Attachment Schedule S Tech Data

This document pretains to SAT-LOI-20080603-00118 for Letter of Intent on a Satellite Space Stations filing.

IBFS_SATLOI2008060300118_645040

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: SPACEWAY 4 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12.6 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 48 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: 24000 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) 28.1 G 29.1 G R Fixed Satellite Service 18.3 G 19.3 G T Fixed Satellite Service 19.7 G 20.2 G T Fixed Satellite Service 29.25 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: 107.1 W The Ka-band at the nominal 107W.L. location is Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be unassigned. The 107.1W.L. location is selected in N/S Station-Keeping provided (Optional): order to avoid physical collision with other satellites d. Toward West: Degrees E/W 0.05 Degrees Tolerance: that are proposed to operate nominally at 107W.L. 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) SA1 S CONUS, Alaska, Hawaii, Puerto Rico, USVI and portions of Canada and Mexico. SA2 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) SPRL R 50.1 44.6 0.03 0.03 23 N SA1 650 22 31.5 0.5 SPR R 50.1 44.6 0.03 0.03 23 N SA1 650 22 31.5 0.5 SPTL T 51.5 50.8 0.03 0.03 30 N SA1 70.9 SPT T 51.5 50.8 0.03 0.03 30 N SA1 70.9 CON T 35 28.5 0.03 0.03 30 N SA1 64.5 CON T 35 28.5 0.03 0.03 30 N SA1 64.5 TC R 50.1 47.1 0.03 0.03 30 N SA1 3664 12 TM T 22.3 18.3 0.03 0.03 30 N SA2 3.05 9.4 32.04 OMN R 5 2 0.03 0.03 30 N SA2 3707 -30.7 OMN R -0.7 -3.7 0.03 0.03 30 N 0 SA2 7533 -39.5 OMN T 5 2 0.03 0.03 30 N SA2 7.47 2.7 9.3 OMN T -0.7 -3.7 0.03 0.03 30 N 0 SA2 5.24 4.5 5.8

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) SPRL R C -107.1 SPRL.gxt SPR R C -107.1 SPRR.gxt SPTL T C -107.1 SPTL.gxt -119.4 -119.2 -119.1 -119 -118.9 SPT T C -107.1 SPTR.gxt -119.4 -119.2 -119.1 -119 -118.9 CON T C -107.1 CONL.gxt -119.7 -119.6 -119.5 -119.4 -119.3 CON T C -107.1 CONR.gxt -119.7 -119.6 -119.5 -119.4 -119.3 TC R C -107.1 TC.gxt TM T C -107.1 TM.gxt -135.2 -135 -134.8 -134.5 -134.1 OMN T C -107.1 -152.7 -152.7 -152.7 -157.2 -157.2 OMN T C -107.1 -156.2 -156.2 -156.2 -156.2 -156.2

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) UL01 250000 R 28225 L C UL01 UL01 SPRL UL02 250000 R 28225 R C UL02 UL02 SPRR UL03 250000 R 28725 L C UL03 UL03 SPRL UL04 250000 R 28725 R C UL04 UL04 SPRR UL05 250000 R 28975 L C UL05 UL05 SPRL UL06 250000 R 28975 R C UL06 UL06 SPRR UL07 250000 R 28475 L C UL07 UL07 SPRL UL08 250000 R 28475 R C UL08 UL08 SPRR UL09 250000 R 29375 L C UL09 UL09 SPRL UL10 250000 R 29375 R C UL10 UL10 SPRR UL11 250000 R 29625 L C UL11 UL11 SPRL UL12 250000 R 29625 R C UL12 UL12 SPRR UL13 250000 R 29875 L C DL01 DL01 SPTL UL14 250000 R 29875 R C DL02 DL02 SPTR DL01 500000 T 19050 L C DL03 DL03 SPTL DL02 500000 T 19050 R C DL04 DL04 SPTR DL03 500000 T 18550 L C DL05 DL05 SPTL DL04 500000 T 18550 R C DL06 DL06 SPTR DL05 500000 T 19950 L C DL07 DL01 CONL DL06 500000 T 19950 R C DL08 DL02 CONR CMD1 1300 R 29252 L T DL09 DL03 CONL CMD2 1300 R 29254 L T DL10 DL04 CONR CMD3 1300 R 29252 H T DL11 DL05 CONL CMD4 1300 R 29254 H T DL12 DL06 CONR TM1 106 T 19701.25 L T TC1 CMD1 TC TM2 106 T 19702.25 L T TC2 CMD2 TC TM3 106 T 19701.25 H T TC3 CMD1 OMNUL TM4 106 T 19702.25 H T TC4 CMD2 OMNUL BCN1 25 R 29999 L T TC5 CMD3 OMNUH BCN2 25 R 29998.5 L T TC6 CMD4 OMNUH

