNR23 KNRH KNT23 KNTV KNR24 36000 R 14480 V C KNN24 110.4 KNR24 KNRV KNT24 KNTH KNR25 72000 R 13875 H C KNN25 110.4 KNR25 KNRH KNT25 KNTV KNR26 72000 R 13875 V C KNN26 110.4 KNR26 KNRV KNT26 KNTH KNR27 72000 R 13955 H C KNN27 110.4 KNR27 KNRH KNT27 KNTV KNR28 72000 R 13955 V C KNN28 110.4 KNR28 KNRV KNT28 KNTH KNT01 36000 T 11720 V C KSS01 109.5 KSR01 KSRH KST01 KSTV KNT02 36000 T 11740 H C KSS02 109.5 KSR02 KSRV KST02 KSTH

KNT03 36000 T 11760 V C KSS03 109.5 KSR03 KSRH KST03 KSTV KNT04 36000 T 11780 H C KSS04 109.5 KSR04 KSRV KST04 KSTH KNT05 36000 T 11800 V C KSS05 109.5 KSR05 KSRH KST05 KSTV KNT06 36000 T 11820 H C KSS06 109.5 KSR06 KSRV KST06 KSTH KNT07 36000 T 11840 V C KSS07 109.5 KSR07 KSRH KST07 KSTV KNT08 36000 T 11860 H C KSS08 109.5 KSR08 KSRV KST08 KSTH KNT09 36000 T 11880 V C KSS09 109.5 KSR09 KSRH KST09 KSTV KNT10 36000 T 11900 H C KSS10 109.5 KSR10 KSRV KST10 KSTH KNT11 36000 T 11920 V C KSS11 109.5 KSR11 KSRH KST11 KSTV KNT12 36000 T 11940 H C KSS12 109.5 KSR12 KSRV KST12 KSTH KNT13 36000 T 11960 V C KSS13 109.5 KSR13 KSRH KST13 KSTV KNT14 36000 T 11980 H C KSS14 109.5 KSR14 KSRV KST14 KSTH KNT15 36000 T 12000 V C KSS15 109.5 KSR15 KSRH KST15 KSTV KNT16 36000 T 12020 H C KSS16 109.5 KSR16 KSRV KST16 KSTH KNT17 36000 T 12040 V C KSS17 109.5 KSR17 KSRH KST17 KSTV KNT18 36000 T 12060 H C KSS18 109.5 KSR18 KSRV KST18 KSTH KNT19 36000 T 12080 V C KSS19 109.5 KSR19 KSRH KST19 KSTV KNT20 36000 T 12100 H C KSS20 109.5 KSR20 KSRV KST20 KSTH KNT21 36000 T 12120 V C KSS21 109.5 KSR21 KSRH KST21 KSTV KNT22 36000 T 12140 H C KSS22 109.5 KSR22 KSRV KST22 KSTH KNT23 36000 T 12160 V C KSS23 109.5 KSR23 KSRH KST23 KSTV KNT24 72000 T 12180 H C KSS24 109.5 KSR24 KSRV KST24 KSTH KNT25 72000 T 11575 V C KSS25 109.5 KSR25 KSRH KST25 KSTV KNT26 72000 T 11575 H C KSS26 109.5 KSR26 KSRV KST26 KSTH KNT27 72000 T 11655 V C KSS27 109.5 KSR27 KSRH KST27 KSTV KNT28 72000 T 11655 H C KSS28 109.5 KSR28 KSRV KST28 KSTH KSR01 36000 R 14020 H C KNS01 110.2 KNR01 KNRH KST01 KSTV KSR02 36000 R 14040 V C KNS02 110.2 KNR02 KNRV KST02 KSTH KSR03 36000 R 14060 H C KNS03 110.2 KNR03 KNRH KST03 KSTV KSR04 36000 R 14080 V C KNS22 110.2 KNR22 KNRV KST22 KSTH KSR05 36000 R 14100 H C KNS23 110.2 KNR23 KNRH KST23 KSTV KSR06 36000 R 14120 V C KNS24 110.2 KNR24 KNRV KST24 KSTH KSR07 36000 R 14140 H C KNS25 110.2 KNR25 KNRH KST25 KSTV KSR08 36000 R 14160 V C KNS26 110.2 KNR26 KNRV KST26 KSTH KSR09 36000 R 14180 H C KNS27 110.2 KNR27 KNRH KST27 KSTV KSR10 36000 R 14200 V C KNS28 110.2 KNR28 KNRV KST28 KSTH KSR11 36000 R 14220 H C KSN01 109.7 KSR01 KSRH KNT01 KNTV KSR12 36000 R 14240 V C KSN02 109.7 KSR02 KSRV KNT02 KNTH KSR13 36000 R 14260 H C KSN03 109.7 KSR03 KSRH KNT03 KNTV

