Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20060821-00090 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2006082100090_521807

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: SOLIDARIDAD 2 8/1/2006 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 14.5 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 34 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: 10/7/1994 1728 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) 5925 M 6425 M R Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 11700 M 12200 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: 114.9 W The orbital location is consistent with the Trilateral Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Agreement between Canada, Mexico and the United N/S Station-Keeping provided (Optional): States of America. 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) SA1 S -6 dB contour of beam C1UH SA2 S -6 dB contour of beam C1DV SA3 S -6 dB contour of beam C2UH SA4 S -6 dB contour of beam C2DV SA5 S -6 dB contour of beam C3UH SA6 S -6 dB contour of beam C3DV SA7 S -6 dB contour of beam C4UV SA8 S -6 dB contour of beam C4DH SA9 S -6 dB contour of beam K1UV SA10 S -6 dB contour of beam K1UH SA11 S -6 dB contour of beam K1DH SA12 S -6 dB contour of beam K1DV SA13 S -6 dB contour of beam K2UV SA14 S -6 dB contour of beam K2DH SA15 S Visible 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) C1U R 37 31 0.13 0 33 N 0 SA1 465 10.3 -96 14 2 C1D T 32.9 26.9 0.13 0 33 N 90 SA2 1.6 6.9 41.3 C2U R 33.4 27.4 0.13 0 33 N 0 SA3 450 6.8 -93 14 2 C2D T 30.9 23.9 0.13 0 33 N 90 SA4 1.7 9.5 40.7 C3U R 35.4 29.4 0.13 0 33 N 0 SA5 580 7.8 -93 14 2 C3D T 31.1 25.1 0.13 0 33 N 90 SA6 1.8 6.6 39.3 C4U R 35.9 29.9 0.13 0 33 N 90 SA7 650 7.8 -94 14 2 C4D T 33.8 27.8 0.13 0 33 N 0 SA8 1.6 9.8 43.7 K1UV R 38.8 32.8 0.13 0 33 N 90 SA9 685 10.5 -97 22 2 K1U R 38.8 32.8 0.13 0 33 N 0 SA10 685 10.5 -97 22 2 K1D T 36.7 30.7 0.13 0 33 N 0 SA11 1.3 31.6 51.7 K1DV T 36.7 30.7 0.13 0 33 N 90 SA12 1.3 31.6 51.7 K2UV R 40.2 34.2 0.13 0 33 N 90 SA13 740 11.5 -94 22 2 K2D T 38.5 32.5 0.13 0 33 N 0 SA14 1.8 27.5 52.9 OMNI R 2 0 0.13 0 30 N 0 SA15 9600 -37.8 OMNI T 2 0 0.13 0 30 N 90 SA15 3 3.8 7.8

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) C1U R C -114.9 C1UH.gxt C1D T C -114.9 C1DV.gxt -169 -168.9 -168.8 -168.7 -168.6 C2U R C -114.9 C2UH.gxt C2D T C -114.9 C2DV.gxt -157.6 -156.8 -155.7 -154.3 -152.9 C3U R C -114.9 C3UH.gxt C3D T C -114.9 C3DV.gxt -152 -151.7 -151.3 -151 -150.7 C4U R C -114.9 C4UV.gxt C4D T C -114.9 C4DH.gxt -168.6 -168.4 -166.3 -166.2 -166.1 K1UV R C -114.9 K1UV.GXT K1U R C -114.9 K1UH.GXT K1D T C -114.9 K1DH.GXT K1DV T C -114.9 K1DV.GXT K2UV R C -114.9 K2UV.gxt K2D T C -114.9 K2DH.gxt OMNI T C -114.9 -167.7 -167.7 -167.7 -167.7 -167.7

