Attachment Sched S Tech Report.

This document pretains to SAT-LOA-20160915-00089 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2016091500089_1150026

Approved by OMD Control Number 3060-0678 Estimated Burden Hours: 80 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: Intelsat 37e N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 20 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 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: 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 f. Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode 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) 5850 M 5925 M R Fixed Satellite Service 5925 M 6425 M R Fixed Satellite Service 6425 M 6525 M R Fixed Satellite Service 6525 M 6650 M R Fixed Satellite Service 3400 M 3500 M T Fixed Satellite Service 3500 M 3550 M T Fixed Satellite Service 3550 M 3600 M T Fixed Satellite Service 3600 M 3650 M T Fixed Satellite Service 3650 M 3700 M T Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 13 G 13.25 G R Fixed Satellite Service 13.75 G 14 G R Fixed Satellite Service 14 G 14.2 G R Fixed Satellite Service 14.2 G 14.47 G R Fixed Satellite Service 14.47 G 14.5 G R Fixed Satellite Service 10.7 G 11.7 G T Fixed Satellite Service 11.7 G 11.95 G T Fixed Satellite Service

12.5 G 12.7 G T Fixed Satellite Service 12.7 G 12.75 G T Fixed Satellite Service 18.3 G 18.6 G T Fixed Satellite Service 18.6 G 18.8 G T Fixed Satellite Service 19.7 G 20.2 G T Fixed Satellite Service 28.35 G 28.85 G R Fixed Satellite Service 29.5 G 30 G R 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: 18 W Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be 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 Angle (o) Other Plane (Seconds) Node (Deg.) (Degrees) 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) 1 S Africa and Europe 2 S Central Africa 3 S Latin America 4 S Europe 5 S North America 6 S South America 7 S Falkland 8 S Africa, Europe, Middle East, South America,North America, & Asia 9 S Europe, Middle East, & Asia 10 S Algeria 11 S Central Atlantic 12 S Africa, South America, Europe 13 S GLOBAL

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) Input (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Losses Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) (dB) Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dBW) Temp (k) (db/K) (dBW/m2) CELD T 1 1 0.07 0.24 24 N 1 43.3 CER T 1 1 0.07 0.24 24 N 1 43.3 KZH T 1 1 0.07 0.24 24 N 0 10 51.5 C1LD T 1 1 0.07 0.24 24 N 4 52.1 C1R T 1 1 0.07 0.24 24 N 4 52.1 C2LD T 1 1 0.07 0.24 24 N 5 52.1 C2R T 1 1 0.07 0.24 24 N 5 52.1 C3LD T 1 1 0.07 0.24 24 N 6 51.8 C3R T 1 1 0.07 0.24 24 N 6 51.8 C4LD T 1 1 0.07 0.24 24 N 7 51.4 CALD T 1 1 0.07 0.24 24 N 2 47.9 CAR T 1 1 0.07 0.24 24 N 2 47.9 CGL T 1 1 0.07 0.24 24 N 13 38 CGR T 1 1 0.07 0.24 24 N 13 38 KUH T 1 1 0.07 0.24 24 N 08 51 KUV T 1 1 0.07 0.24 24 N 90 8 51 K56D T 1 1 0.07 0.24 24 N 90 11 50.3 KSH T 1 1 0.07 0.24 24 N 0 13 56 KSV T 1 1 0.07 0.24 24 N 90 13 56 KGH T 1 1 0.07 0.24 27 N 0 12 50.8 KGV T 1 1 0.07 0.24 27 N 90 12 50.8 ASLD T 1 1 0.07 0.24 27 N 13 58 ASR T 1 1 0.07 0.24 27 N 13 58 CML T 1 1 0.07 0.24 27 N 6 46.5 CMR T 1 1 0.07 0.24 27 N 6 46.5 THR T 1 1 0.07 0.24 22 N 13 -1.6 TPR T 1 1 0.07 0.24 22 N 13 6.4 TGH T 1 1 0.07 0.24 22 N 0 13 7.9 CLVD T 1 1 0.07 0.24 22 N 90 13 11

