Attachment Schedule S Tech Data

This document pretains to SAT-APL-20090115-00005 for Amendment of Permitted List App on a Satellite Space Stations filing.

IBFS_SATAPL2009011500005_694073

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 3F4 1/7/2009 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: 68 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 T Mobile-Satellite Service 1626.5 M 1660.5 M R Mobile-Satellite Service 6425 M 6454 M R Feeder Link for Mobile Satellite Service in FSS 3600 M 3629 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 6454.4 M 6456.6 M R Fixed Satellite Service 3629.4 M 3631.6 M T Fixed Satellite Service 1574.4 M 1576.6 M T Radio Navigation 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: 54 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-3 F4 satellite at 54 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 2.7 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. NC S NC_SA (54W).gxt North central part of visible areas of the Earth NW S NW_SA (54W).gxt North west part of visible areas of the Earth SC S SC_SA (54W).gxt South central part of visible areas of the Earth SE S SE_SA (54W).gxt South east part of visible areas of the Earth SW2 S SW2_SA (54W).gxt South west part of visible areas of the Earth SW S SW_SA (54W).gxt South west part of visible areas of the Earth NE S NE_SA (54W).gxt North east part of 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 0.1 0.1 30 N GLOBAL 891 -9 -172.1 24 2 CGU R 20.5 16.5 0.1 0.1 30 N GLOBAL 891 -9 -172.1 24 2 CGD T 20 16.5 0.1 0.1 30 N GLOBAL 3.3 10.5 30.5 CGD T 20 16.5 0.1 0.1 30 N GLOBAL 3.3 10.5 30.5 LRU R 34 30 0.1 0.1 N GLOBAL LRD T 34 30 0.1 0.1 N GLOBAL LGD T 19.5 17 0.1 0.1 N GLOBAL 4.1 159 41.5 LGU R 18.5 16 0.1 0.1 N GLOBAL 562 -9 -171.3 23 2 LND1 T 19 15.5 0.1 0.1 30 N GLOBAL 3 50 33 LRD1 T 28.2 25.2 0.1 0.1 N NC 3 210 51.4 CNU R 20.5 16.5 0.1 0.1 N GLOBAL 1585 -11.5 -172.1 24 2 LRD2 T 28.2 25.2 0.1 0.1 N NE 3 210 51.4 LRD3 T 28.2 25.2 0.1 0.1 N NW 3 210 51.4 LRD4 T 28.2 25.2 0.1 0.1 N SC 3 210 51.4 LRD5 T 28.2 25.2 0.1 0.1 N SE 3 210 51.4 LRD6 T 28.2 25.2 0.1 0.1 N SW2 3 210 51.4 LRD7 T 28.2 25.2 0.1 0.1 N SW 3 210 51.4 LRU1 R 28.2 25.2 0.1 0.1 N NC 740 -0.5 -171.3 24 2 LRU2 R 28.2 25.2 0.1 0.1 N NE 740 -0.5 -171.3 24 2 LRU3 R 28.2 25.2 0.1 0.1 N NW 740 -0.5 -171.3 24 2 LRU4 R 28.2 25.2 0.1 0.1 N SC 740 -0.5 -171.3 24 2 LRU5 R 28.2 25.2 0.1 0.1 N SE 740 -0.5 -171.3 24 2 LRU6 R 28.2 25.2 0.1 0.1 N SW2 740 -0.5 -171.3 24 2 LRU7 R 28.2 25.2 0.1 0.1 N SW 740 -0.5 -171.3 24 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 -54 CGU (54W).gxt CGU R C -54 CGU (54W).gxt CGD T C -54 CGD (54W).gxt -165.9 -165.7 -165.5 -165.2 -164.9 CGD T C -54 CGD (54W).gxt -165.9 -165.7 -165.5 -165.2 -164.9 LGD T C -54 LGD (54W).gxt LGU R C -54 LGU (54W).gxt LND1 T C -54 LND1 (54W).gxt LRD1 T C -54 LRD1 (LRDNC_54W).gxt LRD2 T C -54 LRD2 (LRDNE_54W).gxt LRD3 T C -54 LRD3 (LRDNW_54W).gxt LRD4 T C -54 LRD4 (LRDSC_54W).gxt LRD5 T C -54 LRD5 (LRDSE_54W).gxt LRD6 T C -54 LRD6 (LRDSW2_54W).gxt LRD7 T C -54 LRD7 (LRDSW_54W).gxt LRU1 R C -54 LRU1 (LRUNC_54W).gxt LRU2 R C -54 LRU2 (LRUNE_54W).gxt LRU3 R C -54 LRU3 (LRUNW_54W).gxt LRU4 R C -54 LRU4 (LRUSC_54W).gxt LRU5 R C -54 LRU5 (LRUSE_54W).gxt LRU6 R C -54 LRU6 (LRUSW2_54W).gxt LRU7 R C -54 LRU7 (LRUSW_54W).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) CXU 29000 R 6439.5 R C FL5 177 CXU CGUR LD LGD CYU 29000 R 6439.5 L C FL6 177 CYU CGUL LD LGD CXD 29000 T 3614.5 R C RL5 175 LU LGU CXD CGDR CYD 29000 T 3614.5 L C RL6 175 LU LGU CYD CGDL LU 34000 R 1643.5 R C CC1 141 CCU CGUL CCD CGDR LD 34000 T 1542 R C FL11 177 CXU CGUR LD LRD1 C1 2200 R 6455.5 R C FL12 177 CYU CGUL LD LRD1 L1 2200 T 1575.5 R C FL13 177 CXU CGUR LD LRD2 CCU 900 R 6432.75 L C FL14 177 CYU CGUL LD LRD2 CCD 900 T 3607.75 R C FL15 177 CXU CGUR LD LRD3 C1D 2200 T 3630.5 L C FL16 177 CYU CGUL LD LRD3 FL17 177 CXU CGUR LD LRD4 FL18 177 CYU CGUL LD LRD4 FL19 177 CXU CGUR LD LRD5 FL20 177 CYU CGUL LD LRD5 FL21 177 CXU CGUR LD LRD6 FL22 177 CYU CGUL LD LRD6 FL23 177 CXU CGUR LD LRD7 FL24 177 CYU CGUL LD LRD7 RL11 165 LU LRU1 CXD CGDR RL12 165 LU LRU1 CYD CGDL RL13 165 LU LRU2 CXD CGDR RL14 165 LU LRU2 CYD CGDL RL15 165 LU LRU3 CXD CGDR RL16 165 LU LRU3 CYD CGDL RL17 165 LU LRU4 CXD CGDR RL18 165 LU LRU4 CYD CGDL RL19 165 LU LRU5 CXD CGDR RL20 165 LU LRU5 CYD CGDL RL21 165 LU LRU6 CXD CGDR

