Attachment Schedule S Tech Data

This document pretains to SES-AMD-20081215-01614 for Amended Filing on a Satellite Earth Station filing.

IBFS_SESAMD2008121501614_684308

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 2F1 11/22/2008 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 4 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: 10/1/1991 10/31/1991 23 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) 1530 M 1548 M T Mobile-Satellite Service 1626.5 M 1649.5 M R Mobile-Satellite Service 6425 M 6443 M R Feeder Link for Mobile Satellite Service in FSS 3600 M 3623 M T Feeder Link for Mobile Satellite Service in FSS 6170 M 6180 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: 142 W Inmarsat is authorized by the United Kingdom to Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be operate the Inmarsat-2 F1 satellite at 142 W.L. N/S Station-Keeping provided (Optional): d. Toward West: Degrees E/W 0.1 Degrees Tolerance: g. Westernmost: e. Toward East: 0.1 Degrees 3 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) 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 20.5 16.5 0.2 0.1 30 N GLOBAL 891 -9 CGD T 20.5 17 0.2 0.1 30 N GLOBAL 3.5 4.5 27 LGD T 18.5 17 0.2 0.1 N GLOBAL 3 112.2 39 TCN R 2 0 0.2 0.1 30 N GLOBAL 1500 -29.8 LGU R 18.5 16 0.2 0.1 N GLOBAL 562 -9 TLML T 0 -3 0.2 0.1 30 N GLOBAL 3.5 0.38 -4.2

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 -142 I2_CGUR (142W).gxt CGD T C -142 I2_CGDL (142W).gxt -165.9 -165.7 -165.5 -165.2 -164.9 LGD T C -142 I2_LGD (142W).gxt TCN R C -142 I2_TNCR (142W).gxt LGU R C -142 I2_LGU (142W).gxt TLML T C -142 I2_TML (142W).gxt -171.4 -171.4 -171.3 -171.2 -171.1

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 18000 R 6434 R C FL5 176 CXU CGUR LD LGD CYD 23000 T 3611.5 L C RL6 176 LU LGU CYD CGDL LU 23000 R 1638 R C TC TLCR TCNR LD 18000 T 1539 R C TM TLML TLML TLCR 10000 R 6175 R T TLML 10000 T 3950 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) 13 20K0G1E 20 4 12 0.5 5.1 17.3 14 100KG1X 100 4 64 0.5 5 17.2 15 10K0G1X 10 2 3 0.5 0.6 12.8 16 10K0G1W 10 4 4 0.5 5 17.2 17 10K0G1X 10 2 3 0.5 2.8 15 18 10K0G1X 10 2 3 0.5 2.8 15 19 10K0G1X 10 2 3 0.5 2.8 15 20 5K00G1D 5 2 0.3 0.5 3.5 15.7 21 2K50F1D 2.5 2 0.001 0.242 -10.9 1.3 22 20K0G1E 20 4 12 0.5 5.1 17.3 23 100KG1X 100 4 64 0.5 5 17.2 24 20K0G1X 20 4 12 0.5 4.4 16.6 25 10K0G1W 10 4 4 0.5 5 17.2 26 20K0G1X 20 2 1.5 0.5 1.7 13.9 27 20K0G1X 20 2 1.5 0.5 1.2 13.4 28 5K00G1D 5 2 0.3 0.5 3.5 15.7 29 2K50F1D 2.5 2 0.064 0.5 -3.7 8.5 50 7K50G1D 7.5 2 10.5 0.5 5 17.2 51 5K00G1D 5 2 4.8 0.5 4.7 16.9 52 2K50G1D 2.5 2 1.2 0.5 3.2 15.4 53 45K0G7D 45 4 64 0.5 7.7 19.9 54 5K00G1W 5 2 4.8 0.5 5.4 17.6 55 7K50G1W 7.5 2 4.8 0.5 5.4 17.6 63 7K50G1D 7.5 2 10.5 0.5 5 17.2 64 5K00G1D 5 2 4.8 0.5 4.7 16.9 65 2K50G1D 2.5 2 1.2 0.5 3.2 15.4 66 45K0G7D 45 4 64 0.5 7.7 19.9 67 5K00G1W 5 2 4.8 0.5 5.4 17.6 68 5K00G1W 5 2 4.8 0.5 5.4 17.6 76 100KN0N 100 1 15 27.2 77 100KN0N 100 1 15 27.2


