Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20060727-00083 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2006072700083_516102

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: ICO GS-2 8/1/2009 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 2/1/2007 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 2/1/2009 98 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: 3/1/2009 5/1/2009 1960 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) 2000 M 2020 M R Mobile-Satellite Service 2180 M 2200 M T Mobile-Satellite Service 18.55 G 18.8 G T Feeder Link for Mobile Satellite Service in FSS 19.7 G 20.2 G T Feeder Link for Mobile Satellite Service in FSS 29.25 G 30 G R Feeder Link for Mobile Satellite Service in FSS 20198.85 M 20199.15 M T Fixed Satellite Service 29998.5 M 29999.5 M R Fixed Satellite Service 5925 M 5930 M R Fixed Satellite Service 6420 M 6425 M R Fixed Satellite Service 3700 M 3705 M T Fixed Satellite Service 4195 M 4200 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: 114.75 W This orbital location provides high elevation angles to Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be all of CONUS, which is very important for the link N/S Station-Keeping provided (Optional): between the satellite and the user terminal in the d. Toward West: Degrees E/W 0.05 Degrees Tolerance: MSS. The high elevation angle minimizes the risk of g. Westernmost: e. Toward East: 0.05 Degrees signal blockage due to buildings and foliage. This 6 Degrees h. Easternmost: orbital location also eliminates any station-keeping volume overlap with that of the satellite operator at i. Reason for service are selection (Optional): 114.9W.

114.9W.

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) SA1 S CONUS, Alaska, Hawaii, Puerto Rico, US Virgin Islands SA2 S CONUS

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) SU R 44 41 0.1 1 20 N SA1 427 17.7 20 1 SD T 43 40 0.1 1 20 N SA1 1.1 1677 75.2 KAUL R 49.2 46.2 0.1 1 30 N SA2 1234 18.3 20 1 KAU R 49.2 46.2 0.1 1 30 N SA2 1234 18.3 20 1 KADL T 49.5 46.5 0.1 1 30 N SA2 4 51.8 66.6 KAD T 49.5 46.5 0.1 1 30 N SA2 4 51.8 66.6 GBL T 28 25 1 1 30 N SA2 8 0.063 16 OMN R 0 -4 1 1 30 N 0 SA2 1000 -30 OMN T 0 -4 1 1 30 N 0 SA2 4.4 14.5 11.6 OMN R 0 -4 1 1 30 N 90 SA2 1000 -30 OMN T 0 -4 1 1 30 N 90 SA2 4.4 14.5 11.6 KAU R 49.2 46.2 1 1 30 N SA2 1778 16.7

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) SU R C -114.75 SD T C -114.75 KAUL R C -114.75 KAU R C -114.75 KADL T C -114.75 -132.5 -132.5 -132.5 -132.5 -132.5 KAD T C -114.75 -132.5 -132.5 -132.5 -132.5 -132.5 GBL T C -114.75 -146 -146 -146 -146 -146 KAU R C -114.75 OMN T C -114.75 -154 -154 -154 -154 -154 OMN T C -114.75 -154 -154 -154 -154 -154

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) U0001 20000 R 29325 L C RL037 130 SU001 SU D0037 KADR U0002 20000 R 29350 L C RL038 130 SU001 SU D0038 KADR U0003 20000 R 29375 L C RL039 130 SU001 SU D0039 KADR U0004 20000 R 29400 L C RL040 130 SU001 SU D0040 KADR U0005 20000 R 29425 L C RL041 130 SU001 SU D0041 KADR U0006 20000 R 29450 L C RL042 130 SU001 SU D0042 KADR U0007 20000 R 29475 L C RL043 130 SU001 SU D0043 KADR U0008 20000 R 29500 L C RL044 130 SU001 SU D0044 KADR U0009 20000 R 29525 L C RL045 130 SU001 SU D0045 KADR U0010 20000 R 29550 L C RL046 130 SU001 SU D0046 KADR U0011 20000 R 29575 L C RL047 130 SU001 SU D0047 KADR U0012 20000 R 29600 L C RL048 130 SU001 SU D0048 KADR U0013 20000 R 29625 L C RL049 130 SU001 SU D0049 KADR U0014 20000 R 29650 L C RL050 130 SU001 SU D0050 KADR U0015 20000 R 29675 L C C001 CMD1 OMNRH U0016 20000 R 29700 L C C002 CMD2 OMNRV U0017 20000 R 29725 L C C003 CMD3 KAUCR U0018 20000 R 29750 L C T001 TLM1 OMNTH U0019 20000 R 29775 L C T002 TLM2 OMNTV U0020 20000 R 29800 L C T003 TLM3 GBL U0021 20000 R 29825 L C FL001 120 U0001 KAUL SD001 SD U0022 20000 R 29850 L C FL002 120 U0002 KAUL SD001 SD U0023 20000 R 29875 L C FL003 120 U0003 KAUL SD001 SD U0024 20000 R 29900 L C FL004 120 U0004 KAUL SD001 SD U0025 20000 R 29325 R C FL005 120 U0005 KAUL SD001 SD U0026 20000 R 29350 R C FL006 120 U0006 KAUL SD001 SD U0027 20000 R 29375 R C FL007 120 U0007 KAUL SD001 SD U0028 20000 R 29400 R C FL008 120 U0008 KAUL SD001 SD U0029 20000 R 29425 R C FL009 120 U0009 KAUL SD001 SD U0030 20000 R 29450 R C FL010 120 U0010 KAUL SD001 SD

