Attachment Sched S Tech Report

This document pretains to SES-MFS-20110707-00793 for Modification w/ Foreign Satellite (earth station) on a Satellite Earth Station filing.

IBFS_SESMFS2011070700793_905290

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: QUETZSAT-1 10/7/2011 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 2/4/2009 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 7/12/2011 32 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: 8/1/2011 8/31/2011 768 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) 17300 M 17800 M R Feeder Link for Broadcasting Satellite Service in FSS 12200 M 12700 M T Broadcasting Satellite Service - Video 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: 77 W Licensed by the Mexican Administration at this orbital Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be location 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) NA S CONUS, Puerto Rico, Mexico, Central America CHEYENNE S Area around Cheyenne, WY GILBERT S Area around Gilbert, AZ MEX S Area around Mexico City GLOBAL S Visible Earth

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) RRC R 44.9 41.9 0.12 0.2 27 N CHEYENN 1549 13 -105.8 21 1 RRG R 44.7 41.7 0.12 0.2 27 N GILBERT 1542 12.8 -105.6 21 1 RRM R 43.2 40.2 0.12 0.2 27 N MEX 2296 9.6 -102.4 21 1 RLC R 44.9 41.9 0.12 0.2 27 N CHEYENN 1762 12.4 -105.2 21 1 RLG R 44.6 41.6 0.12 0.2 27 N GILBERT 1774 12.2 -105 21 1 RLM R 43.2 40.2 0.12 0.2 27 N MEX 2523 9.2 -102 21 1 TEL T 35.7 25.7 0.12 0.2 27 N NA 2.5 155 57.6 TER T 35.6 25.6 0.12 0.2 27 N NA 2.5 155 57.5 TWL T 35.6 25.6 0.12 0.2 27 N NA 2.5 155 57.5 TWR T 35.5 25.5 0.12 0.2 27 N NA 2.5 155 57.4 TCO R 3 -2.5 0.12 0.2 30 Y MEX 4467 -33.5 -90 TMO T 35.5 29.5 0.12 0.2 27 Y MEX 7.6 0.1 24.4

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) RRC R C -77 uplink_Ch_R_RRC.gxt RRG R C -77 uplink_Gi_R_RRG.gxt RRM R C -77 uplink_Mx_R_RRM.gxt RLC R C -77 uplink_Ch_L_RLC.gxt RLG R C -77 uplink_Gi_L_RLG.gxt RLM R C -77 uplink_MX_L_RLM.gxt TEL T C -77 Downlink_16_TEL.gxt TER T C -77 Downlink_17_TER.gxt TWL T C -77 Downlink_18_TWL.gxt TWR T C -77 Downlink_15_TWR.gxt TMO T C -77

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) RO1 24000 R 17324.0 R C CMDA CMD1 TCO R02 24000 R 17338.58 L C CMDB CMD2 TCO R03 24000 R 17353.16 R C TLMA TLM1 TMO R04 24000 R 17367.74 L C TLMB TLM2 TMO R05 24000 R 17382.32 R C TLMC TLM3 TMO R06 24000 R 17396.90 L C TLMD TLM4 TMO R07 24000 R 17411.48 R C C01 114.5 RO1 RRC T01 TER R08 24000 R 17426.06 L C C02 113.9 R02 RLC T02 TWL R09 24000 R 17440.64 R C CO3 114.5 R03 RRC T03 TWR R10 24000 R 17455.22 L C C04 113.9 R04 RLC T04 TEL R11 24000 R 17469.80 R C C05 114.5 R05 RRC T05 TER R12 24000 R 17484.38 L C C06 113.9 R06 RLC T06 TWL R13 24000 R 17498.96 R C C07 114.5 R07 RRC T07 TWR R14 24000 R 17513.54 L C C08 113.9 R08 RLC T08 TEL R15 24000 R 17528.12 R C C09 114.5 R09 RRC T09 TER R16 24000 R 17542.70 L C C10 113.9 R10 RLC T10 TWL R17 24000 R 17557.28 R C C11 114.5 R11 RRC T11 TWR R18 24000 R 17571.86 L C C12 113.9 R12 RLC T12 TEL R19 24000 R 17586.44 R C C13 114.5 R13 RRC T13 TER R20 24000 R 17601.02 L C C14 113.9 R14 RLC T14 TWL R21 24000 R 17615.60 R C C15 114.5 R15 RRC T15 TWR R22 24000 R 17630.18 L C C16 113.9 R16 RLC T16 TEL R23 24000 R 17644.76 R C C17 114.5 R17 RRC T17 TER R24 24000 R 17659.34 L C C18 113.9 R18 RLC T18 TWL R25 24000 R 17673.92 R C C19 114.5 R19 RRC T19 TWR R26 24000 R 17688.50 L C C20 113.9 R20 RLC T20 TEL R27 24000 R 17703.08 R C C21 114.5 R21 RRC T21 TER R28 24000 R 17717.66 L C C22 113.9 R22 RLC T22 TWL R29 24000 R 17732.24 R C C23 114.5 R23 RRC T23 TWR R30 24000 R 17746.82 L C C24 113.9 R24 RLC T24 TEL

