Attachment Schedule S Tech Data

This document pretains to SES-LFS-20050930-01352 for License to use Foreign Satellite (earth) on a Satellite Earth Station filing.

IBFS_SESLFS2005093001352_457875

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: INMARSAT 4F2 12/31/2005 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/1/2001 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 6/1/2005 1260 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: 10/1/2005 10/31/2005 252 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) 1525 M 1559 M R Mobile-Satellite Service 1626.5 M 1660.5 M T Mobile-Satellite Service 6425 M 6515.8 M R Feeder Link for Mobile Satellite Service in FSS 3564.2 M 3657.8 M T Feeder Link for Mobile Satellite Service in FSS 6338 M 6342 M R Fixed Satellite Service 3945 M 3955 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: 52.75 W The Inmarsat 4F2 satellite will operate at the Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be 52.75°W.L. geostationary orbital location. The N/S Station-Keeping provided (Optional): Inmarsat 4F2 satellite will replace the Inmarsat 3 d. Toward West: Degrees E/W 0.1 Degrees Tolerance: satellite, which currently operates at 54°W.L. and for g. Westernmost: e. Toward East: 0.1 Degrees which the Commission has already authorized the 3 Degrees h. Easternmost: provision of service. This orbital location optimizes i. Reason for service are selection (Optional): Atlantic Ocean coverage while complementing the coverage provided by the Inmarsat 4F1 satellite at 64°E.L.

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) GLOBAL S All visible areas of the Earth.

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) CGU R 22 18 0.2 0.1 30 N GLOBAL 692 -6.4 -174.7 16 1 CGU R 22 18 0.2 0.1 30 N GLOBAL 692 -6.4 -174.7 16 1 CGD T 22 18 0.2 0.1 30 N GLOBAL 3.4 20.1 35 CGD T 22 18 0.2 0.1 30 N GLOBAL 3.4 20.1 35 LSU R 42 39 0.2 0.1 N GLOBAL 583 14.3 -188.8 16 2 LRU R 34 30 0.2 0.1 N GLOBAL 1259 3 -168.8 16 2 LSD T 42 39 0.2 0.1 N GLOBAL 4.1 631 70 LRD T 34 30 0.2 0.1 N GLOBAL 4.1 251.2 58 LGD T 22 18 0.2 0.1 N GLOBAL 4.1 125.9 43 TCN R 9 1.5 0.2 0.1 30 N GLOBAL 501 -18 -175.1 TCNL R 9 1.5 0.2 0.1 30 N GLOBAL 501 -18 -175.1 CRD T 22 18 0.2 0.1 30 N GLOBAL 3.5 0.355 17.5 CRD T 22 18 0.2 0.1 30 N GLOBAL 3.5 0.355 17.5

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) CGU R C -52.75 CGUR.GXT CGU R C -52.75 CGUL.GXT CGD T C -52.75 CGDR.GXT -169.5 -169.3 -169.1 -168.8 -168.5 CGD T C -52.75 CGDL.GXT -169.5 -169.3 -169.1 -168.8 -168.5 LSU R C -52.75 LSU.GXT LRU R C -52.75 LRU.GXT LSD T C -52.75 LSD.GXT LRD T C -52.75 LRD.GXT LGD T C -52.75 LGD.GXT TCN R C -52.75 TCNR.GXT TCNL R C -52.75 TCNL.GXT CRD T C -52.75 CRDR.GXT -170.9 -170.7 -170.5 -170.2 -169.9 CRD T C -52.75 CRDL.GXT -170.9 -170.7 -170.5 -170.2 -169.9

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) CXU 90800 R 6470.4 R C FL1 192 CXU CGUR LD LSD CYU 90800 R 6470.4 L C FL2 192 CYU CGUL LD LSD CXD 106400 T 3604.6 R C FL3 176 CXU CGUR LD LRD CYD 106400 T 3604.6 L C FL4 176 CYU CGUL LD LRD LU 34000 R 1542 R C FL5 176 CXU CGUR LD LGD LD 34000 T 1643.5 R C FL6 176 CYU CGUL LD LGD TLCR 4000 R 6340 R T RL1 192 LU LSU CXD CGDR TLCL 4000 R 6340 L T RL2 192 LU LSU CYD CGDL TLMR 10000 T 3950 R T RL3 176 LU LRU CXD CGDR TLML 10000 T 3950 L T RL4 176 LU LRU CYD CGDL TC1 TLCR TCNR TC2 TLCL TCNL TM1 TLMR CRDR

