Attachment Sched S Tech Report.

This document pretains to SAT-LOA-20151202-00080 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2015120200080_1125579

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: HORIZONS 3E N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 36 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: 2424 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 12.920 G 13.250 G R Fixed Satellite Service 13.750 G 14.000 G R Fixed Satellite Service 10.850 G 11.700 G T Fixed Satellite Service 12.200 G 12.700 G T Fixed Satellite Service 14.000 G 14.500 G R Fixed Satellite Service 12.700 G 12.750 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: 169 E 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 Degrees E/W 0.05 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 of (l) Argument of Active Service Arc Range (Degrees) Plane No. Satellites in Angle (degrees) Period the Ascending Node Perigee (m) Begin (n) End Angle (o) Other Plane (Seconds) (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) GLB 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) CGV R 20.8 16.8 0.1 0.4 22 N 90 GLB 1 1 CPLU R 1.2 1.2 0.1 0.4 22 N GLB 1 1 CHLU R 4.8 4.8 0.1 0.4 22 N GLB 1 1 TGH T 20.1 16.1 0.1 0.4 22 N 0 GLB 13.7 TPLD T 7.6 7.6 0.1 0.4 22 N GLB 15.4 THLD T 3.3 3.3 0.1 0.4 22 N GLB 11.9 CLHD T 11.5 11.5 0.1 0.4 22 N GLB 9.4 KLRD T 18.1 18.1 0.1 0.4 22 N GLB 16 KLLD T 19.4 19.4 0.1 0.4 22 N GLB 16.8 PVR R 29.6 25.6 0.1 0.4 22 N 90 GLB 4 -106 1 1 PHR R 29.6 25.6 0.1 0.4 22 N 0 GLB 4 -106 1 1 PHT T 27.8 23.8 0.1 0.4 22 N 0 GLB 49.5 PVT T 27.8 23.8 0.1 0.4 22 N 90 GLB 49.5 GLR R 21.1 18.6 0.1 0.4 30 N GLB -6 -102 1 1 GRR R 21.1 18.6 0.1 0.4 30 N GLB -6 -102 1 1 GRT T 21 18.5 0.1 0.4 30 N GLB 36 GLT T 21 18.5 0.1 0.4 30 N GLB 36

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 Gain Max. Power Flux Density (dBW/M2/Hz) Beam T/R Cross Ref. Orbital Contour Description Contour Data (GXT File) At Angle of Arrival above horizontal (for emission with highest PFD) ID Mode Polar Longitude (Figure/Table/ Exhibit) (g) 5 Deg (h) 10 Deg (i) 15 Deg (j) 20 Deg (k) 25 Deg Mode ("C" (Deg. E/W) or" X") CGV R C 169 CPLU R C 169 CHLU R C 169 TGH T C 169 -168.4 -168.3 -168.1 -168 -167.9 TPLD T C 169 -166.7 -166.6 -166.4 -166.3 -166.2 THLD T C 169 -170.2 -170.1 -169.9 -169.8 -169.7 CLHD T C 169 -154.3 -153.2 -152.1 -150.9 -150.8 KLRD T C 169 -155.3 -155.2 -155.1 -154.9 -154.8 KLLD T C 169 -154.5 -154.4 -154.3 -154.1 -154 PVR R C 169 PVR.gxt PHR R C 169 PHR.gxt PHT T C 169 PHT.gxt -148.2 -148.1 -148 -147.9 -147.8 PVT T C 169 PVT.gxt -148.2 -148.1 -148 -147.9 -147.8 GLR R C 169 GRR R C 169 GRT T C 169 -159.3 -159.2 -159.1 -159 -158.9 GLT T C 169 -159.3 -159.2 -159.1 -159 -158.9

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 L C TC001 CU001 GLR CU003 36000 R 5985 L C TC002 CU003 GLR CU005 36000 R 6025 L C TC003 CU005 GLR CU007 36000 R 6065 L C TC004 CU007 GLR CU009 108000 R 6145 L C TC005 CU009 GLR CU011 108000 R 6265 L C TC006 CU011 GLR CU013 36000 R 6345 L C TC007 CU013 GLR CU015 36000 R 6385 L C TC008 CU015 GLR CU002 36000 R 5945 R C TC009 CU002 GRR CU004 36000 R 5985 R C TC010 CU004 GRR CU006 36000 R 6025 R C TC011 CU006 GRR CU008 36000 R 6065 R C TC012 CU008 GRR CU010 108000 R 6145 R C TC013 CU010 GRR CU012 108000 R 6265 R C TC014 CU012 GRR CU014 36000 R 6345 R C TC015 CU014 GRR CU016 36000 R 6385 R C TC016 CU016 GRR CD001 36000 T 3720 R C TC017 CD001 GRT CD003 36000 T 3760 R C TC018 CD003 GRT CD005 36000 T 3800 R C TC019 CD005 GRT CD007 36000 T 3840 R C TC020 CD007 GRT CD009 108000 T 3920 R C TC021 CD009 GRT CD011 108000 T 4040 R C TC022 CD011 GRT CD013 36000 T 4120 R C TC023 CD013 GRT CD015 36000 T 4160 R C TC024 CD015 GRT CD002 36000 T 3720 L C TC025 CD002 GLT CD004 36000 T 3760 L C TC026 CD004 GLT CD006 36000 T 3800 L C TC027 CD006 GLT CD008 36000 T 3840 L C TC028 CD008 GLT CD010 108000 T 3920 L C TC029 CD010 GLT CD012 108000 T 4040 L C TC030 CD012 GLT

