Attachment Schedule S Tech Data

This document pretains to SAT-PPL-20091222-00150 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2009122200150_791109

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: SES-1 4/20/2010 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 2/1/2007 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 2/10/2010 48 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: 3/15/2010 4/15/2010 1728 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) 14.00 G 14.50 G R Fixed Satellite Service 11.70 G 12.20 G T Fixed Satellite Service 14.00 G 14.50 G R Direct to Home in the Fixed Fixed Satellite Service 11.70 G 12.20 G T Direct to Home in the Fixed Fixed Satellite Service 5.925 G 6.425 G R Fixed Satellite Service 3.70 G 4.20 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: 101 W Nominal orbital location is that of AMC-2 which will be Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be replaced by SES-1 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) K-DL E CONUS, Alaska, Hawaii, and parts of Caribbean. K-UL E CONUS, Alaska, Hawaii and parts of Caribbean C-DL E CONUS, Alaska, Hawaii, Mexico, and parts of Caribbean C-UL E CONUS, Alaska, Hawaii, Mexico, and parts of Caribbean

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) CRH R 32.2 22.2 0.15 0 30 Y 0 C-UL 540 4.9 -100.2 21 1 CRV R 32.5 22.5 0.15 0 30 Y 90 C-UL 590 4.8 -100.1 21 1 KRH R 33.9 23.9 0.15 0 30 Y 0 K-UL 490 7 -100 21 1 KRV R 33.6 23.6 0.15 0 30 Y 90 K-UL 470 6.9 -100 21 1 CTH T 31.2 21.2 0.15 0 30 Y 0 C-DL 2.5 11 41.7 CTV T 31.1 21.1 0.15 0 30 Y 90 C-DL 2.5 11 41.6 KTH T 35.4 25.4 0.15 0 30 Y 0 K-DL 2.5 65 53.6 KTV T 34.4 24.4 0.15 0 30 Y 90 K-DL 2.5 50 52.3

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) CRH R C -101 CRH.gxt CRV R C -101 CRV.gxt KRH R C -101 KRH.gxt KRV R C -101 KRV.gxt CTH T C -101 CTH.gxt -156.2 -155.6 -154.8 -153.7 -152.5 CTV T C -101 CTV.gxt -156.3 -155.7 -154.9 -153.8 -152.6 KTH T C -101 KTH.gxt KTV T C -101 KTV.gxt

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) KR01 36000 R 14020 H C K01 119.5 KR01 KRH KT01 KTV KR02 36000 R 14040 V C K03 119.5 KR03 KRH KT03 KTV KR03 36000 R 14060 H C K05 119.5 KR05 KRH KT05 KTV KR04 36000 R 14080 V C K07 119.5 KR07 KRH KT07 KTV KR05 36000 R 14100 H C K09 119.5 KR09 KRH KT09 KTV KR06 36000 R 14120 V C K11 119.5 KR11 KRH KT11 KTV KR07 36000 R 14140 H C K13 119.5 KR13 KRH KT13 KTV KR08 36000 R 14160 V C K15 119.5 KR15 KRH KT15 KTV KR09 36000 R 14180 H C K17 119.5 KR17 KRH KT17 KTV KR10 36000 R 14200 V C K19 119.5 KR19 KRH KT19 KTV KR11 36000 R 14220 H C K21 119.5 KR21 KRH KT21 KTV KR12 36000 R 14240 V C K23 119.5 KR23 KRH KT23 KTV KR13 36000 R 14260 H C K02 119.5 KR02 KRV KT02 KTH KR14 36000 R 14280 V C K04 119.5 KR04 KRV KT04 KTH KR15 36000 R 14300 H C K06 119.5 KR06 KRV KT06 KTH KR16 36000 R 14320 V C K08 119.5 KR08 KRV KT08 KTH KR17 36000 R 14340 H C K10 119.5 KR10 KRV KT10 KTH KR18 36000 R 14360 V C K12 119.5 KR12 KRV KT12 KTH KR19 36000 R 14380 H C K14 119.5 KR14 KRV KT14 KTH KR20 36000 R 14400 V C K16 119.5 KR16 KRV KT16 KTH KR21 36000 R 14420 H C K18 119.5 KR18 KRV KT18 KTH KR22 36000 R 14440 V C K20 119.5 KR20 KRV KT20 KTH KR23 36000 R 14460 H C K22 119.5 KR22 KRV KT22 KTH KR24 36000 R 14480 V C K24 119.5 KR24 KRV KT24 KTH KT01 36000 T 11720 V C C01 105.5 CR01 CRH CT01 CTV KT02 36000 T 11740 H C C03 105.5 CR03 CRH CT03 CTV KT03 36000 T 11760 V C C05 105.5 CR05 CRH CT05 CTV KT04 36000 T 11780 H C C07 105.5 CR07 CRH CT07 CTV KT05 36000 T 11800 V C C09 105.5 CR09 CRH CT09 CTV KT06 36000 T 11820 H C C11 105.5 CR11 CRH CT11 CTV