KSR14 36000 R 14280 V C KSN04 109.7 KSR04 KSRV KNT04 KNTH KSR15 36000 R 14300 H C KSN05 109.7 KSR05 KSRH KNT05 KNTV KSR16 36000 R 14320 V C KSN06 109.7 KSR06 KSRV KNT06 KNTH KSR17 36000 R 14340 H C KSN07 109.7 KSR07 KSRH KNT07 KNTV KSR18 36000 R 14360 V C KSN08 109.7 KSR08 KSRV KNT08 KNTH KSR19 36000 R 14380 H C KSN09 109.7 KSR09 KSRH KNT09 KNTV KSR20 36000 R 14400 V C KSN10 109.7 KSR10 KSRV KNT10 KNTH KSR21 36000 R 14420 H C KSN11 109.7 KSR11 KSRH KNT11 KNTV KSR22 36000 R 14440 V C KSN12 109.7 KSR12 KSRV KNT12 KNTH KSR23 36000 R 14460 H C KSN13 109.7 KSR13 KSRH KNT13 KNTV KSR24 36000 R 14480 V C KNS04 110.2 KNR04 KNRV KST04 KSTH KSR25 72000 R 13875 H C KNS05 110.2 KNR05 KNRH KST05 KSTV KSR26 72000 R 13875 V C KNS06 110.2 KNR06 KNRV KST06 KSTH KSR27 72000 R 13955 H C KNS07 110.2 KNR07 KNRH KST07 KSTV KSR28 72000 R 13955 V C KNS08 110.2 KNR08 KNRV KST08 KSTH KST01 36000 T 11720 V C KNS09 110.2 KNR09 KNRH KST09 KSTV KST02 36000 T 11740 H C KNS10 110.2 KNR10 KNRV KST10 KSTH KST03 36000 T 11760 V C KNS11 110.2 KNR11 KNRH KST11 KSTV KST04 36000 T 11780 H C KNS12 110.2 KNR12 KNRV KST12 KSTH KST05 36000 T 11800 V C KNS13 110.2 KNR13 KNRH KST13 KSTV KST06 36000 T 11820 H C KNS14 110.2 KNR14 KNRV KST14 KSTH KST07 36000 T 11840 V C KNS15 110.2 KNR15 KNRH KST15 KSTV KST08 36000 T 11860 H C KNS16 110.2 KNR16 KNRV KST16 KSTH KST09 36000 T 11880 V C KNS17 110.2 KNR17 KNRH KST17 KSTV KST10 36000 T 11900 H C KNS18 110.2 KNR18 KNRH KST18 KSTH KST11 36000 T 11920 V C KNS19 110.2 KNR19 KNRH KST19 KSTV KST12 36000 T 11940 H C KNS20 110.2 KNR20 KNRV KST20 KSTH KST13 36000 T 11960 V C KNS21 110.2 KNR21 KNRH KST21 KSTV KST14 36000 T 11980 H C KSN14 109.7 KSR14 KSRV KNT14 KNTH KST15 36000 T 12000 V C KSN15 109.7 KSR15 KSRH KNT15 KNTV KST16 36000 T 12020 H C KSN16 109.7 KSR16 KSRV KNT16 KNTH KST17 36000 T 12040 V C KSN17 109.7 KSR17 KSRH KNT17 KNTV KST18 36000 T 12060 H C KSN18 109.7 KSR18 KSRV KNT18 KNTH KST19 36000 T 12080 V C KSN19 109.7 KSR19 KSRH KNT19 KNTV KST20 36000 T 12100 H C KSN20 109.7 KSR20 KSRV KNT20 KNTH KST21 36000 T 12120 V C KSN21 109.7 KSR21 KSRH KNT21 KNTV KST22 36000 T 12140 H C KSN22 109.7 KSR22 KSRV KNT22 KNTH KST23 36000 T 12160 V C KSN23 109.7 KSR23 KSRH KNT23 KNTV KST24 36000 T 12180 H C KSN24 109.7 KSR24 KSRV KNT24 KNTH