KLRD T 1 1 0.07 0.24 24 N 13 14 ALVD T 1 1 0.07 0.24 24 N 90 13 19.5 CELU R 1 1 0.07 0.24 27 N 1 -1 -108 1 1 CER R 1 1 0.07 0.24 27 N 1 -1 -106 1 1 KZVU R 1 1 0.07 0.24 24 N 90 10 12 -116.3 1 1 C1LU R 1 1 0.07 0.24 27 N 4 13 -110 1 1 C1R R 1 1 0.07 0.24 27 N 4 13 -110 1 1 C2LU R 1 1 0.07 0.24 27 N 5 13 -110 1 1 C2R R 1 1 0.07 0.24 27 N 5 13 -110 1 1 C3LU R 1 1 0.07 0.24 27 N 6 12 -110.1 1 1 C3R R 1 1 0.07 0.24 27 N 6 12 -110.1 1 1 C4R R 1 1 0.07 0.24 27 N 7 12 -109.3 1 1 CALU R 1 1 0.07 0.24 27 N 2 3 -106.1 1 1 CAR R 1 1 0.07 0.24 27 N 2 3 -106.1 1 1 CGL R 1 1 0.07 0.24 24 N 13 -6 -106.8 1 1 CGR R 1 1 0.07 0.24 24 N 13 -6 -106.8 1 1 KUV R 1 1 0.07 0.24 24 N 90 8 14 -114 1 1 KUH R 1 1 0.07 0.24 24 N 08 14 -114 1 1 K56U R 1 1 0.07 0.24 24 N 0 11 10 -113.9 1 1 KSH R 1 1 0.07 0.24 24 N 0 13 12 -113.2 1 1 KSV R 1 1 0.07 0.24 24 N 90 13 12 -113.2 1 1 KGV R 1 1 0.07 0.24 24 N 90 12 14 -113.8 1 1 KGH R 1 1 0.07 0.24 24 N 0 12 14 -113.8 1 1 ASLU R 1 1 0.07 0.24 27 N 13 11 -96.8 1 1 ASR R 1 1 0.07 0.24 27 N 13 11 -96.8 1 1 CML R 1 1 0.07 0.24 27 N 6 1 -104.3 1 1 CMR R 1 1 0.07 0.24 27 N 6 1 -104.3 1 1 CPLU R 1 1 0.07 0.24 22 N 13 -80 1 1 CHL R 1 1 0.07 0.24 22 N 13 -80 1 1 CGV R 1 1 0.07 0.24 22 N 90 13 -75 1 1

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) CELD T -18 -154.6 -154.5 -154.4 -154.3 -154.2 CER T -18 -154.6 -154.5 -154.4 -154.3 -154.2 KZH T -18 -150 -149.9 -149.8 -149.7 -149.6 C1LD T -18 -154.6 -154.5 -154.4 -154.3 -154.2 C1R T -18 -154.6 -154.5 -154.4 -154.3 -154.2 C2LD T -18 -154.6 -154.5 -154.4 -154.3 -154.2 C2R T -18 -154.6 -154.5 -154.4 -154.3 -154.2 C3LD T -18 -154.6 -154.5 -154.4 -154.3 -154.2 C3R T -18 -154.6 -154.5 -154.4 -154.3 -154.2 C4LD T -18 -154.6 -154.5 -154.4 -154.3 -154.2 CALD T -18 -154.6 -154.5 -154.4 -154.3 -154.2 CAR T -18 -154.6 -154.5 -154.4 -154.3 -154.2 CGL T -18 -160.3 -160.2 -160.1 -160 -159.9 CGR T -18 -160.3 -160.2 -160.1 -160 -159.9 KUH T -18 -150 -149.9 -149.8 -149.7 -149.6 KUV T -18 -150 -149.9 -149.8 -149.7 -149.6 K56D T -18 -150 -149.9 -149.8 -149.7 -149.6 KSH T -18 -150 -149.9 -149.8 -149.7 -149.6 KSV T -18 -150 -149.9 -149.8 -149.7 -149.6 KGH T -18 -150 -149.9 -149.8 -149.7 -149.6 KGV T -18 -150 -149.9 -149.8 -149.7 -149.6 ASLD T -18 -119.3 -119.2 -119.1 -119 -118.9 ASR T -18 -119.3 -119.2 -119.1 -119 -118.9 CML T -18 -154.6 -154.5 -154.4 -154.3 -154.2 CMR T -18 -154.6 -154.5 -154.4 -154.3 -154.2 THR T -18 -183.7 -183.6 -183.4 -183.3 -183.2 TPR T -18 -180.7 -180.6 -180.4 -180.3 -180.2 TGH T -18 -171.2 -171.1 -170.9 -170.8 -170.7