KT07 36000 T 11840 V C C13 105.5 CR13 CRH CT13 CTV KT08 36000 T 11860 H C C15 105.5 CR15 CRH CT15 CTV KT09 36000 T 11880 V C C17 105.5 CR17 CRH CT17 CTV KT10 36000 T 11900 H C C19 105.5 CR19 CRH CT19 CTV KT11 36000 T 11920 V C C21 105.5 CR21 CRH CT21 CTV KT12 36000 T 11940 H C C23 105.5 CR23 CRH CT23 CTV KT13 36000 T 11960 V C C02 105.5 CR02 CRV CT02 CTH KT14 36000 T 11980 H C C04 105.5 CR04 CRV CT04 CTH KT15 36000 T 12000 V C C06 105.5 CR06 CRV CT06 CTH KT16 36000 T 12020 H C C08 105.5 CR08 CRV CT08 CTH KT17 36000 T 12040 V C C10 105.5 CR10 CRV CT10 CTH KT18 36000 T 12060 H C C12 105.5 CR12 CRV CT12 CTH KT19 36000 T 12080 V C C14 105.5 CR14 CRV CT14 CTH KT20 36000 T 12100 H C C16 105.5 CR16 CRV CT16 CTH KT21 36000 T 12120 V C C18 105.5 CR18 CRV CT18 CTH KT22 36000 T 12140 H C C20 105.5 CR20 CRV CT20 CTH KT23 36000 T 12160 V C C22 105.5 CR22 CRV CT22 CTH KT24 36000 T 12180 H C C24 105.5 CR24 CRH CT24 CTH CR01 36000 R 5945 H C X01 112.5 KR14 KRV CT14 CTH CR02 36000 R 5965 V C X02 112.5 KR16 KRV CT16 CTH CR03 36000 R 5985 H C X03 112.5 KR18 KRV CT18 CTH CR04 36000 R 6005 V C X04 112.5 KR20 KRV CT20 CTH CR05 36000 R 6025 H C X05 112.5 KR22 KRV CT22 CTH CR06 36000 R 6045 V C X06 112.5 KR24 KRV CT24 CTH CR07 36000 R 6065 H C X07 111 CR14 CRV KT14 KTH CR08 36000 R 6085 V C X08 111 CR16 CRV KT16 KTH CR09 36000 R 6105 H C X09 111 CR18 CRV KT18 KTH CR10 36000 R 6125 V C X10 111 CR20 CRV KT20 KTH CR11 36000 R 6145 H C X11 111 CR22 CRV KT22 KTH CR12 36000 R 6165 V C X12 111 CR24 CRV KT24 KTH CR13 36000 R 6185 H C TCC CC1 CRH CR14 36000 R 6205 V C TCK KUC1 KRV CR15 36000 R 6225 H C TBC1 CBCN1 CTH CR16 36000 R 6245 V C TBC2 CBCN2 CTV CR17 36000 R 6265 H C TBK1 KBCN1 KTV CR18 36000 R 6285 V C TBK2 KBCN2 KTH CR19 36000 R 6305 H C CR20 36000 R 6325 V C CR21 36000 R 6345 H C