U0031 20000 R 29475 R C FL011 120 U0011 KAUL SD001 SD U0032 20000 R 29500 R C FL012 120 U0012 KAUL SD001 SD U0033 20000 R 29525 R C FL013 120 U0013 KAUL SD001 SD U0034 20000 R 29550 R C FL014 120 U0014 KAUL SD001 SD U0035 20000 R 29575 R C FL015 120 U0015 KAUL SD001 SD U0036 20000 R 29600 R C FL016 120 U0016 KAUL SD001 SD U0037 20000 R 29625 R C FL017 120 U0017 KAUL SD001 SD U0038 20000 R 29650 R C FL018 120 U0018 KAUL SD001 SD U0039 20000 R 29675 R C FL019 120 U0019 KAUL SD001 SD U0040 20000 R 29700 R C FL020 120 U0020 KAUL SD001 SD U0041 20000 R 29725 R C FL021 120 U0021 KAUL SD001 SD U0042 20000 R 29750 R C FL022 120 U0022 KAUL SD001 SD U0043 20000 R 29775 R C FL023 120 U0023 KAUL SD001 SD U0044 20000 R 29800 R C FL024 120 U0024 KAUL SD001 SD U0045 20000 R 29825 R C FL025 120 U0025 KAUR SD001 SD U0046 20000 R 29850 R C FL026 120 U0026 KAUR SD001 SD U0047 20000 R 29875 R C FL027 120 U0027 KAUR SD001 SD U0048 20000 R 29900 R C FL028 120 U0028 KAUR SD001 SD D0001 20000 T 18600 L C FL029 120 U0029 KAUR SD001 SD D0002 20000 T 18625 L C FL030 120 U0030 KAUR SD001 SD D0003 20000 T 18650 L C FL031 120 U0031 KAUR SD001 SD D0004 20000 T 18675 L C FL032 120 U0032 KAUR SD001 SD D0005 20000 T 18700 L C FL033 120 U0033 KAUR SD001 SD D0006 20000 T 18725 L C FL034 120 U0034 KAUR SD001 SD D0007 20000 T 18750 L C FL035 120 U0035 KAUR SD001 SD D0008 20000 T 18775 L C FL036 120 U0036 KAUR SD001 SD D0009 20000 T 19725 L C FL037 120 U0037 KAUR SD001 SD D0010 20000 T 19750 L C FL038 120 U0038 KAUR SD001 SD D0011 20000 T 19775 L C FL039 120 U0039 KAUR SD001 SD D0012 20000 T 19800 L C FL040 120 U0040 KAUR SD001 SD D0013 20000 T 19825 L C FL041 120 U0041 KAUR SD001 SD D0014 20000 T 19850 L C FL042 120 U0042 KAUR SD001 SD D0015 20000 T 19875 L C FL043 120 U0043 KAUR SD001 SD D0016 20000 T 19900 L C FL044 120 U0044 KAUR SD001 SD D0017 20000 T 19925 L C FL045 120 U0045 KAUR SD001 SD D0018 20000 T 19950 L C FL046 120 U0046 KAUR SD001 SD D0019 20000 T 19975 L C FL047 120 U0047 KAUR SD001 SD D0020 20000 T 20000 L C FL048 120 U0048 KAUR SD001 SD D0021 20000 T 20025 L C RL001 130 SU001 SU D0001 KADL

