Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20040614-00114 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2004061400114_384401

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-1 6/25/2005 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12/17/1999 12.6 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 12/31/2004 10 MHz d. Estimated Launch Date: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply: 1/15/2005 1000 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) 18.3 G 18.8 G T Fixed Satellite Service 19.7 G 20.2 G T Fixed Satellite Service 19.7 G 20.2 G T Direct to Home in the Fixed Fixed Satellite Service 28.35 G 28.6 G R Fixed Satellite Service 29.25 G 29.5 G R Fixed Satellite Service 29.5 G 30.0 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: 103.05 W 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) SAID-1 S See file "BeamID&ZipCode103W.pdf" for zip codes covered by each SAID SAID-106 S Mexico City, Mexico SAID-107 S See file "BeamID&ZipCode103W.pdf" for zip codes covered by each SAID SAID-108 S Caracas, Venezuela SAID-109 S Bogota, Columbia SAID-110 S Sao Paulo/Rio de Janeiro, Brazil SAID-111 S Lima, Peru SAID-112 S Buenos Aires, Argentina SAID-113 S Southern CA and Central CO SAID-A S CONUS+Alaska+Hawaii+Mexico City+Puerto Rico+Caracas+Bogota+Sao Paulo/Rio+Lima+Buenos Aires SAID-B S Western U.S. SAID-2 S See file "BeamID&ZipCode103W.pdf" for zip codes covered by SAID-2 SAID-52 S See file "BeamID&ZipCode103W.pdf" for zip codes covered by SAID-52 SAID-90 S See file "BeamID&ZipCode103W.pdf" for zip codes covered by SAID-90 SAID-91 S See file "BeamID&ZipCode103W.pdf" for zip codes covered by SAID-91

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) 112 R 50.1 46.1 0.03 23 N SAID-112 650 22 31.5 0.5 113 R 47 44 0.03 30 N SAID-113 1452 15.4 -90 8 0.1 DL-A T 51.5 50.5 0.03 30 Y SAID-A 74.5 DL-B T 22 21 0.03 19 Y SAID-B 4.74 11.8 27.98 2 R 50.1 46.1 0.03 23 N SAID-2 650 22 31.5 0.5 52 R 50.1 46.1 0.03 23 N SAID-52 650 22 31.5 0.5 90 R 50.1 46.1 0.03 23 N SAID-90 650 22 31.5 0.5 91 R 50.1 46.1 0.03 23 N SAID-91 650 22 31.5 0.5 1 R 50.1 46.1 0.03 23 N SAID-1 650 22 31.5 0.5

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) 112 R C -103 Beam 112 (103W).gxt DL-A T C -103 DL-A (103W).gxt 113 R C -103 Beam 113 (103W).gxt DL-B T C -103 Beam DL-B (103W)_R2.gxt -152 -152 -152 -152 -152 1 R C -103 Beam 1 (103W).gxt 2 R C -103 Beam 2 (103W).gxt 90 R C -103 Beam 90 (103W).gxt 91 R C -103 Beam 91 (103W).gxt 52 R C -103 Beam 52 (103W).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) RL001 165000 R 28442.5 L C T0001 TL100 DL-A RL002 165000 R 29342.5 L C T0002 TL101 DL-A RL003 62500 R 29531.25 L C A0302 TL012 DL-A RL004 62500 R 29593.75 L C A0303 TR012 DL-A RL005 62500 R 29656.25 L C A0304 TL013 DL-A RL006 62500 R 29718.75 L C A0305 TR013 DL-A RL007 62500 R 29781.25 L C B0001 120 RL001 113 TL001 DL-B RL008 62500 R 29843.75 L C B0002 120 RL001 113 TR001 DL-B RL009 62500 R 29906.25 L C B0003 133 RL002 1 TL002 DL-B RL010 62500 R 29968.75 L C B0004 133 RL002 1 TR002 DL-B RR002 165000 R 29342.5 R C B0005 133 RR002 112 TL002 DL-B RR003 62500 R 29531.25 R C B0006 133 RR002 112 TR002 DL-B RR004 62500 R 29593.75 R C A0001 71.5 RL003 1 TL003 DL-A RR005 62500 R 29656.25 R C A0002 71.5 RL003 1 TR003 DL-A RR006 62500 R 29718.75 R C A0003 71.5 RR003 112 TL003 DL-A RR007 62500 R 29781.25 R C A0004 71.5 RR003 112 TR003 DL-A RR008 62500 R 29843.75 R C A0005 71.5 RL003 1 TL010 DL-A RR009 62500 R 29906.25 R C A0006 71.5 RL003 1 TR010 DL-A RR010 62500 R 29968.75 R C A0007 71.5 RR003 112 TL010 DL-A TL001 165000 T 18447.5 L C A0008 71.5 RR003 112 TR010 DL-A TL002 165000 T 18652.5 L C A0009 71.5 RL010 1 TL010 DL-A TL003 62500 T 19731.25 L C A0010 71.5 RL010 1 TR010 DL-A TL004 62500 T 19793.75 L C A0011 71.5 RR010 112 TL010 DL-A TL005 62500 T 19856.25 L C A0012 71.5 RR010 112 TR010 DL-A TL006 62500 T 19918.75 L C A0013 71.5 RL010 1 TL003 DL-A TL007 62500 T 19981.25 L C A0014 71.5 RL010 1 TR003 DL-A TL008 62500 T 20043.75 L C A0015 71.5 RR010 112 TL003 DL-A TL009 62500 T 20106.25 L C A0016 71.5 RR010 112 TR003 DL-A TL010 62500 T 20168.75 L C A0103 RL003 1 TR001 165000 T 18447.5 R C A0104 RL004 1

