Attachment Sched S Tech Report

This document pretains to SAT-PPL-20120823-00140 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2012082300140_964987

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: SATMEX 8 11/15/2012 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 4/1/2010 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 7/1/2012 64 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: 10/1/2012 10/31/2012 2358 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) 5925 M 6425 M R Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 11700 M 12200 M T Fixed Satellite Service 3700 M 4200 M T Direct to Home in the Fixed Fixed Satellite Service 11700 M 12200 M T Direct to Home in the Fixed 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: 116.8 W The orbital location is consistent with the Trilateral Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Agreement reached between Canada, Mexico and the N/S Station-Keeping provided (Optional): United States of America in 1988. 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) SA1 S -6 dB contour of beams CUH and CUV SA2 S -6 dB contour of beams CDH and CDV SA3 S -6 dB contour of beams KHUH and KHUV SA4 S -6 dB contour of beams KNUH and KNUV SA5 S -6 dB contour of beams KHDH and KHDV SA6 S -6 dB contour of beams KNDH and KNDV

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) CUH R 28 22 0.1 30 N 0 SA1 469 1.3 -94 31 1 CUV R 28 22 0.1 30 N 90 SA1 469 1.3 -94 31 1 CDH T 26 20 0.1 30 N 0 SA2 1.4 46.8 42.7 CDV T 26 20 0.1 30 N 90 SA2 1.4 46.8 42.7 KHU R 31.8 25.8 0.11 30 N 0 SA3 528 4.6 -94 31 1 KHU R 31.8 25.8 0.11 30 N 90 SA3 528 4.6 -94 31 1 KNU R 32.9 26.9 0.12 30 N 0 SA4 484 6 -94 31 1 KNU R 32.9 26.9 0.12 30 N 90 SA4 484 6 -94 31 1 KHD T 29.9 23.9 0.11 30 N 0 SA5 1.4 107 50.2 KHD T 29.9 23.9 0.11 30 N 90 SA5 1.4 107 50.2 KND T 32.2 26.2 0.12 30 N 0 SA6 1.5 105 52.4 KND T 32.2 26.2 0.12 30 N 90 SA6 1.5 105 52.4

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) CUH R C -116.8 CUH.gxt CUV R C -116.8 CUV.gxt CDH T C -116.8 CDH.gxt -161.1 -160.9 -160.8 -160.6 -160.5 CDV T C -116.8 CDV.gxt -161.1 -160.9 -160.8 -160.6 -160.5 KHU R C -116.8 KHUH.gxt KHU R C -116.8 KHUV.gxt KNU R C -116.8 KNUH.gxt KNU R C -116.8 KNUV.gxt KHD T C -116.8 KHDH.gxt KHD T C -116.8 KHDV.gxt KND T C -116.8 KNDH.gxt KND T C -116.8 KNDV.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 (T ID Gain (dB) No. ID No. or C) CU001 36000 R 5945 H C C0001 120 CU001 CUH CD001 CDV CU002 36000 R 5985 H C C0002 120 CU002 CUH CD002 CDV CU003 36000 R 6025 H C C0003 120 CU003 CUH CD003 CDV CU004 36000 R 6065 H C C0004 120 CU004 CUH CD004 CDV CU005 36000 R 6105 H C C0005 120 CU005 CUH CD005 CDV CU006 36000 R 6145 H C C0006 120 CU006 CUH CD006 CDV CU007 36000 R 6185 H C C0007 120 CU007 CUH CD007 CDV CU008 36000 R 6225 H C C0008 120 CU008 CUH CD008 CDV CU009 36000 R 6265 H C C0009 120 CU009 CUH CD009 CDV CU010 36000 R 6305 H C C0010 120 CU010 CUH CD010 CDV CU011 36000 R 6345 H C C0011 120 CU011 CUH CD011 CDV CU012 36000 R 6385 H C C0012 120 CU012 CUH CD012 CDV CU013 36000 R 5965 V C C0013 120 CU013 CUV CD013 CDH CU014 36000 R 6005 V C C0014 120 CU014 CUV CD014 CDH CU015 36000 R 6045 V C C0015 120 CU015 CUV CD015 CDH CU016 36000 R 6085 V C C0016 120 CU016 CUV CD016 CDH CU017 36000 R 6125 V C C0017 120 CU017 CUV CD017 CDH CU018 36000 R 6165 V C C0018 120 CU018 CUV CD018 CDH CU019 36000 R 6205 V C C0019 120 CU019 CUV CD019 CDH CU020 36000 R 6245 V C C0020 120 CU020 CUV CD020 CDH CU021 36000 R 6285 V C C0021 120 CU021 CUV CD021 CDH CU022 36000 R 6325 V C C0022 120 CU022 CUV CD022 CDH CU023 36000 R 6365 V C C0023 120 CU023 CUV CD023 CDH CU024 36000 R 6405 V C C0024 120 CU024 CUV CD024 CDH CD001 36000 T 3720 V C K0001 126.5 KU001 KNUV KD001 KNDH CD002 36000 T 3760 V C K0002 126.5 KU002 KNUV KD002 KNDH CD003 36000 T 3800 V C K0003 126.5 KU003 KNUV KD003 KNDH CD004 36000 T 3840 V C K0004 126.5 KU004 KNUV KD004 KNDH CD005 36000 T 3880 V C K0005 126.5 KU005 KNUV KD005 KNDH CD006 36000 T 3920 V C K0006 126.5 KU006 KNUV KD006 KNDH