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) C1F2 200KD7W 200 16 492 0.822 12.3 24.5 C2F2 200KD7W 200 16 464 0.775 11.4 23.6 C3F2 200KD7W 200 16 384 0.642 9.1 21.3 C1F3 50K0D7W 50 16 98 0.766 11.4 23.6 C2F3 50K0D7W 50 16 90 0.703 10.3 22.5 C3F3 50K0G7W 50 4 49.2 0.796 5.4 17.6 C1F4 12K5G7W 12.5 4 12.2 0.897 8.1 20.3 C2F4 12K5G7W 12.5 4 12.2 0.897 8.1 20.3 C3F4 12K5G7W 12.5 4 12.2 0.897 8.1 20.3 C1R3 50K0D7W 50 16 101.6 0.852 12 24.2 C2R3 50K0G7W 50 4 52.8 0.87 6.6 18.8 C3R3 25K0G7W 25 4 20 0.73 4.4 16.6 C1RT 200KD7W 200 16 492.8 0.852 12.7 24.9 C2RT 200KD7W 200 16 448 0.775 10.8 23 C3RT 200KG7W 200 4 239.6 0.83 4.8 17

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) FL1 FL2 C1F2 630 200 C1F2 LB.doc 57 -4.7 0.3 41.5 44.5 -9.7 FL1 FL2 C2F2 630 200 C2F2 LB.doc 57 -4.7 0.3 41.5 44.5 -12.5 FL1 FL2 C3F2 630 200 C3F2 LB.doc 57 -4.7 0.3 41.5 44.5 -16.9 FL3 FL4 C1F3 2520 50 C1F3 LB.doc 57 -1 4 29.2 33.2 -9.7 FL3 FL4 C2F3 2520 50 C2F3 LB.doc 57 -1 4 29.2 33.2 -12.5 FL3 FL4 C3F3 2520 50 C3F3 LB.doc 57 -1 4 29.2 33.2 -16.9 FL5 FL6 C1F4 1 C1F4 LB.doc 57 -1.7 3.3 29 33 -9.7 FL5 FL6 C2F4 1 C2F4 LB.doc 57 -1.7 3.3 29 33 -12.5 FL5 FL6 C3F4 1 C3F4 LB.doc 57 -1.7 3.3 29 33 -16.9 RL1 RL2 C1R3 2520 50 C1R3 LB.doc 16 2 5 -0.5 6.5 -165.8 32.3 RL1 RL2 C2R3 2520 50 C2R3 LB.doc 13 0.1 3.1 -6.5 1.6 -170.7 32.3 RL1 RL2 C3R3 5040 25 C3R3 LB.doc 8 0 3 -11.7 -3.5 -172.8 32.3 RL3 RL4 C1RT 630 200 C1RT LB.doc 16 2 5 5 14.5 -164.3 32.3 RL3 RL4 C2RT 630 200 C2RT LB.doc 13 0.1 3.1 5 9.6 -169.2 32.3 RL3 RL4 C3RT 630 200 C3RT LB.doc 8 0 3 -2 4.5 -174.3 32.3

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): Yes Remote Control (TT C) Location(s): S14a: Street Address: c/o Telespazio, Stazione del Fucino P.Fanti S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: ORTUCCHIO L'AQUILA 67050 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +39 0863 5501

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 3340 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2619 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5959 18 0.74 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 350 45 0.89 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 89.3 8 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): 8981 8981 8981 8981 Bus (Watts): (b): (g): (l): (q): 840 596 840 596 Total (Watts): (c): (h): (m): (r): 11635 10423 11696 10423 Solar Array (Watts): (d): (i): (n): (s): 14086 13208 13388 12038 Depth of Battery (e) (j) (o) (t) Discharge (%): 68 % 0 % 72 % 12 % 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: 2005-10-03 12:11:04
Document Modified: 2005-10-03 12:11:04
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