Attachment Sched S Tech Report

This document pretains to SAT-MPL-20130528-00078 for Modification Permitted List (space station) on a Satellite Space Stations filing.

IBFS_SATMPL2013052800078_1005599

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: NSS-806 2/28/1998 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 17 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 31 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: 2/28/1998 2/28/1998 1523 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) 3465 M 4200 M T Fixed Satellite Service 5850 M 6425 M R Fixed Satellite Service 6490 M 6650 M R Fixed Satellite Service 11.7 G 11.95 G T Fixed Satellite Service 14 G 14.25 G R Fixed Satellite Service 3465 M 4200 M T Direct to Home in the Fixed Fixed Satellite Service 11.7 G 11.95 G 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: 47.5 W This orbit location was selected to provide reasonable Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be elevation angles to the desired service areas, and to N/S Station-Keeping provided (Optional): increase the isolation to the two adjacent satellites. d. Toward West: Degrees E/W 0.1 Degrees Tolerance: g. Westernmost: e. Toward East: 0.1 Degrees 0.1 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) HA S North and South America, Western Europe HB S North and South America, Western Europe S1_A S United States, Caribbean S1_B S United States, Caribbean 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) HAU R 24.4 18.4 0.19 0.34 30 N HA 562 -3.1 -93 20 2 HAD T 24.9 18.9 0.19 0.34 30 N HA 1.7 44.7 41.4 HBU R 24.4 18.4 0.19 0.34 30 N HB 562 -3.1 -93 20 2 HBD T 24.9 18.9 0.19 0.34 30 N HB 1.7 44.7 41.4 S1U R 33.1 27.1 0.19 0.34 30 N 90 S1_B 631 5.1 -100 22 2 S1D T 32.3 26.3 0.19 0.34 30 N 0 S1_B 1.7 91.2 51.9 CMD R 10.3 9.3 0.19 0.34 30 N GLB 550 -17.1 -90 TLM T 11.3 10.3 0.19 0.34 30 N GLB 3 1.2 12 BNC T 11.3 10.3 0.19 0.34 30 N GLB 3 0.9 11 BNK T 32.3 26.3 0.19 0.34 30 N S1_B 3 0.1 9

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) S1U R C -47.5 NSS-806 S1U.gxt S1D T C -47.5 NSS-806 S1D.gxt -155.1 -153.7 -152 -150 -148.2 HAU R C -47.5 NSS-806 HAU.gxt HAD T C -47.5 NSS-806 HAD.gxt -154.1 -154 -153.9 -153.7 -153.6 CMD R C -47.5 NSS-806 CMD.gxt TLM T C -47.5 NSS-806 TLM.gxt -162.2 -162.1 -162 -161.9 -161.7 BNC T C -47.5 NSS-806 BNC.gxt -161.2 -161.1 -161 -160.9 -160.7 BNK T C -47.5 NSS-806 BNK.gxt -172.2 -170.9 -169.2 -167.2 -165.3 HBU R C -47.5 NSS-806 HBU.gxt HBD T C -47.5 NSS-806 HBD.gxt -149.8 -149.6 -149.5 -149.4 -149.3

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) HBDL 36000 T 4095 L C 1 124.5 HAUA HAU HADA HAD HBDM 36000 T 4135 L C 2 124.6 HAUB HAU HADB HAD HBDN 41000 T 4177.5 L C 3 123.6 HAUC HAU HADC HAD S1UA 77000 R 14042.5 V C 4 123.7 HAUD HAU HADD HAD S1UB 72000 R 14125 V C 5 123.8 HAUE HAU HADE HAD S1UC 72000 R 14205 V C 6 123.9 HAUF HAU HADF HAD S1UD 72000 R 14042.5 V C 7 123.9 HAUG HAU HADG HAD S1UE 36000 R 14125 V C 8 124 HAUH HAU HADH HAD S1UF 36000 R 14205 V C 9 124.1 HAUI HAU HADI HAD S1DA 77000 T 11747.5 H C 10 124.1 HAUJ HAU HADJ HAD S1DB 72000 T 11830 H C 11 124.2 HAUK HAU HADK HAD S1DC 72000 T 11910 H C 12 124.2 HAUL HAU HADL HAD S1DD 72000 T 11747.5 H C 13 124.3 HAUM HAU HADM HAD S1DE 36000 T 11830 H C 14 124.3 HAUN HAU HADN HAD S1DF 36000 T 11910 H C 15 124.5 HBUA HBU HBDA HBD TM1 300 T 3947.5 R T 16 124.6 HBUB HBU HBDB HBD TM2 300 T 3948 R T 17 123.6 HBUC HBU HBDC HBD TM3 300 T 3952.5 R T 18 123.7 HBUD HBU HBDD HBD TM4 300 T 3952 R T 19 123.8 HBUE HBU HBDE HBD CMD1 800 R 6173.7 L T 20 123.9 HBUF HBU HBDF HBD CMD2 800 R 6176.3 L T 21 123.9 HBUG HBU HBDG HBD BC1 25 T 3950 V T 22 124 HBUH HBU HBDH HBD BK1 25 T 11701 H T 23 124.1 HBUI HBU HBDI HBD HAUA 72000 R 6527 L C 24 124.1 HBUJ HBU HBDJ HBD HAUB 72000 R 6607 L C 25 124.2 HBUK HBU HBDK HBD HAUC 72000 R 5888 L C 26 124.2 HBUL HBU HBDL HBD HAUD 72000 R 5968 L C 27 124.3 HBUM HBU HBDM HBD HAUE 36000 R 6028 L C 28 124.3 HBUN HBU HBDN HBD HAUF 36000 R 6068 L C 29 132.6 S1UA S1U S1DA S1D HAUG 36000 R 6108 L C 30 132.7 S1UB S1U S1DB S1D

HAUH 36000 R 6148 L C 31 132.7 S1UC S1U S1DC S1D HAUI 34000 R 6201 L C 32 129.5 S1UD S1U HADD HAD HAUJ 36000 R 6240 L C 33 129.6 S1UE S1U HADF HAD HAUK 36000 R 6280 L C 34 129.6 S1UF S1U HADH HAD HAUL 36000 R 6320 L C 35 126.8 HAUD HAU S1DD S1D HAUM 36000 R 6360 L C 36 127 HAUF HAU S1DE S1D HAUN 41000 R 6402.5 L C 37 127.1 HAUH HAU S1DF S1D HADA 72000 T 3502 R C 38 TM1 TLM HADB 72000 T 3582 R C 39 TM2 TLM HADC 72000 T 3663 R C 40 TM3 TLM HADD 72000 T 3743 R C 41 TM4 TLM HADE 36000 T 3803 R C 42 CMD1 CMD HADF 36000 T 3843 R C 43 CMD2 CMD HADG 36000 T 3883 R C 44 BC1 BNC HADH 36000 T 3923 R C 45 BK1 BNK HADI 34000 T 3976 R C HADJ 36000 T 4015 R C HADK 36000 T 4055 R C HADL 36000 T 4095 R C HADM 36000 T 4135 R C HADN 41000 T 4177.5 R C HBUA 72000 R 6527 R C HBUB 72000 R 6607 R C HBUC 72000 R 5888 R C HBUD 72000 R 5968 R C HBUE 36000 R 6028 R C HBUF 36000 R 6068 R C HBUG 36000 R 6108 R C HBUH 36000 R 6148 R C HBUI 34000 R 6201 R C HBUJ 36000 R 6240 R C HBUK 36000 R 6280 R C HBUL 36000 R 6320 R C HBUM 36000 R 6360 R C HBUN 41000 R 6402.5 R C HBDA 72000 T 3502 L C HBDB 72000 T 3582 L C HBDC 72000 T 3663 L C HBDD 72000 T 3743 L C

HBDE 36000 T 3803 L C HBDF 36000 T 3843 L C HBDG 36000 T 3883 L C HBDH 36000 T 3923 L C HBDI 34000 T 3976 L C HBDJ 36000 T 4015 L C HBDK 36000 T 4055 L C

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 346KG7W 346 4 256 0.5 6 18.2 D2 461KG7W 461 4 512 0.75 9.3 21.5 D3 1M85G7W 1843 4 2048 0.75 9.3 21.5 D4 8M25G7W 8250 4 8448 0.692 6.9 19.1 D5 36M0G7W 35999 4 41470 0.692 6.9 19.1 D6 72M2G7W 72196 8 155000 0.816 12.7 24.9 D7 36M0G7W 35874 4 38000 0.691 8.9 21.1 D8 2M00G1W 1933 4 1365 0.461 5.6 17.8 D9 8M00G1W 7974 4 5631 0.461 5.6 17.8

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 36M0F3F 36000 TV/FM 1 PAL 13.2 1.5 10 24 TTC1 800KF9D 800 1 10 24 TTC2 300KF9D 300 1 0 14 TTC3 25K0N0N 25 1 0 14

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) 29 31 D1 184 391 NSS-806_Link_ 51 -4.9 1.1 20.3 26.3 -153.8 25.3 29 31 D2 105 685 Please see NS 52.8 -4.4 1.6 22.7 28.7 -152.7 27.8 29 31 D3 37 1945 Please see NS 52.8 0.2 6.2 27.2 33.2 -154.2 29.8 29 31 D4 6 12000 Please see NS 51 9.5 15.5 34.7 40.7 -153.2 25.3 29 31 D6 1 Please see NS 52.8 20.8 26.8 45.9 51.9 -152.2 31.6 29 31 A1 2 36000 Please see NS 2000 59.1 7.7 13.7 38.5 44.5 -144.5 27.8 32 32 D1 200 360 Please see NS 50.9 -3.6 2.4 9.1 15.1 -165 21.8 32 32 D2 112 642 Please see NS 52.8 -2.9 3.1 11.6 17.6 -163.7 25.2 32 32 D3 28 2571 Please see NS 52.8 3.2 9.2 17.7 23.7 -163.7 25.2 32 32 D4 8 9000 Please see NS 50.9 10.3 16.3 23 29 -164.9 23.3 32 32 D6 1 Please see NS 56.4 18.3 24.3 35.4 41.4 -162.6 27.1 32 32 A1 2 36000 Please see NS 2000 59.1 12.4 18.4 31.8 37.8 -151.3 21.8 33 34 D1 104 346 Please see NS 51 -2.5 3.5 12.2 18.2 -161.9 20 33 34 D2 69 521 Please see NS 52.8 -2.6 3.4 14 20 -161.4 22 33 34 D3 17 2117 Please see NS 52.8 3.5 9.5 20 26 -161.4 22 33 34 D4 4 9000 Please see NS 51 11.2 17.2 25.9 31.9 -162 20 33 34 D5 1 Please see NS 52.8 18.1 24.1 33.6 39.6 -161.2 20 33 34 A1 1 Please see NS 2000 59.1 12.4 18.4 31.8 37.8 -151.3 22 35 35 D1 171 421 Please see NS 45.3 0.5 6.5 20.6 26.6 -153.5 25.3 35 35 D2 126 571 Please see NS 47.1 0.1 6.1 21.9 27.9 -153.5 29.7 35 35 D3 39 1846 Please see NS 47.1 5.1 11.1 26.9 32.9 -154.5 31.7 35 35 D4 7 10285 Please see NS 45.3 13.8 19.8 33.9 39.9 -154 27.8 35 35 D6 1 Please see NS 54.9 19.2 25.2 45.9 51.9 -152.2 37.1 35 35 A1 2 36000 Please see NS 2000 51.8 15.1 21.1 39.2 45.2 -143.9 29.7 36 37 D1 104 346 Please see NS 45.5 1.7 7.7 22 28 -152.1 25.3 36 37 D2 78 461 Please see NS 47.2 1.4 7.4 23.4 29.4 -152 27.8 36 37 D3 19 1894 Please see NS 47.2 7.2 13.2 29.2 35.2 -152.2 29.8 36 37 D4 4 9000 Please see NS 45.5 15.5 21.5 35.8 41.8 -152.1 25.3 36 37 D5 1 Please see NS 49.1 20.8 26.8 42.7 48.7 -152.1 25.3

36 37 A1 1 Please see NS 2000 51.8 15.1 21.1 39.2 45.2 -143.9 29.8 45 45 TTC3 1 Please see NS 3 9 -161 38.4 42 43 TTC1 1 Please see NS 54 12 18 38 41 TTC2 1 Please see NS 6 12 -168.8 30 1 28 D7 1 Please see NS 45.5 26 32 32.5 38.5 -162 20.5 1 28 D8 18 2000 Please see NS 45.5 7.5 13.5 15.7 21.7 -166 18.7 1 28 D9 4 8000 Please see NS 45.5 13.6 19.6 21.9 27.9 -166 18.7

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: Manassas Teleport S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Bristow VA 20136 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +1 703 367 7300 E980076 Remote Control (TT C) Location(s): S14a: Street Address: Arqiva Chalfont S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Gerrards Cross SL9 8TW S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +44 8708 798 787

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 1550 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1725 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3275 23.94 0.864 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 454 2.46 0.891 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 51.3 4.77 0.769 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): 4302 3935 4302 3935 Bus (Watts): (b): (g): (l): (q): 581 557 581 557 Total (Watts): (c): (h): (m): (r): 4883 4492 4883 4492 Solar Array (Watts): (d): (i): (n): (s): 6294 6004 5399 4826 Depth of Battery (e) (j) (o) (t) Discharge (%): 70 % % 70 % % 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: 2013-07-25 16:23:07
Document Modified: 2013-07-25 16:23:07
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