R31 24000 R 17761.40 R C C25 114.5 R25 RRC T25 TEL R32 24000 R 17775.98 L C C26 113.9 R26 RLC T26 TWL T01 24000 T 12224.00 R C C27 114.5 R27 RRC T27 TWR T02 24000 T 12238.58 L C C28 113.9 R28 RLC T28 TEL T03 24000 T 12253.16 R C C29 114.5 R29 RRC T29 TER T04 24000 T 12267.74 L C C30 113.9 R30 RLC T30 TWL T05 24000 T 12282.32 R C C31 114.5 R31 RRC T31 TWR T06 24000 T 12296.90 L C C32 113.9 R32 RLC T32 TEL T07 24000 T 12311.48 R C G01 114.3 RO1 RRG T01 TER T08 24000 T 12326.06 L C G02 113.7 R02 RLG T02 TWL T09 24000 T 12340.64 R C G03 114.3 R03 RRG T03 TWR T10 24000 T 12355.22 L C G04 113.7 R04 RLG T04 TEL T11 24000 T 12369.80 R C G05 114.3 R05 RRG T05 TER T12 24000 T 12384.38 L C G06 113.7 R06 RLG T06 TWL T13 24000 T 12398.96 R C G07 114.3 R07 RRG T07 TWR T14 24000 T 12413.54 L C G08 113.7 R08 RLG T08 TEL T15 24000 T 12428.12 R C G09 114.3 R09 RRG T09 TER T16 24000 T 12442.70 L C G10 113.7 R10 RLG T10 TWL T17 24000 T 12457.28 R C G11 114.3 R11 RRG T11 TWR T18 24000 T 12471.86 L C G12 113.7 R12 RLG T12 TEL T19 24000 T 12486.44 R C G13 114.3 R13 RRG T13 TER T20 24000 T 12501.02 L C G14 113.7 R14 RLG T14 TWL T21 24000 T 12515.60 R C G15 114.3 R15 RRG T15 TWR T22 24000 T 12530.18 L C G16 113.7 R16 RLG T16 TEL T23 24000 T 12544.76 R C G17 114.3 R17 RRG T17 TER T24 24000 T 12559.34 L C G18 113.7 R18 RLG T18 TWL T25 24000 T 12573.92 R C G19 114.3 R19 RRG T19 TWR T26 24000 T 12588.50 L C G20 113.7 R20 RLG T20 TEL T27 24000 T 12603.08 R C G21 114.3 R21 RRG T21 TER T28 24000 T 12617.66 L C G22 113.7 R22 RLG T22 TWL T29 24000 T 12632.24 R C G23 114.3 R23 RRG T23 TWR T30 24000 T 12646.82 L C G24 113.7 R24 RLG T24 TEL T31 24000 T 12661.40 R C G25 114.3 R25 RRG T25 TEL T32 24000 T 12675.98 L C G26 113.7 R26 RLG T26 TWL CMD1 1000 R 17797.0 R T G27 114.3 R27 RRG T27 TWR CMD2 1000 R 17793.0 R T G28 113.7 R28 RLG T28 TEL TLM1 250 T 12694.5 R T G29 114.3 R29 RRG T29 TER TLM2 250 T 12698.5 R T G30 113.7 R30 RLG T30 TWL TLM3 250 T 12692 R T G31 114.3 R31 RRG T31 TWR