CLVD T -18 -162.1 -162 -161.9 -161.7 -161.6 KLRD T -18 -157.3 -152.2 -152.1 -151.9 -151.8 ALVD T -18 -127.8 -128.2 -128.1 -128 -127.9 CELU R -18 CER R -18 KZVU R -18 C1LU R -18 C1R R -18 C2LU R -18 C2R R -18 C3LU R -18 C3R R -18 C4R R -18 CALU R -18 CAR R -18 CGL R -18 CGR R -18 KUV R -18 KUH R -18 K56U R -18 KSH R -18 KSV R -18 KGV R -18 KGH R -18 ASLU R -18 ASR R -18 CML R -18 CMR R -18 CPLU R -18 CHL R -18 CGV R -18

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 (T ID Gain (dB) No. ID No. or C) AFCLU 226550 R 6208.025 L C C1 1 AFCLU CELU AFCRU 213500 R 6209.4 R C C2 1 AFCRU CERU CAFLU 213500 R 5975 L C C3 1 CAFLU CALU CAFRU 213500 R 5975 R C C4 1 CAFRU CARU LAMLU 213500 R 5975 L C C5 1 LAMLU CMLU LAMRU 213500 R 5975 R C C6 1 LAMRU CMRU C1L1U 213500 R 5975 L C C7 1 C1L1U C1LU C1L3U 182300 R 6547.9 L C C8 1 C1L3U C1LU C1R2U 213500 R 5975 R C C9 1 C1R2U C1RU C1R4U 182300 R 6547.9 R C C10 1 C1R4U C1RU C2L1U 132800 R 6254.9 L C C11 1 C2L1U C2LU C2L3U 70300 R 6129.9 L C C12 1 C2L3U C2LU C2R2U 213500 R 6209.4 R C C13 1 C2R2U C2RU C3L1U 213500 R 6209.4 L C C14 1 C3L1U C3LU C3R2U 213500 R 6209.4 R C C15 1 C3R2U C3RU C4R1U 213500 R 6209.4 R C C16 1 C4R1U C4RU GCL1U 75500 R 6374.7 L C C17 1 GCL1U CGLU GCR2U 75500 R 6374.7 R C C18 1 GCR2U CGRU AFCRD 231700 T 3983.9 R C C19 1 AFCRD CERD AFCLD 231700 T 3983.9 L C C20 1 AFCLD CELD CAFRD 229100 T 3744.6 R C C21 1 CAFRD CARD CAFLD 229100 T 3744.6 L C C22 1 CAFLD CALD LAMRD 229100 T 3744.6 R C C23 1 LAMRD CMRD LAMLD 151000 T 3783.65 L C C24 1 LAMLD CMLD C1R1D 411400 T 3634.4 R C C25 1 C1R1D C1RD C1L2D 411400 T 3634.4 L C C26 1 C1L2D C1LD C2R1D 210900 T 3980.5 R C C27 1 C2R1D C2RD C2L2D 210900 T 3980.5 L C C28 1 C2L2D C2LD C3R1D 210900 T 3980.5 R C C29 1 C3R1D C3RD C3L2D 210900 T 3980.5 L C C30 1 C3L2D C3LD