TR002 165000 T 18652.5 R C A0105 RL005 1 TR003 62500 T 19731.25 R C A0106 RL006 1 TR004 62500 T 19793.75 R C A0107 RL007 1 TR005 62500 T 19856.25 R C A0108 RL008 1 TR006 62500 T 19918.75 R C A0109 RL009 1 TR007 62500 T 19981.25 R C A0110 RL010 1 TR008 62500 T 20043.75 R C A0203 RR003 112 TR009 62500 T 20106.25 R C A0204 RR004 112 TR010 62500 T 20168.75 R C A0205 RR005 112 RL100 1300 R 29501.3021 L T A0206 RR006 112 RL101 1300 R 29509.1146 L T A0207 RR007 112 RL102 25 R 29527.3438 L T A0208 RR008 112 RL103 25 R 29532.5521 L T A0209 RR009 112 TL100 106 T 19701.25 L T A0210 RR010 112 TL101 106 T 19702.25 L T A0300 TL011 DL-A TL011 500000 T 19950 L C A0301 TR011 DL-A TR011 500000 T 19950 R C C0001 RL100 113 TL012 167000 T 19950 L C C0002 RL101 113 TR012 167000 T 19950 R C C0003 RL102 113 TL013 100000 T 19950 L C C0004 RL103 113 TR013 100000 T 19950 R 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) E1/4 650KG7W 650 4 520.8 0.6 7.3 20 E1 2M61G7W 2610 4 2083 0.6 7.3 19 8E1 20M9G7W 20800 4 16666 0.6 7.3 19.9 BB1 500MG7W 500000 4 400000 0.61 6.8 18.4 BB2 167MG7W 167000 4 133333 0.61 6.8 18.4 BB3 125MG7W 125000 4 100000 0.61 6.8 18.4 DTH 24M0G7W 24000 8 60000 0.75 9 20.8 BH1 24M0G7W 24000 4 40000 0.5 1.9 13.8 BH2 36M0G7W 36000 4 60000 0.5 1.9 15 BH3 54M0G7W 54000 4 90000 0.5 1.9 13.3

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) C1 1M30F9D 1300 1 15 26 B1 25K0N0N 25 1 25 44.2 T1 106KG9D 160 1 14 11.5

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) T0001 T0002 T1 1 5.82 32 -130 37.9 C0001 C0002 C1 1 64.5 50 89.5 C0003 C0004 B1 1 64.5 53.1 89.5 B0001 B0006 BH1 4 66.8 8.2 13.2 23 23 -153.2 39.3 B0001 B0006 BH2 2 66.7 10.7 15.7 26 26 -150.2 39.3 B0001 B0006 BH3 2 66.7 11.7 16.7 26 26 -150.2 39.3 A0001 A0016 DTH 2 66.8 8.1 13.1 58.4 58.4 -118 19.4 A0300 A0301 BB3 1 64 64 -118 17.2 A0300 A0301 BB2 1 64 66.2 -118 17.2 A0300 A0301 BB1 1 64 71 -118 17.2 A0300 A0301 BB3 1 64 64 -118 29 A0300 A0301 BB2 1 64 66.2 -118 29 A0300 A0301 BB1 1 64 71 -118 29 A0001 A0016 8E1 2 53.3 57 58.7 A0001 A0016 E1 24 45.8 47 51 A0001 A0016 E1/4 96 45.8 42 47.4 A0001 A0016 8E1 2 58.9 57 78.3 A0001 A0016 E1 24 58.9 48 78.3 A0001 A0016 E1/4 96 58.9 42 78.3

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): No Remote Control (TT C) Location(s): S14a: Street Address: 8900 Desoto Ave S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Canoga Park Los Angeles CA 91303 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 818 586 0734 E020241 Remote Control (TT C) Location(s): S14a: Street Address: 7235 W. Titan Rd S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Littleton Douglas CO 80125 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 303 486 3902 E020242

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 3635 (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: 6060 41 0.86 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 260 8 0.89 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 65 7 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): 8601 8601 8601 8601 Bus (Watts): (b): (g): (l): (q): 4248 3152 4248 3152 Total (Watts): (c): (h): (m): (r): 12849 11753 12849 11753 Solar Array (Watts): (d): (i): (n): (s): 15878 14116 14271 12859 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? 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: 2004-07-29 07:54:34
Document Modified: 2004-07-29 07:54:34
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