RL22 165 LU LRU6 CYD CGDL RL23 165 LU LRU7 CXD CGDR RL24 165 LU LRU7 CYD CGDL NCL 169 C1 CGUR L1 LND1 NCC 141 C1 CGUR C1D CGDL

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 30 20K0G1E 20 4 12 0.5 5.1 17.3 31 100KG1X 100 4 64 0.5 5 17.2 32 10K0G1W 10 4 4 0.5 5 17.2 33 5K00G1E 5 4 2.8 0.5 5.4 17.6 34 60K0D1W 60 16 64 0.476 7.7 19.9 35 5K00G1W 5 4 3.6 0.643 5.4 17.6 36 5K00G1D 5 2 0.3 0.5 3.5 15.7 37 2K50F1D 2.5 2 0.001 0.242 -10.9 1.3 38 20K0G1E 20 4 12 0.5 5.1 17.3 39 100KG1X 100 4 64 0.5 5 17.2 40 10K0G1W 10 4 4 0.5 5 17.2 41 5K00G1E 5 4 2.8 0.5 5.4 17.6 42 60K0D1W 60 16 64 0.476 7.7 19.9 43 5K00G1W 5 4 3.6 0.643 5.4 17.6

44 5K00G1D 5 2 0.3 0.5 3.5 15.7 45 2K50F1D 2.5 2 0.064 0.5 2.3 14.5 46 180KG3X 180 2 4.8 0.5 11 23.2 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 56 7K50G1E 7.5 2 2.8 0.5 5.4 17.6 57 7K50G1D 7.5 2 10.5 0.5 5 17.2 58 12K5G1D 12.5 2 8.4 0.5 2.9 15.1 59 45K0G7D 45 4 64 0.5 7.7 19.9 60 45K0G7D 45 4 64 0.5 7.7 19.9 61 17K5G1D 17.5 2 9.6 0.5 4.5 16.7 62 45K0G7D 45 4 64 0.5 7.7 19.9 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 69 7K50G1E 7.5 2 2.8 0.5 5.4 17.6 70 7K50G1D 7.5 2 10.5 0.5 5 17.2 71 12K5G1D 12.5 2 8.4 0.5 2.9 15.1 72 45K0G7D 45 4 64 0.5 7.7 19.9 73 45K0G7D 45 4 64 0.5 7.7 19.9 74 17K5G1D 17.5 2 9.6 0.5 4.5 16.7 75 45K0G7D 45 4 64 0.5 7.7 19.9 76 100KN0N 100 1 15 27.2 77 100KN0N 100 1 15 27.2 78 200KG7W 200 2 320 0.875 9 21.2 79 2M20G1D 2200 2 1023 1 -28 -15.8