C4L1D 210900 T 3980.5 L C C31 1 C4L1D C4LD GCRD 83400.000 T 4147.95 R C C32 1 GCRD CGRU GCLD 83400.000 T 4147.95 L C C33 1 GCLD CGLU KG1VU 250000 R 13125 V C K1 1 KG1VU KGVU KG1HU 250000 R 13125 H C K2 1 KG1HU KGHU KG2VU 250000 R 13875 V C K3 1 KG2VU KGVU KG2HU 250000 R 13875 H C K4 1 KG2HU KGHU KSH1U 109400 R 13065.1 H C K5 1 KSH1U KSHU KSV1U 109400 R 13065.1 V C K6 1 KSV1U KSVU KSH2U 441000 R 14250 H C K7 1 KSH2U KSHU KSV2U 441000 R 14250 V C K8 1 KSV2U KSVU K1HU 125000 R 14062.5 H C K9 1 K1HU KUHU K1VU 125000 R 14062.5 V C K10 1 K1VU KUVU K2HU 125000 R 14125 H C K11 1 K2HU KUHU K2VU 125000 R 14125 V C K12 1 K2VU KUVU K3HU 125000 R 14187.5 H C K13 1 K3HU KUHU K3VU 125000 R 14187.5 V C K14 1 K3VU KUVU K4HU 125000 R 14250 H C K15 1 K4HU KUHU K4VU 125000 R 14250 V C K16 1 K4VU KUVU K5HU 125000 R 14312.5 H C K17 1 K5HU KUHU K5VU 125000 R 14312.5 V C K18 1 K5VU KUVU K6HU 125000 R 14375 H C K19 1 K6HU KUHU K6VU 125000 R 14375 V C K20 1 K6VU KUVU K7HU 125000 R 14437.5 H C K21 1 K7HU KUHU K7VU 125000 R 14437.5 V C K22 1 K7VU KUVU K8HU 125000 R 14500 H C K23 1 K8HU KUHU K8VU 125000 R 14500 V C K24 1 K8VU KUVU AlgKV 164100 R 14095 V C K25 1 AlgKV KZVU K56HU 109400 R 14184.9 H C K26 1 K56HU K56U KG1VD 250000 T 11575 V C K27 1 KG1VD KGVD KG1HD 125000 T 10887.5 H C K28 1 KG1HD KGHD KG2VD 250000 T 11325 V C K29 1 KG2VD KGVD KG2HD 250000 T 11325 H C K30 1 KG2HD KGHD KSV2D 109400 T 11009.9 V C K31 1 KSV2D KSVD KSH3D 218700 T 11580.2 H C K32 1 KSH3D KSHD KSV3D 218700 T 11580.2 V C K33 1 KSV3D KSVD KSV1D 109400 T 10765.1 V C K34 1 KSV1D KSVD KSH1D 109400 T 10765.1 H C K35 1 KSH1D KSHD K1HD 125000 T 11012.5 H C K36 1 K1HD KUHD

K1VD 125000 T 11012.5 V C K37 1 K1VD KUVD K2HD 125000 T 11075 H C K38 1 K2HD KUHD K2VD 125000 T 11075 V C K39 1 K2VD KUVD K3HD 125000 T 11137.5 H C K40 1 K3HD KUHD K3VD 125000 T 11137.5 V C K41 1 K3VD KUVD K4HD 125000 T 11200 H C K42 1 K4HD KUHD K4VD 125000 T 11200 V C K43 1 K4VD KUVD K5HD 125000 T 11512.5 H C K44 1 K5HD KUHD K5VD 125000 T 11512.5 V C K45 1 K5VD KUVD K6HD 125000 T 11575 H C K46 1 K6HD KUHD K6VD 125000 T 11575 V C K47 1 K6VD KUVD K7HD 125000 T 11637.5 H C K48 1 K7HD KUHD K7VD 125000 T 11637.5 V C K49 1 K7VD KUVD K8HD 125000 T 11700 H C K50 1 K8HD KUHD K8VD 125000 T 11700 V C K51 1 K8VD KUVD K9HD 125000 T 11762.5 H C K52 1 K9HD KUHD K9VD 125000 T 11762.5 V C K53 1 K9VD KUVD K10HD 125000 T 11825 H C K54 1 K10HD KUHD K10VD 125000 T 11825 V C K55 1 K10VD KUVD K11HD 125000 T 11887.5 H C K56 1 K11HD KUHD K11VD 125000 T 11887.5 V C K57 1 K11VD KUVD K12HD 125000 T 12437.5 H C K58 1 K12HD KUHD K12VD 125000 T 12437.5 V C K59 1 K12VD KUVD K13HD 125000 T 12500 H C K60 1 K13HD KUHD K13VD 125000 T 12500 V C K61 1 K13VD KUVD K14HD 125000 T 12562.5 H C K62 1 K14HD KUHD K14VD 125000 T 12562.5 V C K63 1 K14VD KUVD K15HD 125000 T 12625 H C K64 1 K15HD KUHD K15VD 125000 T 12625 V C K65 1 K15VD KUVD K16HD 125000 T 12687.5 H C K66 1 K16HD KUHD K16VD 125000 T 12687.5 V C K67 1 K16VD KUVD AlgKH 164100 T 11039.8 H C K68 1 AlgKH KZHD K56VD 109400 T 11009.9 V C K69 1 K56VD K56D KaL1U 440100 R 29750 L C K70 1 KaL1U ASLU KaR1U 440100 R 29750 R C K71 1 KaR1U ASRU KaL2U 440100 R 28600 L C K72 1 KaL2U ASLU KaR2D ASRD KaR2U 440100 R 28600 R C K73 1 KaR2U ASRU KaL2D ASLD KaR1D 440100 T 19950 R C K74 1 KaR1D ASRD KaL1D 440100 T 19950 L C K75 1 KaL1D ASLD