CD007 36000 T 3960 V C K0007 126.5 KU007 KNUV KD007 KNDH CD008 36000 T 4000 V C K0008 126.5 KU008 KNUV KD008 KNDH CD009 36000 T 4040 V C K0009 126.5 KU013 KNUH KD013 KNDV CD010 36000 T 4080 V C K0010 126.5 KU014 KNUH KD014 KNDV CD011 36000 T 4120 V C K0011 126.5 KU015 KNUH KD015 KNDV CD012 36000 T 4160 V C K0012 126.5 KU016 KNUH KD016 KNDV CD013 36000 T 3740 H C K0013 126.5 KU017 KNUH KD017 KNDV CD014 36000 T 3780 H C K0014 126.5 KU018 KNUH KD018 KNDV CD015 36000 T 3820 H C K0015 126.5 KU019 KNUH KD019 KNDV CD016 36000 T 3860 H C K0016 126.5 KU020 KNUH KD020 KNDV CD017 36000 T 3900 H C K0017 127.1 KU009 KHUV KD009 KHDH CD018 36000 T 3940 H C K0018 127.1 KU010 KHUV KD010 KHDH CD019 36000 T 3980 H C K0019 127.1 KU011 KHUV KD011 KHDH CD020 36000 T 4020 H C K0020 127.1 KU012 KHUV KD012 KHDH CD021 36000 T 4060 H C K0021 127.1 KU021 KHUH KD021 KHDV CD022 36000 T 4100 H C K0022 127.1 KU022 KHUH KD022 KHDV CD023 36000 T 4140 H C K0023 127.1 KU023 KHUH KD023 KHDV CD024 36000 T 4180 H C K0024 127.1 KU024 KHUH KD024 KHDV KU001 36000 R 14020 V C CMD1 CMD1 CUV KU002 36000 R 14060 V C CMD2 CMD2 CUH KU003 36000 R 14100 V C TLM1 TLM1 CDV KU004 36000 R 14140 V C TLM2 TLM2 CDV KU005 36000 R 14180 V C BCN1 BCN1 KNDV KU006 36000 R 14220 V C BCN2 BCN2 KHDH KU007 36000 R 14260 V C KU008 36000 R 14300 V C KU009 36000 R 14340 V C KU010 36000 R 14380 V C KU011 36000 R 14420 V C KU012 54000 R 14470 V C KU013 54000 R 14030 H C KU014 36000 R 14080 H C KU015 36000 R 14120 H C KU016 36000 R 14160 H C KU017 36000 R 14200 H C KU018 36000 R 14240 H C KU019 36000 R 14280 H C KU020 36000 R 14320 H C KU021 36000 R 14360 H C

KU022 36000 R 14400 H C KU023 36000 R 14440 H C KU024 36000 R 14480 H C KD001 36000 T 11720 H C KD002 36000 T 11760 H C KD003 36000 T 11800 H C KD004 36000 T 11840 H C KD005 36000 T 11880 H C KD006 36000 T 11920 H C KD007 36000 T 11960 H C KD008 36000 T 12000 H C KD009 36000 T 12040 H C KD010 36000 T 12080 H C KD011 36000 T 12120 H C KD012 54000 T 12170 H C KD013 54000 T 11730 V C KD014 36000 T 11780 V C KD015 36000 T 11820 V C KD016 36000 T 11860 V C KD017 36000 T 11900 V C KD018 36000 T 11940 V C KD019 36000 T 11980 V C KD020 36000 T 12020 V C KD021 36000 T 12060 V C KD022 36000 T 12100 V C KD023 36000 T 12140 V C KD024 36000 T 12180 V C CMD1 1000 R 5926.5 V T CMD2 1000 R 6424.5 H T TLM1 300 T 4198.6 V T TLM2 300 T 4199.4 V T BCN1 25 T 11700.5 V T BCN2 25 T 12199.3 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) D1 48K6G7W 48.6 4 56 0.691 5.7 17.9 D2 1M34G7W 1340 4 1544 0.691 5.7 17.9 D3 6M33G7W 6330 4 8448 0.801 5.8 18 D4 36M0G7W 36000 4 41505 0.691 5.7 17.9 D5 36M0G7W 36000 8 76502 0.841 6.5 18.7

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) C0001 C0024 D1 617 58 LB1.docx 47.4 -8.5 -2.5 5.6 11.6 -161.5 23.6 C0001 C0024 D2 22 1608 LB2.docx 47.4 5.9 11.9 20 26 -161.5 23.6 C0001 C0024 D3 5 7200 LB3.docx 47.4 12.6 18.6 26.7 32.7 -161.6 23.6 C0001 C0024 D4 1 LB4.docx 51.3 20.1 26.1 36.7 42.7 -159.1 21.9 C0001 C0024 D5 1 LB5.docx 53.5 18.3 24.3 36.7 42.7 -159.1 21.9 K0001 K0016 D1 617 58 LB6.docx 49.2 -13.1 -7.1 15.5 21.5 24.4 K0001 K0016 D2 22 1608 LB7.docx 43.2 5.2 11.2 28.1 34.1 26.9 K0001 K0016 D3 5 7200 LB8.docx 49.2 8.8 14.8 36.4 42.4 26.9 K0001 K0016 D4 1 LB9.docx 54.7 16.5 22.5 46.4 52.4 20.8 K0001 K0016 D5 1 LB10.docx 54.7 16.5 22.5 46.4 52.4 22.8 K0017 K0024 D1 617 58 LB11.docx 49.3 -13.1 -6.1 13.3 19.3 27 K0017 K0024 D2 22 1608 LB12.docx 43.3 5.3 11.3 26 32 30.8 K0017 K0024 D3 5 7200 LB13.docx 49.3 8.8 14.8 34.2 40.2 27 K0017 K0024 D4 1 LB14.docx 54.8 16.6 26.6 44.2 50.2 22.9 K0017 K0024 D5 1 LB15.docx 54.8 16.6 26.6 44.2 50.2 24.5

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): No Remote Control (TT C) Location(s): S14a: Street Address: CONTEL - Edificio SGA-II S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Mexico,D.F. CP 09310 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 1 52 (55) 5804 7300 Remote Control (TT C) Location(s): S14a: Street Address: Carretera a Bahía Kino Km 5.5 S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Hermosillo, Sonora CP 83210 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 01 (662) 2600289

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 2317 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3140 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5463 26.1 0.8871 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1221 7.8 0.8847 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 74.2 7.4 0.7848 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): 10833 10833 10833 10833 Bus (Watts): (b): (g): (l): (q): 2637 1389 2637 1389 Total (Watts): (c): (h): (m): (r): 13470 12222 13470 12222 Solar Array (Watts): (d): (i): (n): (s): 17404 15540 15491 14031 Depth of Battery (e) (j) (o) (t) Discharge (%): 67.8 % % 67.8 % % 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: 2012-08-30 16:14:26
Document Modified: 2012-08-30 16:14:26
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