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 FL6 13 368 20 FLG INM-B 20 58.5 -7.9 -2.9 17.3 21.3 -4 FL5 FL6 14 112 100 FLG INM-B 100 58.5 -4.7 0.3 22.5 26.5 -4 FL5 FL6 15 2089 10 FLG INM-B 10 58.5 -15.4 -10.4 9.8 13.8 -4 FL5 FL6 16 288 10 FLG INM-M 10 58.5 -6.8 -1.8 18.4 22.4 -10 FL5 FL6 17 479 10 FLG INM-M 10 58.5 -9 -4 16.2 20.2 -10 FL5 FL6 18 135 10 FLG MINI-M 10 58.5 -3.5 1.5 21.7 25.7 -17 FL5 FL6 19 135 10 FLG M4 10 kHz 58.5 -3.5 1.5 21.7 25.7 -7 FL5 FL6 20 209 10 FLG INM-C.doc 58.5 -5.4 -0.4 19.8 23.8 -23 FL5 FL6 21 178 5 FLG INM-D.doc 58.5 -6.7 -1.7 20.5 24.5 -22.1 RL5 RL6 22 6300 20 RLG INM-B 20 21 5 12 -8.4 2.6 -165.2 33.2 RL5 RL6 23 1260 100 RLG INM-B 100 21 8 16 -1.4 8.6 -166.5 33.2 RL5 RL6 24 6300 20 RLG INM-B 20 21 4.3 13 -9.1 3.6 -164.2 33.2 RL5 RL6 25 12600 10 RLG INM-M 10 14 7 13 -13.4 -6.4 -169.4 33.2 RL5 RL6 26 6300 20 RLG INM-M 20 14 3 11 -17.4 -5.4 -167.2 33.2 RL5 RL6 27 6300 20 RLG MINI-M 20 10 3 7 -21.4 -13.4 -175.5 33.2 RL5 RL6 28 25200 5 RLG INM-C.doc 0 4 10.5 -23 -12.6 -174.7 33.2 RL5 RL6 29 25200 2.5 RLG INM-D.doc 3.5 -3 9 -30.2 -16.2 -178.3 33.2 FL11 FL24 30 6300 20 FLR INM-B 20 58.5 -8.7 -3.7 19.5 23.5 -4 FL11 FL24 31 1260 100 FLR INM-B 100 58.5 -3.7 1.3 24.5 28.5 -4 FL11 FL24 32 4898 10 FLR INM-M 10 58.5 -7.1 -2.1 21.1 25.1 -12 FL11 FL24 33 17378 5 FLR MINI-M 5 k 58.5 -4 1 15.6 19.6 -7 FL11 FL24 34 832 60 FLR M4 60 kHz 58.5 0.6 5.6 28.8 32.8 -7 FL11 FL24 35 17378 5 FLR M4 5 kHz. 58.5 -12.6 -7.6 15.6 19.6 -7 FL11 FL24 35 6166 5 FLR INM-C.doc 58.5 -8.1 -3.1 20.1 24.1 -23 FL11 FL24 37 5623 5 FLR INM-D.doc 58.5 -9.1 -4.1 20.5 24.5 -22.1 RL11 RL24 38 6300 20 RLR INM-B 20 21 -3.3 5 -10.7 1.6 -166.2 33.2 RL11 RL24 39 1260 100 RLR INM-B 100 21 -0.2 13 -3.6 13.3 -160.8 33.2 RL11 RL24 40 12600 10 RLR INM-M 10 12 0.8 9 -15.6 -3.4 -166.4 33.2 RL11 RL24 41 25200 5 RLR MINI-M 5 18 -9.5 -1 -16.9 -2.2 -165.9 33.2