KST25 72000 T 11575 V C KSN25 109.7 KSR25 KSRH KNT25 KNTV KST26 72000 T 11575 H C KSN26 109.7 KSR26 KSRV KNT26 KNTH KST27 72000 T 11655 V C KSN27 109.7 KSR27 KSRH KNT27 KNTV KST28 72000 T 11655 H C KSN28 109.7 KSR28 KSRV KNT28 KNTH CR01 36000 R 5945 H C C01 107.3 CR01 CRH CT01 CTV CR02 36000 R 5965 V C C02 106.3 CR02 CRV CT02 CTH CR03 36000 R 5985 H C C03 107.3 CR03 CRH CT03 CTV CR04 36000 R 6005 V C C04 106.3 CR04 CRV CT04 CTH CR05 36000 R 6025 H C C05 107.3 CR05 CRH CT05 CTV CR06 36000 R 6045 V C C06 106.3 CR06 CRV CT06 CTH CR07 36000 R 6065 H C C07 107.3 CR07 CRH CT07 CTV CR08 36000 R 6085 V C C08 106.3 CR08 CRV CT08 CTH CR09 36000 R 6105 H C C09 107.3 CR09 CRH CT09 CTV CR10 36000 R 6125 V C C10 106.3 CR10 CRV CT10 CTH CR11 36000 R 6145 H C C11 107.3 CR11 CRH CT11 CTV CR12 36000 R 6165 V C C12 106.3 CR12 CRV CT12 CTH CR13 36000 R 6185 H C C13 107.3 CR13 CRH CT13 CTV CR14 36000 R 6205 V C C14 106.3 CR14 CRV CT14 CTH CR15 36000 R 6225 H C C15 107.3 CR15 CRH CT15 CTV CR16 36000 R 6245 V C C16 106.3 CR16 CRV CT16 CTH CR17 36000 R 6265 H C C17 107.3 CR17 CRH CT17 CTV CR18 36000 R 6285 V C C18 106.3 CR18 CRV CT18 CTH CR19 36000 R 6305 H C C19 107.3 CR19 CRH CT19 CTV CR20 36000 R 6325 V C C20 106.3 CR20 CRV CT20 CTH CR21 36000 R 6345 H C C21 107.3 CR21 CRH CT21 CTV CR22 36000 R 6365 V C C22 106.3 CR22 CRV CT22 CTH CR23 36000 R 6385 H C C23 107.3 CR23 CRH CT23 CTV CR24 36000 R 6405 V C C24 106.3 CR24 CRV CT24 CTH CT01 36000 T 3720 V C C1 TC GBLRH CT02 36000 T 3740 H C T1 TM1 CTH CT03 36000 T 3760 V C T2 TM2 CTV CT04 36000 T 3780 H C T3 TM3 KNTH CT05 36000 T 3800 V C T4 TM4 KNTv CT06 36000 T 3820 H C CT07 36000 T 3840 V C CT08 36000 T 3860 H C CT09 36000 T 3880 V C CT10 36000 T 3900 H C CT11 36000 T 3920 V C