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) FL5 FL5 13 368 20 FLG INM-B 20 58.5 -7.9 -2.9 17.3 21.3 -4 FL5 FL5 14 112 100 FLG INM-B 100 58.5 -4.7 0.3 22.5 26.5 -4 FL5 FL5 15 2089 10 FLG INM-B 10 58.5 -15.4 -10.4 9.8 13.8 -4 FL5 FL5 16 288 10 FLG INM-M 10 58.5 -6.8 -1.8 18.4 22.4 -10 FL5 FL5 17 479 10 FLG INM-M 10 58.5 -9 -4 16.2 20.2 -10 FL5 FL5 18 135 10 FLG MINI-M 10 58.5 -3.5 1.5 21.7 25.7 -17 FL5 FL5 19 135 10 FLG M4 10 kHz 58.5 -3.5 1.5 21.7 25.7 -7 FL5 FL5 20 209 10 FLG INM-C.doc 58.5 -5.4 -0.4 19.8 23.8 -23 FL5 FL5 21 178 5 FLG INM-D.doc 58.5 -6.7 -1.7 20.5 24.5 -22.1 RL6 RL6 22 6300 20 RLG INM-B 20 21 5 12 -8.4 2.6 -165.2 33.2 RL6 RL6 23 1260 100 RLG INM-B 100 21 8 16 -1.4 8.6 -166.5 33.2 RL6 RL6 24 6300 20 RLG INM-B 20 21 4.3 13 -9.1 3.6 -164.2 33.2 RL6 RL6 25 12600 10 RLG INM-M 10 14 7 13 -13.4 -6.4 -169.4 33.2 RL6 RL6 26 6300 20 RLG INM-M 20 14 3 11 -17.4 -5.4 -167.2 33.2 RL6 RL6 27 6300 20 RLG MINI-M 20 10 3 7 -21.4 -13.4 -175.5 33.2 RL6 RL6 28 25200 5 RLG INM-C.doc 0 4 10.5 -23 -12.6 -174.7 33.2 RL6 RL6 29 25200 2.5 RLG INM-D.doc 3.5 -3 9 -30.2 -16.2 -178.3 33.2 FL5 FL5 50 186 7.5 FLG AERO-H 7 58.5 -4.9 0.1 20.3 24.3 -13 FL5 FL5 51 112 5 FLG AERO-I 5 58.5 -2.7 2.3 22.5 26.5 -19 FL5 FL5 52 58 2.5 FLG AERO-L 2. 58.5 0.2 5.2 25.4 29.4 -26 FL5 FL5 53 68 45 FLG F77 45 kH 58.5 -3.5 1.5 24.7 25.7 -4 FL5 FL5 54 1023 5 FLG F55 5kHz. 58.5 -13.3 -8.3 12.9 15.9 -7 FL5 FL5 55 323 7.5 FLG F33 7.5 k 58.5 -7.8 -2.8 17.4 21.4 -12.5 RL6 RL6 63 5623 7.5 RLG AERO-H 7 12 7.6 13.5 -6.5 3.5 -160.7 33.2 RL6 RL6 64 13183 5 RLG AERO-I 5 6 9.9 16 -10.2 -0.2 -162.3 33.2 RL6 RL6 65 18577 2.5 RLG AERO-L 2 0 11.8 13.5 -14.7 -9 -169 33.2 RL6 RL6 66 851 45 RLG F77 45 kH 20 10 12 1.7 7.7 -164.4 33.2 RL6 RL6 67 13490 5 RLG F55 5 kHz 17 3 8 -10.3 -1.3 -163.4 33.2 RL6 RL6 68 13490 5 RLG F33 5 kHz 11.5 8.5 13.5 -10.3 -1.3 -163.4 33.2

FL5 FL5 76 4 100 FLG AFC.doc 58.5 -13.5 4.5 10 15 19.2 RL6 RL6 77 4 100 RLG AFC.doc 43.9 -12.9 -2.9 -9 -4 33.2

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): Yes Remote Control (TT C) Location(s): S14a: Street Address: 24 Unity Drive North S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Auckland 1331 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +64 9 913 3800

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 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 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): 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 (%): % % % % 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: 2008-12-16 10:38:22
Document Modified: 2008-12-16 10:38:22
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