D0022 20000 T 20050 L C RL002 130 SU001 SU D0002 KADL D0023 20000 T 20075 L C RL003 130 SU001 SU D0003 KADL D0024 20000 T 20100 L C RL004 130 SU001 SU D0004 KADL D0025 20000 T 20125 L C RL005 130 SU001 SU D0005 KADL D0026 20000 T 18600 R C RL006 130 SU001 SU D0006 KADL D0027 20000 T 18625 R C RL007 130 SU001 SU D0007 KADL D0028 20000 T 18650 R C RL008 130 SU001 SU D0008 KADL D0029 20000 T 18675 R C RL009 130 SU001 SU D0009 KADL D0030 20000 T 18700 R C RL010 130 SU001 SU D0010 KADL D0031 20000 T 18725 R C RL011 130 SU001 SU D0011 KADL D0032 20000 T 18750 R C RL012 130 SU001 SU D0012 KADL D0033 20000 T 18775 R C RL013 130 SU001 SU D0013 KADL D0034 20000 T 19725 R C RL014 130 SU001 SU D0014 KADL D0035 20000 T 19750 R C RL015 130 SU001 SU D0015 KADL D0036 20000 T 19775 R C RL016 130 SU001 SU D0016 KADL D0037 20000 T 19800 R C RL017 130 SU001 SU D0017 KADL D0038 20000 T 19825 R C RL018 130 SU001 SU D0018 KADL D0039 20000 T 19850 R C RL019 130 SU001 SU D0019 KADL D0040 20000 T 19875 R C RL020 130 SU001 SU D0020 KADL D0041 20000 T 19900 R C RL021 130 SU001 SU D0021 KADL D0042 20000 T 19925 R C RL022 130 SU001 SU D0022 KADL D0043 20000 T 19950 R C RL023 130 SU001 SU D0023 KADL D0044 20000 T 19975 R C RL024 130 SU001 SU D0024 KADL D0045 20000 T 20000 R C RL025 130 SU001 SU D0025 KADL D0046 20000 T 20025 R C RL026 130 SU001 SU D0026 KADR D0047 20000 T 20050 R C RL027 130 SU001 SU D0027 KADR D0048 20000 T 20075 R C RL028 130 SU001 SU D0028 KADR D0049 20000 T 20100 R C RL029 130 SU001 SU D0029 KADR D0050 20000 T 20125 R C RL030 130 SU001 SU D0030 KADR SU001 20000 R 2010 R C RL031 130 SU001 SU D0031 KADR SD001 20000 T 2190 L C RL032 130 SU001 SU D0032 KADR CMD1 1000 R 5926 H T RL033 130 SU001 SU D0033 KADR CMD2 1000 R 6424 V T RL034 130 SU001 SU D0034 KADR CMD3 1000 R 29999 R T RL035 130 SU001 SU D0035 KADR TLM1 300 T 3701 H T RL036 130 SU001 SU D0036 KADR TLM2 300 T 4196 V T TLM3 300 T 20199 L 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 200KG7W 200 4 118.75 0.5 3.4 15.6 D2 1M25G7W 1250 4 4.75 0.561 21.1 -18.9 -6.7 D3 8K00G1W 8 4 4.75 0.5 3.4 15.6 D4 8K00G1W 8 4 4.75 0.5 2.3 14.5 D5 1M25G7W 1250 4 4.75 0.561 21.1 -18.9 -6.7

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) A1 1M00F1D 1000 1 10 22.2 A2 300KG1D 300 1 9 21.2 A3 1M00F1D 1000 1 10 22.2 A4 300KG1D 300 1 10.4 22.6

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) FL001 FL048 D1 100 200 HT TDMA Fow 68.1 -14.1 2.7 54.3 57.3 -27 FL001 FL048 D2 16 1250 HT CDMA Fow 68.1 -28.4 -11.6 40 43 -27 FL001 FL048 D3 10 200 HT HPN Fowar 68.1 -12 4.8 56.3 59.3 -27 FL001 FL048 D1 100 200 PA TDMA Fow 68.1 -23.8 -7 44.5 47.5 -22 FL001 FL048 D2 16 1250 PA CDMA Fow 68.1 -38.1 -21.3 30.2 33.2 -22 FL001 FL048 D3 10 200 PA HPN Fowar 68.1 -12 4.8 56.3 59.3 -22 RL001 RL050 D4 2500 8 HT FDMA Retu 0 0 0 5.5 8.5 -132.5 40.6 RL001 RL050 D5 16 1250 HT CDMA Retu 0 -1 -1 8.9 11.9 -132.5 40.6 RL001 RL050 D4 2500 8 PA FDMA Retu 3 3 3 5.5 8.5 -132.5 40.6 RL001 RL050 D5 16 1250 PA CDMA Retu 3 2 2 8.9 11.9 -132.5 40.6 C001 C002 A1 1 C-Band CMD L 53 7.3 28.3 C003 C003 A3 1 Ka-Band CMD 65 -29.7 -8.7 T001 T002 A2 1 C-Band TLM L 7.6 11.6 -154 T003 T003 A4 1 Ka-Band TLM L 13 16 -146

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

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 2735 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3011 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5580 22 0.79 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 850 31 0.84 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 60 11 0.66 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): 6605 6605 6605 6605 Bus (Watts): (b): (g): (l): (q): 2080 1055 2080 1055 Total (Watts): (c): (h): (m): (r): 8685 7660 8685 7660 Solar Array (Watts): (d): (i): (n): (s): 11220 10310 10000 9335 Depth of Battery (e) (j) (o) (t) Discharge (%): 74 % 0 % 74 % 74 % 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: 2006-07-31 13:46:29
Document Modified: 2006-07-31 13:46:29
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