CT12 36000 T 3940 H C CT13 36000 T 3960 V C CT14 36000 T 3980 H C CT15 36000 T 4000 V C CT16 36000 T 4020 H C CT17 36000 T 4040 V C CT18 36000 T 4060 H C CT19 36000 T 4080 V C CT20 36000 T 4100 H C CT21 36000 T 4120 V C CT22 36000 T 4140 H C CT23 36000 T 4160 V C CT24 36000 T 4180 H C TC 800 R 6423.5 H T TM1 300 T 3700.5 H T TM2 300 T 4199.5 V T TM3 300 T 11702 H T TM4 300 T 12198 V T

FEDERAL COMMUNICATIONS COMMISSION Page 7: Digital Modulation SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S11. DIGITAL MODULATION PARAMETERS For each digital emission provide: (a) Digital (b) Emission (c) Assigned (d) No. of (e)Uncoded (f) FEC Error (g) CDMA (h) Total C/N (i) Single Entry Mod. ID Designator Bandwidth Phases Data Rate Correction Processing Performance C/I Objective (kHz) (kbps) Coding Rate Gain (dB) Objective (dB) (dB) A_KU 36M0G7W 36000 4 40000 0.69 6.4 18 B_KU 27M0G7W 27000 4 32000 0.69 6.4 18 C_KU 6M95G1W 6950 4 8000 0.69 6.4 18 D_KU 5M00G1W 5000 4 6000 0.69 6.4 18 E_KU 100KG1W 100 4 56 0.69 6.4 18 F_KU 1M60G1W 1600 4 1544 0.69 6.4 18 G_KU 36M7W 36000 8 50000 0.61 9.9 20 H_C 36M0G7W 36000 4 40000 0.69 6.8 18 I_C 6M95G1W 6950 4 8000 0.69 6.8 18 J_C 36M0G7W 36000 8 60000 0.61 9.9 22 K_C 36M7W 36000 16 110000 0.81 16.6 24 L_C 100KG1D 100 4 56 0.75 7.2 18 M_C 1M60G1D 1600 4 1544 0.75 7.2 18

FEDERAL COMMUNICATIONS COMMISSION Page 8: Analog Modulation SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S12. ANALOG MODULATION PARAMETERS For each analog emission provide: (a) (b) Emission (c) (d) Signal (e) Multi-channel Telephony (j) Video (k) Video (l) Video (m) SCPC/FM (n) Total C/N (o) Single Analog Designator Assigned Type Channels Standard Noise- and Compander, Performance Entry C/I (f) Ave. (g) Bottom (h) Top (i) RMS Mod. ID Bandwidth per Carrier NTSC, Weighting SCPC/FM Preemphasis, Objective Objective Companded Baseband Baseband Modulation (kHz) PAL, etc. (dB) Modulation and Noise (dB) (dB) Talker Level Freq. (MHz) Freq. (MHz) Index Index Weighting (dB) (dBm0) Q_C 800KF9D 800 1 10 21 R_C 300KF9D 300 1 9 21 S_KU 300KF9D 300 1 9 21 0