TLM4 250 T 12693 R T G32 113.7 R32 RLG T32 TEL M01 111.1 RO1 RRM T01 TER M02 110.7 R02 RLM T02 TWL M03 111.1 R03 RRM T03 TWR M04 110.7 R04 RLM T04 TWR M05 111.1 R05 RRM T05 TER M06 110.7 R06 RLM T06 TWL M07 111.1 R07 RRM T07 TWR M08 110.7 R08 RLM T08 TEL M09 111.1 R09 RRM T09 TER M10 110.7 R10 RLM T10 TWL M11 111.1 R11 RRM T11 TWR M12 110.7 R12 RLM T12 TEL M13 111.1 R13 RRM T13 TER M14 110.7 R14 RLM T14 TWL M15 111.1 R15 RRM T15 TWR M16 110.7 R16 RLM T16 TEL M17 111.1 R17 RRM T17 TER M18 110.7 R18 RLM T18 TWL M19 111.1 R19 RRM T19 TWR M20 110.7 R20 RLM T20 TEL M21 111.1 R21 RRM T21 TER M22 110.7 R22 RLM T22 TWL M23 111.1 R23 RRM T23 TWR M24 110.7 R24 RLM T24 TEL M25 111.1 R25 RRM T25 TEL M26 110.7 R26 RLM T26 TWL M27 111.1 R27 RRM T27 TWR M28 110.7 R28 RLM T28 TEL M29 111.1 R29 RRM T29 TER M30 110.7 R30 RLM T30 TWL M31 111.1 R31 RRM T31 TWR M32 110.7 R32 RLM T32 TEL

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) QPSK1 24M0G7W 24000 4 26667 0.67 3.7 20 QPSK2 25M8G7W 25800 4 35833 0.83 5.7 20 QPSK3 27M0G7W 27000 4 37500 0.83 5.7 20 8PSK1 25M8G7W 25800 8 43000 0.67 7.2 20 8PSK2 25M8G7W 25800 8 48375 0.75 8 20 8PSK3 25M8G7W 25800 8 51600 0.8 8.5 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) CMD 1M00F2D 1000 1 10 22 TLM 500KF2D 500 1 5 22

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) C01 M32 QPSK1 1 Link budgeta co 65 5 15 47.6 57.6 13.5 C01 M32 QPSK2 1 Link budgeta co 65 5 15 47.6 57.6 13.5 C01 M32 QPSK3 1 Link budgeta co 65 5 15 47.6 57.6 13.5 C01 M32 8PSK1 1 Link budgeta co 65 5 15 47.6 57.6 13.5 C01 M32 8PSK2 1 Link budgeta co 65 5 15 47.6 57.6 13.5 C01 M32 8PSK3 1 Link budgeta co 65 5 15 47.6 57.6 13.5 CMDA CMDB CMD 1 Link budgtes T 64 19 37 -33.5 TLMA TLMD TLM 1 Link budgtes T 10.5 24.4 38.1

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 Remote Control (TT C) Location(s): S14a: Street Address: Primary S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Mexico City DF 11510 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 52-55-5093-9615 Remote Control (TT C) Location(s): S14a: Street Address: Additional Facility S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Gilbert Maricopa County AZ 85233 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 480-558-2778 Remote Control (TT C) Location(s): S14a: Street Address: Backup S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Chihuahua CH 31170 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 52-61-4439-3141

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 2346 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3146 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5492 32.4 0.932 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1248.6 7.3 0.88 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 32.4 7 0.823 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): 13853 13853 13853 13853 Bus (Watts): (b): (g): (l): (q): 3265 1730 3265 1730 Total (Watts): (c): (h): (m): (r): 17118 15583 17118 15583 Solar Array (Watts): (d): (i): (n): (s): 21209 19010 19079 17286 Depth of Battery (e) (j) (o) (t) Discharge (%): 69.2 % 69.2 % 69.2 % 69.2 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO X 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: 2011-07-08 10:09:14
Document Modified: 2011-07-08 10:09:14
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