CR22 36000 R 6365 V C CR23 36000 R 6385 H C CR24 36000 R 6405 V C CT01 36000 T 3720 V C CT02 36000 T 3740 H C CT03 36000 T 3760 V C CT04 36000 T 3780 H C CT05 36000 T 3800 V C 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 CC1 800 R 6423.5 H T KUC1 800 R 14499 V T CBCN1 400 T 3700.5 H T CBCN2 400 T 4199.5 V T KBCN1 400 T 11701 V T KBCN2 400 T 12199 H 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) K_A 36M0G7W 36000 4 40000 0.69 6.4 19 K_B 27M0G7W 27000 4 32000 0.69 6.4 19 K_C 6M95G1W 6950 4 8000 0.69 6.4 19 K_D 5M00G1W 5000 4 6000 0.69 6.4 19 K_E 100KG1W 100 4 56 0.69 6.4 19 K_F 1M60G1W 1600 4 1544 0.69 6.4 19 K_G 36M0G7W 36000 8 50000 0.61 9.9 20 C_A 36M0G7W 36000 4 40000 0.69 6.4 19 C_B 27M0G7W 27000 4 32000 0.69 6.4 19 C_C 6M95G1W 6950 4 8000 0.69 6.4 19 C_D 5M00G1W 5000 4 6000 0.69 6.4 19 C_E 100KG1W 100 4 56 0.69 6.4 19 C_F 1M60G1W 1600 4 1544 0.69 6.4 19 C_G 36M0G7W 36000 8 50000 0.61 9.9 20

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) K_H 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 11 20 C_H 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 11 20 K_TC 800KF9D 800 10 20 K_TM 400KF9D 400 10 20 C_TC 800KF9D 800 10 20 C_TM 400KF9D 400 10 20

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) K01 K24 K_A 1 Link budgets.xl 57.2 20 25 47.4 51.8 -149.9 17.1 K01 K24 K_B 1 Link budgets.xl 57.2 20 25 47.4 51.8 -148.6 17.1 K01 K24 K_C 5 6950 Link budgets.xl 52.9 8.9 14 33.7 36.7 -157.8 25.6 K01 K24 K_D 6 5000 Link budgets.xl 52.9 8.9 14 32.3 35.3 -157.8 25.6 K01 K24 K_E 250 100 Link budgets.xl 46.6 -2 3 16.5 19.5 -156.6 19.6 K01 K24 K_F 20 1544 Link budgets.xl 46.6 8 13 26.5 29.5 -158.6 25.6 K01 K24 K_G 1 Link budgets.xl 57.2 20 25 47.4 51.8 -149.9 25.6 C01 C24 C_A 1 Link budgets.xl 53.2 25.1 30 35 41.7 -160 21.8 C01 C24 C_B 1 Link budgets.xl 53.2 20 25 35 41.7 -158.7 21.8 C01 C24 C_C 5 6950 Link budgets.xl 53.2 9.6 14 23.8 30.8 -163.7 21.8 C01 C24 C_D 6 5000 Link budgets.xl 53.2 12 17 23.8 30.8 -162.3 21.8 C01 C24 C_E 250 100 Link budgets.xl 47.2 -3.4 1.6 4.8 11 -165.1 21.8 C01 C24 C_F 20 1544 Link budgets.xl 47.2 11.8 16 20 27 -161.1 21.8 C01 C24 C_G 1 Link budgets.xl 53.2 25.1 30 35 41.7 -160 21.8 K01 K24 K_H 1 Link budgets.xl 2000 57.2 21 25 47.4 51.8 -137 19.6 C01 C24 C_H 1 Link budgets.xl 2000 53.2 23 27 35 41.7 -147.4 21.8 TCK TCK K_TC 1 Link budgets.xl 59.5 10 15 TCC TCC C_TC 1 Link budgets.xl 56 10 15 TBK1 TBK2 K_TM 1 Link budgets.xl 17 27 -155.1 33.2 TBC1 TBC2 C_TM 1 Link budgets.xl 12 22 -160.1 23

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): 410-549-4300 E7169 Remote Control (TT C) Location(s): S14a: Street Address: Vernon Valley Spacecraft Operations 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 1378 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1822 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3200 23.5 0.94 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 619 7.7 0.88 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 39 3.9 0.83 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): 4916 4916 4916 4916 Bus (Watts): (b): (g): (l): (q): 429 361 467 375 Total (Watts): (c): (h): (m): (r): 5345 5277 5383 5291 Solar Array (Watts): (d): (i): (n): (s): 7312 6561 6265 5720 Depth of Battery (e) (j) (o) (t) Discharge (%): 15 % 12.6 % 10.9 % 19.1 % 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: 2009-12-23 11:54:46
Document Modified: 2009-12-23 11:54:46
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