Attachment Schedule S Tech Data

This document pretains to SES-AMD-20050617-00772 for Amended Filing on a Satellite Earth Station filing.

IBFS_SESAMD2005061700772_441412

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: HISPASAT-1C 2/3/2000 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 12 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: 432 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) 13750.00 M 14000.00 M R Digital Data, Video, and Internet Services from 64 Kbps to 45 Mbps 11700.00 M 12200.00 M T Digital Data, Video, and Internet Services from 64 Kbps to 45 Mbps 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: 30 W The HISPASAT-1C satellite is operated at 30 degrees Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be West longitude orbital location. Operation of the N/S Station-Keeping provided (Optional): HISPASAT-1C satellite has been coordinated with the d. Toward West: Degrees E/W 0.07 Degrees Tolerance: United States. In fact, the American beams have g. Westernmost: e. Toward East: 0.07 Degrees already notified in from the ITU under the HISPASAT 0.05 Degrees h. Easternmost: 2C3KU filing. 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) Please see Attachment. All .gxt files are listed and described in the S6 attachment, and are attached to this appli

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) AME R 31.4 26.9 0.07 0.05 31 N AMERICA 530 4.1 -96 15 1 AME- R 31.4 26.9 0.07 29 N AMERICA 530 4.1 -96 15 1 AME- T 31.2 26.7 0.07 31 N AMERICA 1.7 48 AME- T 31.2 26.7 0.07 29 N AMERICA 1.7 48

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) AME R C -30 AMEKU_R_HC.gxt AME R X -30 AMEKU_R_HX.gxt AME- R C -30 AMEKU_R_VC.gxt AME- R X -30 AMEKU_R_VX.gxt AME- T C -30 AMEKU_T_HC.gxt AME- T X -30 AMEKU_T_HX.gxt AME- T C -30 AMEKU_T_VC.gxt AME- T X -30 AMEKU_T_VX.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) 53R 36000 R 13772 V C 53 125 53R AMER 53T AME-3 53T 36000 T 11972 H C 54 125 54R AMER 54T AME-3 54R 36000 R 13812 V C 55 125 55R AMER 55T AME-3 54T 36000 T 12012 H C 56 125 56R AMER 56T AME-3 55R 36000 R 13852 V C 57 125 57R AMER 57T AME-3 55T 36000 T 12052 H C 58 125 58R AMER 58T AME-3 56R 36000 R 13892 V C 59 125 59R AMER 59T AME-3 56T 36000 T 12092 H C 60 125 60R AMER 60T AME-3 57R 36000 R 13772 H C 61 125 61R AMER 61T AME-3 57T 36000 T 11972 V C 62 125 62R AMER 62T AME-3 58R 36000 R 13812 H C 63 125 63R AMER 63T AME-3 58T 36000 T 12012 V C 64 125 64R AMER 64T AME-3 59R 36000 R 13852 H C BEAC 125 BEAC. AMER BEAC. AME-3 59T 36000 T 12052 V C TC 125 TC AMER TC AME-3 60R 36000 R 13892 H C TM 125 TM AMER TM AME-3 60T 36000 T 12092 V C S/TC 125 S/TC AMER S/TC AME-3 61R 36000 R 13932 V C S/TM 125 S/TM AMER S/TM AME-3 61T 36000 T 12132 H C 62R 36000 R 13972 H C 62T 36000 T 12172 H C 63R 36000 R 13932 H C 63T 36000 T 12132 V C 64R 36000 R 13932 H C 64T 36000 T 12172 V C BEAC. 500 T 11702 H T TC 1400 R 14000 H T TM 500 T 12748.25 H T S/TC 600 R 2052.0 R T S/TM 600 R 2228.4163 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) 64K 76K8G1X 76.8 64 5 14.8 TO 45K 36M0G7X 36000 45000 7.6 15.9

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)

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) 53 64 64K 311 7070 57.2 15.2 25.2 44.3 47.3 -130.6 22 53 64 45K 1 55 -10 -2 17 20 -130.6 19.2

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: S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Arganda S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): ATTACHMENT

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: 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): 7300 6300 Bus (Watts): (b): (g): (l): (q): Total (Watts): (c): (h): (m): (r): Solar Array (Watts): (d): (i): (n): (s): Depth of Battery (e) (j) (o) (t) Discharge (%): 75.5 % % 70.68 % % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO X 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? YES NO X 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: 2005-07-14 17:39:36
Document Modified: 2005-07-14 17:39:36
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