TM1 TM1 TM TM2 TM2 TM TM3 TM1 OMNDL TM4 TM2 OMNDL TM5 TM3 OMNDH TM6 TM4 OMNDH BCN1 BCN1 SPRL BCN2 BCN2 SPRL UL13 UL13 SPRL UL14 UL14 SPRR

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 651KG7W 651 4 520.8 0.6 8.8 21 D2 2M60G7W 2600 4 2083 0.6 8.8 21 D3 20M8G7W 20800 4 16666 0.6 8.8 21 D4 250MG7W 250000 4 200000 0.6 8.8 21 D5 500MG7W 500000 4 400000 0.61 6.7 18.9 D6 167MG7W 167000 4 133333 0.61 6.7 18.9 D7 125MG7W 125000 4 125000 0.61 6.7 18.9

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 1M30F9D 1300 1 15 27.2 A2 25K0N0N 25 1 25 35 A3 106KG9D 106 1 14 26.2

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) UL01 UL02 D4 1 ULB4.doc 64.2 -1.3 14.5 UL03 UL14 D1 384 651 ULB1.doc 45.6 -8.5 7.3 UL03 UL14 D2 96 2600 ULB2.doc 53.3 -10.2 5.6 UL03 UL14 D3 12 20800 ULB3.doc 59.1 -7 8.8 DL01 DL06 D5 1 DLB1.doc 64.3 70.9 -118.3 18.6 DL01 DL06 D5 1 DLB2.doc 64.3 70.9 -118.3 26.1 DL01 DL06 D5 1 DLB3.doc 64.3 70.9 -118.3 36.5 DL07 DL12 D6 1 DLB4.doc 58 64.5 -120.2 18.6 DL07 DL12 D7 1 DLB5.doc 58 64.5 -119 18.6 TC1 TC2 A1 1 TC LB.doc 64.5 -27.8 -19.2 TC3 TC4 A1 1 Emergency TC 64.5 16.2 26.8 TC5 TC6 A1 1 Emergency TC 64.5 23.7 27.4 BCN1 BCN2 A2 1 BCN LB.doc 64.5 -16.5 -14 TM1 TM2 A3 1 TM LB.doc 28.04 32.04 -130 38 TM3 TM4 A3 1 Pipe TM LB.do 7.9 9.3 -152.8 38 TM5 TM6 A3 1 Bicone TM LB. 5.82 5.82 -156.3 38

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: 5281 East Garton S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Castle Rock Douglas CO 80104 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 303-660-7200 E060382 Remote Control (TT C) Location(s): S14a: Street Address: 33 East Telegraph Road S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Fillmore Ventura CA 93015 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 805-524-4444 E060383

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 3950 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2425 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6375 54 0.86 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 960 8.5 0.89 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 104.5 7.5 0.77 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): 14400 14400 14400 14400 Bus (Watts): (b): (g): (l): (q): 4500 2500 4500 2500 Total (Watts): (c): (h): (m): (r): 18900 16900 18900 16900 Solar Array (Watts): (d): (i): (n): (s): 20500 18614 18860 18102 Depth of Battery (e) (j) (o) (t) Discharge (%): 73 % 73 % 73 % 73 % 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: 2008-06-05 12:37:40
Document Modified: 2008-06-05 12:37:40
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