RL11 RL24 42 2100 60 RLR M4 60 kHz 18 4 11 -3.4 1.4 -170.7 33.2 RL11 RL24 43 25200 5 RLR M4 5 kHz. 18 -9.5 -1 -16.9 -2.2 -165.9 33.2 RL11 RL24 44 25200 5 RLR INM-C.doc 0 1.2 10.5 -25.4 -12 -174.1 33.2 RL11 RL24 45 25200 2.5 RLR INM-D.doc 3.5 -5.7 5.5 -25 -8.8 -170.9 33.2 FL5 FL6 50 186 7.5 FLG AERO-H 7 58.5 -4.9 0.1 20.3 24.3 -13 FL5 FL6 51 112 5 FLG AERO-I 5 58.5 -2.7 2.3 22.5 26.5 -19 FL5 FL6 52 58 2.5 FLG AERO-L 2. 58.5 0.2 5.2 25.4 29.4 -26 FL5 FL6 53 68 45 FLG F77 45 kH 58.5 -3.5 1.5 24.7 25.7 -4 FL5 FL6 54 1023 5 FLG F55 5kHz. 58.5 -13.3 -8.3 12.9 15.9 -7 FL5 FL6 55 323 7.5 FLG F33 7.5 k 58.5 -7.8 -2.8 17.4 21.4 -12.5 FL11 FL24 56 2399 7.5 FLR MINI-M 7.5 58.5 -4 1 24.2 28.2 -17 FL11 FL24 57 6457 7.5 FLR AERO-H 7 58.5 -8.9 -3.9 19.9 23.9 -13 FL11 FL24 58 2042 12.5 FLR AERO-I 12 58.5 -4.2 0.8 24.9 28.9 -19 FL11 FL24 59 2291 45 FLR F77 45 kH 58.5 -3.8 1.2 24.4 28.4 -4 FL11 FL24 60 1175 45 FLR F55 45 kH 58.5 -0.9 4.1 27.3 31.3 -7 FL11 FL24 61 1778 17.5 FLR F33 17.5 k 58.5 -2.7 2.3 25.5 29.5 -12.5 FL11 FL24 62 603 45 FLR SWIFT64 58.5 2 7 30.2 34.2 -13 RL5 RL6 63 5623 7.5 RLG AERO-H 7 12 7.6 13.5 -6.5 3.5 -160.7 33.2 RL5 RL6 64 13183 5 RLG AERO-I 5 6 9.9 16 -10.2 -0.2 -162.3 33.2 RL5 RL6 65 18577 2.5 RLG AERO-L 2 0 11.8 13.5 -14.7 -9 -169 33.2 RL5 RL6 66 851 45 RLG F77 45 kH 20 10 12 1.7 7.7 -164.4 33.2 RL5 RL6 67 13490 5 RLG F55 5 kHz 17 3 8 -10.3 -1.3 -163.4 33.2 RL5 RL6 68 13490 5 RLG F33 5 kHz 11.5 8.5 13.5 -10.3 -1.3 -163.4 33.2 RL11 RL24 69 16800 7.5 RLR MINI-M 7. 10 -1.5 7 -16.9 -4.5 -166.6 33.2 RL11 RL24 70 11749 7.5 RLR AERO-H 7 12 2 7.5 -9.7 0.8 -163.4 33.2 RL11 RL24 71 10080 12.5 RLR AERO-I 12 6 6.7 7.5 -11.8 -7 -171.3 33.2 RL11 RL24 72 955 45 RLR F77 45 kH 20 3.6 12 1.2 9.6 -162.5 33.2 RL11 RL24 73 955 45 RLR F55 45 kH 17 6.6 11.6 1.2 6.2 -165.9 33.2 RL11 RL24 74 5248 17.5 RLR F33 17.5 k 11.5 3.7 9.5 -6.2 -1.4 -169.2 33.2 RL11 RL24 75 933 45 RLR SWIFT64 11.5 9.2 13.5 1.3 5.6 -166.5 33.2 FL5 FL6 76 4 100 FLG AFC.doc 58.5 -13.5 4.5 10 15 19.2 RL5 RL6 77 4 100 RLG AFC.doc 43.9 -12.9 -2.9 -9 -4 33.2 CC1 CC1 78 25 200 CtoC.doc 58.5 8.5 13.5 1.7 5.7 -173.4 33.2 NCC NCC 79 1 Nav C-C LB (I3) 57 17 21 -0.2 3.5 -185.6 32 NCL NCL 79 1 Nav C-L LB (I3) 57 17 21 29.5 33 -26

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: 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: S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: 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: 2009-02-03 15:57:02
Document Modified: 2009-02-03 15:57:02
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