KaR2D 440100 T 18550 R C KaL2D 440100 T 18550 L C TLM1 500 T 4197.75 H T TLM2 500 T 4199.25 H T TLM3 500 T 4198.25 H T TLM4 500 T 4198.75 H T TLM5 500 T 4197.75 R T TLM6 500 T 4199.25 R T TLM7 500 T 4198.25 R T TLM8 500 T 4198.75 R T CMDV 3700 R 6423.25 V T CMDP 3700 R 6423.25 L T CMDH 3700 R 5851.75 L T ULPC1 25 T 4199.75 V T ULPC2 25 T 11199 R T ULPC3 25 T 11451.5 R T ULPC4 25 T 12501 R T ULPC5 25 T 20199.5 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) D1 36M0G7W 36000 D2 9M00G7W 9000 D3 1M43G7W 1434 D4 820KG7W 820 D5 10M3G7W 10300 D7 400KG7W 400 D6 1M45G7W 1450

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)

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. Power (o)Assoc. Transponder (kHz) No.) Bandwidth (Table S11) (Table S12) Stn. Max. Power (dBW) Flux Density Stn Rec. (a) Start (b) End (kHz) Antenna (dBW/m2/Hz) G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dB/K) C1 C6 D1 41.3 C1 C6 D2 35.8 C1 C6 D3 27.1 C1 C6 D4 25 C19 C24 D1 C19 C24 D2 C19 C24 D3 C19 C24 D4 C17 C18 D1 38 C17 C18 D2 35.8 C17 C18 D3 27.1 C17 C18 D4 25 C31 C33 D1 C31 C33 D2 C31 C33 D3 C31 C33 D4 C7 C16 D1 41.3 C7 C16 D2 35.8 C7 C16 D3 27.1 C7 C16 D4 25 C25 C31 D1 C25 C31 D2 C25 C31 D3 C25 C31 D4 K27 K69 D1 52.3 K27 K69 D2 46.8 K27 K69 D3 38.1 K27 K69 D4 36 K9 K26 D1

K9 K26 D2 K9 K26 D3 K9 K26 D4 K72 K75 D1 44.5 K72 K75 D2 34.9 K72 K75 D3 24.1 K72 K75 D4 15.8 K70 K71 D1 K70 K71 D2 K70 K71 D3 K70 K71 D4

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): Yes

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: S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: 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. FCC NOTICE REQUIRED BY THE PAPERWORK REDUCTION ACT The public reporting estimate for this collection of information includes the time for reviewing instructions, searching existing data sources, gathering and maintaining the required data, and completing and reviewing the collection of information. If you have any comments on this burden estimate, or how we can improve the collection and reduce the burden it causes you, please write to the Federal Communications Commission, AMD-PERM, Paperwork Reduction Project (3060-0678), Washington, DC 20554. We will also accept your comments regarding the Paperwork Reduction Act aspects of this collection via the Internet if you send them to PERM@fcc.gov. PLEASE DO NOT SEND COMPLETED FORMS TO THIS ADDRESS. Remember - You are not required to respond to a collection of information sponsored by the Federal government, and the government may not conduct or sponsor this collection, unless it displays a currently valid OMB control number or if we fail to provide you with this notice. This collection has been assigned an OMB control number of 3060-0678. THE FOREGOING NOTICE IS REQUIRED BY THE PAPERWORK REDUCTION ACT OF 1995, PUBLIC LAW 104-13, OCTOBER 1, 1995, 44 U.S.C. SECTION 3507.


Document Created: 2016-09-16 09:17:38
Document Modified: 2016-09-16 09:17:38
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