CD014 36000 T 4120 L C TC031 CD014 GLT CD016 36000 T 4160 L C TC032 CD016 GLT KU001 72000 R 12960 H C TK001 KU001 PHR KU003 72000 R 13040 H C TK002 KU003 PHR KU005 72000 R 13120 H C TK003 KU005 PHR KU007 81000 R 13205 H C TK004 KU007 PHR KU009 224000 R 13868 H C TK005 KU009 PHR KU011 108000 R 14046 H C TK006 KU011 PHR KU013 108000 R 14166 H C TK007 KU013 PHR KU015 81000 R 14271 H C TK008 KU015 PHR KU017 81000 R 14361 H C TK009 KU017 PHR KU019 81000 R 14451 H C TK010 KU019 PHR KU002 72000 R 12960 V C TK011 KU002 PVR KU004 72000 R 13040 V C TK012 KU004 PVR KU006 72000 R 13120 V C TK013 KU006 PVR KU008 81000 R 13205 V C TK014 KU008 PVR KU010 224000 R 13868 V C TK015 KU010 PVR KU012 108000 R 14046 V C TK016 KU012 PVR KU014 108000 R 14166 V C TK017 KU014 PVR KU016 81000 R 14271 V C TK018 KU016 PVR KU018 81000 R 14361 V C TK019 KU018 PVR KU020 81000 R 14451 V C TK020 KU020 PVR KD001 72000 T 12240 V C TK021 KD001 PVT KD003 72000 T 12320 V C TK022 KD003 PVT KD005 72000 T 12400 V C TK023 KD005 PVT KD007 81000 T 12485 V C TK024 KD007 PVT KD009 224000 T 10968 V C TK025 KD009 PVT KD011 108000 T 11146 V C TK026 KD011 PVT KD013 108000 T 11266 V C TK027 KD013 PVT KD015 81000 T 11371 V C TK028 KD015 PVT KD017 81000 T 11461 V C TK029 KD017 PVT KD019 81000 T 11551 V C TK030 KD019 PVT KD002 72000 T 12240 H C TK031 KD002 PHT KD004 72000 T 12320 H C TK032 KD004 PHT KD006 72000 T 12400 H C TK033 KD006 PHT KD008 81000 T 12485 H C TK034 KD008 PHT KD010 224000 T 10968 H C TK035 KD010 PHT KD012 108000 T 11146 H C TK036 KD012 PHT KD014 108000 T 11266 H C TK037 KD014 PHT

KD016 81000 T 11371 H C TK038 KD016 PHT KD018 81000 T 11461 H C TK039 KD018 PHT KD020 81000 T 11551 H C TK040 KD020 PHT CMD01 1200 R 5925.5 L T CMD2A 1200 R 6424.5 V T CMD2B 1200 R 6424.5 L T TLM1A 300 T 4197.75 H T TLM1B 300 T 4197.75 L T TLM2A 300 T 4198.25 H T TLM2B 300 T 4198.25 L T TLM3A 300 T 4198.75 H T TLM3B 300 T 4198.75 L T TLM4A 300 T 4199.25 H T TLM4B 300 T 4199.25 L T ULPC1 25 T 4199.75 H T ULPC2 25 T 11451 R T ULPC3 25 T 12200.25 R 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 8M25G7W 8250 D3 1M74G7W 1733 D4 382KG7W 382

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) TC001 TC016 D1 TC001 TC016 D2 TC001 TC016 D3 TC001 TC016 D4 TC017 TC032 D1 36 TC017 TC032 D2 36 TC017 TC032 D3 28.1 TC017 TC032 D4 22.4 TK001 TK020 D1 TK001 TK020 D2 TK001 TK020 D3 TK001 TK020 D4 TK021 TK040 D1 49.5 TK021 TK040 D2 48.8 TK021 TK040 D3 40.1 TK021 TK040 D4 34.3

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: 7900 Tysons One Place S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: McLean Fairfax VA 22102 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 703-559-7701

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 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 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: 2016-02-10 13:38:34
Document Modified: 2016-02-10 13:38:34
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC