Attachment Sched S Tech Report.

This document pretains to SAT-MOD-20141210-00126 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2014121000126_1070880

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: JUPITER 97W N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 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) 18.3 G 18.6 G T Fixed Satellite Service 18.6 G 18.8 G T Fixed Satellite Service 18.8 G 19.3 G T Fixed Satellite Service 19.7 G 20.2 G T Fixed Satellite Service 27.85 G 29.1 G R Fixed Satellite Service 29.25 G 29.5 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: 97.1 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) SA1 E CONUS, Alaska, Puerto Rico, Canada, Mexico and parts of Central and South America SA2 E Cuba SA3 E CONUS, Canada, Mexico

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) GR1 R 0.05 1 30 SA3 25.3 -98 1 1 GT1 T 0.05 1 30 SA3 67.4 UR1 R 0.05 1 21.5 SA1 18.3 -94 1 1 UT1 T 0.05 1 21.5 SA1 71 CR1 R 0.05 1 21.5 SA2 14.2 -94 1 1 CT1 T 0.05 1 21.5 SA2 62 CMD R 0.05 1 20 SA3 -23 -75 1 1 TLM T 0.05 1 20 SA3 15.5 BCN T 0.05 1 20 SA3 24.2 RFAT R 0.05 1 27 SA3 23.3 -114 1 1 IOT T 0.05 1 27 SA3 42.8

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) GR1 R C GR1.gxt GT1 T C GT1.gxt -142.9 -142.7 -142.6 -142.5 -122.4 UR1 R C UR1.gxt UT1 T C UT1.gxt -122.3 -122.2 -122 -121.9 -121.8 CR1 R C CR1.gxt CT1 T C CT1.gxt -145.3 -145.1 -145 -144.9 -144.8 CMD R C TLM T C -146.8 -146.7 -146.6 -146.5 -146.4 BCN T C BCN.gxt -170.1 -169.5 -168.8 -168.7 -168.6 RFAT R C RFAT.gxt IOT T C IOT.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) UL1 250000 R 28225 R C TX1 UL1 GR1 UL2 250000 R 28475 R C TX2 UL2 GR1 UL3 250000 R 28725 R C TX3 UL3 GR1 UL4 250000 R 28975 R C TX4 UL4 GR1 UL5 250000 R 29625 R C TX5 UL5 GR1 UL6 250000 R 29875 R C TX6 UL6 GR1 UL7 250000 R 28225 L C TX7 UL7 GR1 UL8 250000 R 28475 L C TX8 UL8 GR1 UL9 250000 R 28725 L C TX9 UL9 GR1 UL10 250000 R 28975 L C TX10 UL10 GR1 UL11 250000 R 29375 R C TX11 UL11 GR1 UL12 250000 R 27975 L C TX12 UL12 GR1 UL13 250000 R 29375 L C TX13 UL13 GR1 UL14 125000 R 29312.5 L C TX14 UL14 UR1 UL15 125000 R 29437.5 L C TX15 UL15 UR1 UL16 125000 R 29812.5 L C TX16 UL16 UR1 UL17 125000 R 29937.5 L C TX17 UL17 UR1 UL18 125000 R 29687.5 L C TX18 UL18 UR1 UL19 125000 R 29562.5 L C TX19 UL19 UR1 UL20 125000 R 29312.5 R C TX20 UL20 UR1 UL21 125000 R 29437.5 R C TX21 UL21 UR1 UL22 125000 R 29812.5 R C TX22 UL22 UR1 UL23 125000 R 29937.5 R C TX23 UL23 UR1 UL24 125000 R 29562.5 R C TX24 UL24 UR1 UL25 125000 R 29687.5 R C TX25 UL25 UR1 DL1 250000 T 18425 R C TX26 UL14 CR1 DL2 250000 T 18675 R C TX27 UL15 CR1 DL3 250000 T 18925 R C TX28 UL16 CR1 DL4 250000 T 19175 R C TX29 UL17 CR1 DL5 250000 T 19825 R C TX30 UL18 CR1

DL6 250000 T 20075 R C TX31 UL19 CR1 DL7 250000 T 18425 L C TX32 UL20 CR1 DL8 250000 T 18675 L C TX33 UL21 CR1 DL9 250000 T 18925 L C TX34 UL22 CR1 DL10 250000 T 19175 L C TX35 UL23 CR1 DL11 250000 T 19825 L C TX36 UL24 CR1 DL12 250000 T 20075 L C TX37 UL25 CR1 DL13 125000 T 18362.5 L C TX38 DL1 UT1 DL14 125000 T 18487.5 L C TX39 DL2 UT1 DL15 125000 T 18862.5 L C TX40 DL3 UT1 DL16 125000 T 18987.5 L C TX41 DL4 UT1 DL17 125000 T 18737.5 L C TX42 DL5 UT1 DL18 125000 T 18612.5 L C TX43 DL6 UT1 DL19 125000 T 19762.5 L C TX44 DL7 UT1 DL20 125000 T 19887.5 L C TX45 DL8 UT1 DL21 125000 T 19112.5 L C TX46 DL9 UT1 DL22 125000 T 19237.5 L C TX47 DL10 UT1 DL23 125000 T 20012.5 L C TX48 DL11 UT1 DL24 125000 T 20137.5 L C TX49 DL12 UT1 CMD1 1000 R 28351.5 R T TX50 DL1 CT1 CMD2 1000 R 28353.5 R T TX51 DL2 CT1 TLM1 1000 T 19701 R T TX52 DL3 CT1 TLM2 1000 T 19703 R T TX53 DL4 CT1 BCN1 25 T 20199 H T TX54 DL5 CT1 RFAT1 25 R 29998.5 R T TX55 DL6 CT1 RFAT2 25 R 29998.5 L T TX56 DL7 CT1 TX57 DL8 CT1 TX58 DL9 CT1 TX59 DL10 CT1 TX60 DL11 CT1 TX61 DL12 CT1 TX62 DL13 GT1 TX63 DL14 GT1 TX64 DL15 GT1 TX65 DL16 GT1 TX66 DL17 GT1 TX67 DL18 GT1 TX68 DL19 GT1 TX69 DL20 GT1

TX70 DL21 GT1 TX71 DL22 GT1 TX72 DL23 GT1 TX73 DL24 GT1 TC1 CMD1 CMD TC2 CMD2 CMD TC3 CMD1 GR1 TC4 CMD2 GR1 TM1 TLM1 TLM TM2 TLM2 TLM TM3 TLM1 GT1 TM4 TLM2 GT1 BECN BCN1 BCN RF1 RFAT1 RFAT RF2 RFAT2 RFAT

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 250MG7W 250000 D2 125MG7W 125000 D3 40M0G7W 40000 D4 3M67G7W 3672 D5 1M22G7W 1224 D6 612KG7W 612

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) A1 1M00F2D 1000 A2 1M00G2D 1000 A3 25K0N 25

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) TX38 TX49 D1 65 TX38 TX49 D2 62 TX38 TX49 D3 57 TX50 TX61 D1 62 TX50 TX61 D2 59 TX50 TX61 D3 54 TX62 TX73 D4 46.1 TX62 TX73 D5 41.3 TX62 TX73 D6 38.3 TM1 TM2 A2 15.5 TM3 TM4 A2 41.2 BECN BECN A3 24.2

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

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? X YES NO 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: 2014-12-11 12:38:50
Document Modified: 2014-12-11 12:38:50
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC