Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20070207-00027 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2007020700027_549490

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: IS 11 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 34 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: 1552 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 Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode f. 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 12750 M 13250 M R Fixed Satellite Service 13750 M 14000 M R Fixed Satellite Service 10700 M 11450 M 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: 43 W Replaces PAS 8B Satellite 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 (o) Other Plane (Seconds) Node (Deg.) (Degrees) Angle 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) 1 S North America and South America 2 S North America and South America and Europe 3 S East Brazil 4 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) (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Input Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) Losses Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) (db/K) (dBW/m2) CHU R 30.6 20.6 0.1 0.6 18 N 01 488 3.7 -103.7 25 1 CVU R 30.6 20.6 0.1 0.6 18 N 90 1 488 3.7 -103.7 25 1 CHD T 27.5 19.5 0.1 0.6 24 N 0 2 2.2 33.1 42.7 CVD T 27.5 19.5 0.1 0.6 24 N 90 2 2.2 33.1 42.7 KHU R 29.2 23.2 0.1 0.6 26 N 0 2 550 1.8 -98.8 25 1 KVUL R 29.2 23.2 0.1 0.6 26 N 90 2 550 1.8 -98.8 25 1 KHD T 37.5 33.5 0.1 0.6 30 N 0 3 2.5 61.7 55.4 KVDL T 37.5 33.5 0.1 0.6 30 N 90 3 2.5 61.7 55.4 UPC T 13 11 0.1 0.6 N 0 4 1.6 2.1 16.2 UPC T 13 11 0.1 0.6 N 90 4 1.6 2.1 16.2 CMD R 29.2 19.2 0.1 0.6 N 02 5655 -8.3 -117.3 CMD R 29.2 19.2 0.1 0.6 N 90 2 5655 -8.3 -117.3 CMD R 13 6 0.1 0.6 N 4 17038 -29.3 -96.4 CMD R 3 -1 0.1 0.6 N 4 5501 -34.4 -91.3 TLM T 21 18 0.1 0.6 N 04 4.6 0.1 12.4 TLM T 13 6 0.1 0.6 N 4 8.9 1.1 13.4 TLM T 3 -1 0.1 0.6 N 4 5.7 2.3 6.6

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) CHU R C 43 CHUL.gxt CVU R C 43 CVUL.gxt CHD T C 43 CHDL.gxt -152 -150.5 -150.3 -150.2 -150.1 CVD T C 43 CVDL.gxt -152 -150.5 -150.3 -150.2 -150.1 KHU R C 43 KHUL.gxt KVUL R C 43 KVUL.gxt KHD T C 43 KHDL.gxt -150 -147.5 -145 -142.5 -140 KVDL T C 43 KVDL.gxt -150 -147.5 -145 -142.5 -140 UPC T C 43 UPCH.pdf -155 -154.9 -154.8 -154.7 -154.6 UPC T C 43 UPCV.pdf -155 -154.9 -154.8 -154.7 -154.6 CMD R C 43 CMDH.gxt CMD R C 43 CMDV.gxt CMD R C 43 CMDW.pdf CMD R C 43 CMDO.pdf TLM T C 43 TLMG.pdf TLM T C 43 TLMW.pdf TLM T C 43 TLMO.pdf CHU R X 43 CHUX.gxt CVU R X 43 CVUX.gxt CHD T X 43 CHDX.gxt CVD T X 43 CVDX.gxt KHU R X 43 KHUX.gxt KVUL R X 43 KVUX.gxt KHD T X 43 KHDX.gxt KVDL T X 43 KVDX.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 ID Gain (dB) No. ID No. (T or C) CU1 54000 R 5955 H C 1C 125.6 CU1 CHUL CD1 CVDL CU2 54000 R 5955 V C 2C 125.6 CU2 CVUL CD2 CHDL CU3 54000 R 6015 H C 3C 125.6 CU3 CHUL CD3 CVDL CU4 54000 R 6015 V C 4C 125.6 CU4 CVUL CD4 CHDL CU5 54000 R 6075 H C 5C 125.6 CU5 CHUL CD5 CVDL CU6 54000 R 6075 V C 6C 125.6 CU6 CVUL CD6 CHDL CU7 64000 R 6140 H C 7C 125.6 CU7 CHUL CD7 CVDL CU8 64000 R 6140 V C 8C 125.6 CU8 CVUL CD8 CHDL CU9 54000 R 6205 H C 9C 125.6 CU9 CHUL CD9 CVDL CU10 54000 R 6205 V C 10C 125.6 CU10 CVUL CD10 CHDL CU11 54000 R 6265 H C 11C 125.6 CU11 CHUL CD11 CVDL CU12 54000 R 6265 V C 12C 125.6 CU12 CVUL CD12 CHDL CU13 54000 R 6325 H C 13C 125.6 CU13 CHUL CD13 CVDL CU14 54000 R 6325 V C 14C 125.6 CU14 CVUL CD14 CHDL CU15 64000 R 6390 H C 15C 125.6 CU15 CHUL CD15 CVDL CU16 64000 R 6390 V C 16C 125.6 CU16 CVUL CD16 CHDL CD1 54000 T 3730 V C 1K 131.2 KU1 KHUL KD1 KVDL CD2 54000 T 3730 H C 13K 131.2 KU13 KVUL KD13 KHDL CD3 54000 T 3790 V C 3K 131.2 KU3 KHUL KD3 KVDL CD4 54000 T 3790 H C 15K 131.2 KU15 KVUL KD15 KHDL CD5 54000 T 3850 V C 5K 131.2 KU5 KHUL KD5 KVDL CD6 54000 T 3850 H C 17K 131.2 KU17 KVUL KD17 KHDL CD7 64000 T 3915 V C 7K 131.2 KU7 KHUL KD7 KVDL CD8 64000 T 3915 H C 19K 131.2 KU19 KVUL KD19 KHDL CD9 54000 T 3980 V C 9K 131.2 KU9 KHUL KD9 KVDL CD10 54000 T 3980 H C 21K 131.2 KU21 KVUL KD21 KHDL CD11 54000 T 4040 V C 11K 131.2 KU11 KHUL KD11 KVDL CD12 54000 T 4040 H C 23K 131.2 KU23 KVUL KD23 KHDL CD13 54000 T 4100 V C 25K 131.2 KU25 KHUL KD25 KVDL CD14 54000 T 4100 H C 31K 131.2 KU31 KVUL KD31 KHDL

CD15 64000 T 4165 V C 27K 131.2 KU27 KHUL KD27 KVDL CD16 64000 T 4165 H C 33K 131.2 KU33 KVUL KD33 KHDL KU1 36000 R 12772 H C 29K 131.2 KU29 KHUL KD29 KVDL KU13 36000 R 12772 V C 35K 131.2 KU35 KVUL KD35 KHDL KU3 36000 R 12852 H C KU15 36000 R 12852 V C KU5 36000 R 12932 H C KU17 36000 R 12932 V C KU7 36000 R 13022 H C KU19 36000 R 13022 V C KU9 36000 R 13102 H C KU21 36000 R 13102 V C KU11 36000 R 13182 H C KU23 36000 R 13182 V C KU25 36000 R 13774 H C KU31 36000 R 13774 V C KU27 36000 R 13854 H C KU33 36000 R 13854 V C KU29 36000 R 13934 H C KU35 36000 R 13934 V C KD1 36000 T 10722 V C KD13 36000 T 10722 H C KD3 36000 T 10802 V C KD15 36000 T 10802 H C KD5 36000 T 10882 V C KD17 36000 T 10882 H C KD7 36000 T 11222 V C KD19 36000 T 11222 H C KD9 36000 T 11302 V C KD21 36000 T 11302 H C KD11 36000 T 11382 V C KD23 36000 T 11382 H C KD25 36000 T 10970 V C KD31 36000 T 10970 H C KD27 36000 T 11050 V C KD33 36000 T 11050 H C KD29 36000 T 11130 V C KD35 36000 T 11130 H C ULPC1 25 T 3701 H C