FEDERAL COMMUNICATIONS COMMISSION Page 9: Typical Emissions SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S13. TYPICAL EMISSIONS For each planned type of emission provide: Associated Modulation ID (e) Carriers (f) Carrier (g)Noise Budget (h) Energy Receive Band (Assoc. Transmit Stn) Transmit Band (This Space Station) Transponder ID Range per Spacing Reference (Table Dispersal (c) Digital (d) Analog (i)Assoc. Assoc. Station Transmit EIRP (dBW) (n) Max. (o)Assoc. Transponder (kHz) No.) Bandwidth (Table (Table S12) Stn. Max. Power (dBW) Power Flux Stn (a) Start (b) End (kHz) S11) Antenna Density Rec. G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dBW/m2/Hz) (dB/K) KNN01 KSN28 A_KU 1 Dig_Ku_budget 57.2 20 23 43.68 49.68 -151.9 17.1 KNN01 KSN28 B_KU 1 Dig_Ku_budget 57.2 20 23 43.68 49.68 -150.6 17.1 KNN01 KSN28 C_KU 5 6950 Dig_Ku_budget 52.9 8.9 12 30.68 36.68 -157.7 25.6 KNN01 KSN28 D_KU 6 5000 Dig_Ku_budget 52.9 8.9 12 29.68 35.68 -157.3 25.6 KNN01 KSN28 E_KU 250 100 Dig_Ku_budget 46.6 -5 -3 13.48 19.48 -156.5 19.6 KNN01 KSN28 F_KU 20 1544 Dig_Ku_budget 46.6 8 11 23.48 29.48 -158.6 25.6 KNN01 KSN28 G_KU 1 Dig_Ku_budget 57.2 20 23 43.68 49.68 -151.9 25.6 C01 C24 H_C 1 Dig_C_budgets 54.4 17.1 20.1 35.72 41.72 -159.4 21.8 C01 C24 I_C 5 Dig_C_budgets 54.4 9.6 15 25.98 31.98 -162.4 25.2 C01 C24 J_C 1 Dig_C_budgets 54.4 22 25 35.72 41.72 -159.4 33.2 C01 C24 K_C 1 Dig_C_budgets 54.4 22 25 35.72 41.72 -159.4 33.2 C01 C24 L_C 250 15 Dig_C_budgets 47.4 -3.4 2 5.98 11.98 -164 23 C01 C24 M_C 20 1544 Dig_C_budgets 47.4 11 16 23.2 29.2 -158.8 23 C1 C1 Q_C 1 TTC_budgets.xl 54.4 13 16 T1 T2 R_C 1 TTC_budgets.xl 14.3 18.3 -164.9 31 T3 T4 S_KU 1 TTC_budgets.xl 12.4 16.4 -164.7 38.3

FEDERAL COMMUNICATIONS COMMISSION Page 10: TT and C SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S14. Is the space station(s) controlled and monitored remotely? If Yes, provide the location and telephone number of the TT and C control point(s): #Error Remote Control (TT C) Location(s): S14a: Street Address: Woodbine TT&C S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Mt. Airy MD 21771 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 410-548-4300 E7169 Remote Control (TT C) Location(s): S14a: Street Address: Vernon Valley Spacecrafts Ops. S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Sussex NJ 07461 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 973-823-6000 WB81

FEDERAL COMMUNICATIONS COMMISSION Page 11: SATELLITE SPACE STATION AUTHORIZATIONS Characteristics and FCC Form 312 - Schedule S: (Technical and Operational Description) Certifications S15. SPACECRAFT PHYSICAL CHARACTERISTICS: S15a: Mass of spacecraft without fuel (kg): Spacecraft Dimensions Probability of Survival to 1764.6 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2144.3 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3908.9 20.8 0.744 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 640.6 7.6 0.86 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 69.2 5.4 0.64 S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: Spacecraft Electrical Power (Watts) At Electrical Power (Watts) At Subsystem Beginning of Life End of Life At Equinox At Solstice At Equinox At Solstice Payload (Watts): (a): (f): (k): (p): 7061 7061 2116 2304 Bus (Watts): (b): (g): (l): (q): 1397 771 2381 1641 Total (Watts): (c): (h): (m): (r): 8458 7832 4497 3945 Solar Array (Watts): (d): (i): (n): (s): 19775 11660 4518 4047 Depth of Battery (e) (j) (o) (t) Discharge (%): 73.1 % 7.1 % 73.1 % 73.1 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: X YES NO N/A b. Are the appropriate service area coverage requirements of § 25.143(b)(ii) and (iii), or § 25.145(c)(1) and (2) met? YES NO X N/A c. Are the frequency tolerances of § 25.202(e) and the out-of-band emission limits of § 25.202(f)(1), (2) and (3) met? X YES NO N/A In addition to the information required in this Form, the space station applicant is required to provide all the information specified in Section 25.114 of the Commission's rules, 47 C.F.R § 25.114.


Document Created: 2010-04-22 09:52:48
Document Modified: 2010-04-22 09:52:48
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