ULPC2 25 T 4199.5 V C CMD1 1000 R 13246.5 H T CMD2 1000 R 13995.5 V T CMD3 1000 R 13246.5 L T CMD4 1000 R 13995.5 L T TLM1 500 T 11448 H T TLM2 500 T 11449 H T TLM3 500 T 11448 R T TLM4 500 T 11449 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) DC1 49M0G7W 49046.8 4 60000 0.75 6.1 12.7 DC2 44M8G7W 44751.5 4 34368 0.5 3.1 10.8 DC3 4M15G7W 4154 4 6000 0.75 6.7 13.8 DC4 1M21G7W 1212.8 4 1544 0.75 5.7 12.7 DC5 75K4G7W 75.4 4 64 0.5 3 10.5 DK1 30M1G7W 30133 4 36863 0.75 10.6 16.2 DK2 4M15G7W 4154 4 6000 0.75 10 15.9 DK3 1M21G7W 1212.8 4 1544 0.75 9.2 15.1 DK4 1M23G7W 1229 2 512 0.5 8.1 15.5 DK5 307KG7W 307 2 128 0.5 7.8 18.2 DK6 75K4G7W 75.4 4 64 0.5 6.6 13.5

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) AC1 30M0F3F 30000 TV/FM 1 NTSC 12.8 2.6 10 16.1 AC2 24M0F3F 24000 TV/FM 1 NTSC 12.8 2.6 10 16.5 AK1 36M0F3F 36000 TV/FM 1 NTSC 12.8 2.6 13.7 19.9

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. (o)Assoc. Transponder (kHz) No.) Bandwidth (Table (Table S12) Stn. Max. Power (dBW) Power Flux Stn (a) Start (b) End (kHz) S11) Antenna Density Rec. G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dBW/m2/Hz) (dB/K) 1C 16C AC2 2 24000 PAS11_LINK_ 4000 51 14.2 24.2 30.2 38.2 -153.9 31 1C 16C DC2 1 PAS11_NOTE.t 51 13.2 23.2 34.7 42.7 -159.9 21 1C 16C DC3 5 6875 PAS11_NOTE.t 51 7.9 17.9 21.4 29.4 -162.9 26.2 1C 16C DC4 24 1550 PAS11_NOTE.t 51 1.4 11.4 14.9 22.9 -164 26.2 1C 16C DC5 424 100 PAS11_NOTE.t 51 -11.1 -1.1 2.4 10.4 -164.5 23.6 7C 16C AC1 2 30000 PAS11_NOTE.t 51 14.2 24.2 30.2 38.2 -153.9 33 7C 16C DC1 1 PAS11_NOTE.t 51 13.2 23.2 34.7 42.7 -160.3 26.2 7C 16C DC3 6 6875 PAS11_NOTE.t 51 7.1 17.1 20.6 28.6 -163.6 26.6 7C 16C DC4 28 1550 PAS11_NOTE.t 51 0.6 10.6 14.1 22.1 -164.8 26.6 7C 16C DC5 436 100 PAS11_NOTE.t 51 -11.2 -1.2 2.3 10.3 -164.6 23.6 25K 35K AK1 1 PAS11_NOTE.t 4000 56.7 17.4 23.4 51.4 55.4 -136.7 21.6 25K 35K DK1 1 PAS11_NOTE.t 56.7 17.4 23.4 51.4 55.4 -145.5 18.1 25K 35K DK2 3 6875 PAS11_NOTE.t 56.7 10.6 16.6 42.1 46.1 -146.2 18.1 25K 35K DK3 15 1550 PAS11_NOTE.t 56.7 4.5 10.5 36 40 -146.9 18.1 25K 35K DK4 24 1450 PAS11_NOTE.t 56.7 0.4 6.4 31.9 35.9 -151.1 21.6 25K 35K DK5 90 400 PAS11_NOTE.t 46.2 1.2 7.2 22.2 26.2 -154.8 32.4 25K 35K DK6 360 100 PAS11_NOTE.t 56.7 -10.2 -4.2 21.4 25.4 -149.5 18.1

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: 3400 International Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Washington, D.C. DC 20008 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 202-944-7701

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 1171 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1311 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2482 22.4 0.893 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 525 4.2 0.87 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 29.7 3.3 0.777 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): 4847 4847 4465 4465 Bus (Watts): (b): (g): (l): (q): 1206 785 1148 756 Total (Watts): (c): (h): (m): (r): 6053 5632 5613 5221 Solar Array (Watts): (d): (i): (n): (s): 7256 6510 6687 6147 Depth of Battery (e) (j) (o) (t) Discharge (%): 75.3 % % 75.6 % % 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: 2007-02-12 15:40:23
Document Modified: 2007-02-12 15:40:23
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