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) CU001 36000 R 5945 H C C0001 105 CU001 C1UH CD001 C1DV CU002 36000 R 5985 H C C0002 105 CU002 C1UH CD002 C1DV CU003 36000 R 6025 H C C0003 105 CU003 C1UH CD003 C1DV CU004 36000 R 6065 H C C0004 105 CU004 C1UH CD004 C1DV CU005 36000 R 6105 H C C0005 105 CU005 C1UH CD005 C1DV CU006 36000 R 6145 H C C0006 105 CU006 C1UH CD006 C1DV CU007 36000 R 6185 H C C0007 105 CU007 C1UH CD007 C1DV CU008 36000 R 6225 H C C0008 105 CU008 C1UH CD008 C1DV CU009 36000 R 6265 H C C0009 105 CU009 C1UH CD009 C1DV CU010 36000 R 6305 H C C0010 105 CU010 C1UH CD010 C1DV CU011 36000 R 6345 H C C0011 105 CU011 C1UH CD011 C1DV CU012 36000 R 6385 H C C0012 105 CU012 C1UH CD012 C1DV CU013 72000 R 5985 V C C0013 105 CU013 C4UV CD013 C4DH CU014 72000 R 6065 V C C0014 105 CU014 C4UV CD014 C4DH CU015 72000 R 6145 V C C0015 105 CU015 C4UV CD015 C4DH CU016 72000 R 6225 V C C0016 105 CU016 C4UV CD016 C4DH CU017 72000 R 6305 V C C0017 105 CU017 C4UV CD017 C4DH CU018 72000 R 6385 V C C0018 105 CU018 C4UV CD018 C4DH CD001 36000 T 3720 V C C0019 106 CU006 C1UH CD006 C2DV CD002 36000 T 3760 V C C0020 106 CU008 C1UH CD008 C2DV CD003 36000 T 3800 V C C0021 106 CU010 C1UH CD010 C2DV CD004 36000 T 3840 V C C0022 106 CU012 C1UH CD012 C2DV CD005 36000 T 3880 V C C0023 105 CU005 C1UH CD005 C3DV CD006 36000 T 3920 V C C0024 105 CU007 C1UH CD007 C3DV CD007 36000 T 3960 V C C0025 105 CU009 C1UH CD009 C3DV CD008 36000 T 4000 V C C0026 105 CU011 C1UH CD011 C3DV CD009 36000 T 4040 V C C0027 107 CU006 C2UH CD006 C2DV CD010 36000 T 4080 V C C0028 107 CU008 C2UH CD008 C2DV CD011 36000 T 4120 V C C0029 107 CU010 C2UH CD010 C2DV CD012 36000 T 4160 V C C0030 107 CU012 C2UH CD012 C2DV

CD013 72000 T 3760 H C C0031 105 CU005 C2UH CD005 C3DV CD014 72000 T 3840 H C C0032 105 CU007 C2UH CD007 C3DV CD015 72000 T 3920 H C C0033 105 CU009 C2UH CD009 C3DV CD016 72000 T 4000 H C C0034 105 CU011 C2UH CD011 C3DV CD017 72000 T 4080 H C C0035 105 CU006 C3UH CD006 C2DV CD018 72000 T 4160 H C C0036 105 CU008 C3UH CD008 C2DV KU001 54000 R 14030 V C C0037 105 CU010 C3UH CD010 C2DV KU002 54000 R 14091 V C C0038 105 CU012 C3UH CD012 C2DV KU003 54000 R 14152 V C C0039 103 CU005 C3UH CD005 C3DV KU004 54000 R 14213 V C C0040 103 CU007 C3UH CD007 C3DV KU005 54000 R 14274 V C C0041 103 CU009 C3UH CD009 C3DV KU006 54000 R 14335 V C C0042 103 CU011 C3UH CD011 C3DV KU007 54000 R 14396 V C K0001 118 KU001 K1UV KD001 K1DH KU008 54000 R 14457 V C K0002 118 KU002 K1UV KD002 K1DH KU009 54000 R 14043 H C K0003 118 KU003 K1UV KD003 K1DH KU010 54000 R 14104 H C K0004 118 KU004 K1UV KD004 K1DH KU011 54000 R 14165 H C K0005 118 KU005 K1UV KD005 K1DH KU012 54000 R 14226 H C K0006 118 KU006 K1UV KD006 K1DH KU013 54000 R 14287 H C K0007 118 KU007 K1UV KD007 K1DH KU014 54000 R 14348 H C K0008 118 KU008 K1UV KD008 K1DH KU015 54000 R 14409 H C K0009 118 KU009 K1UH KD009 K1DV KU016 54000 R 14470 H C K0010 118 KU010 K1UH KD010 K1DV KD001 54000 T 11730 H C K0011 118 KU011 K1UH KD011 K1DV KD002 54000 T 11791 H C K0012 118 KU012 K1UH KD012 K1DV KD003 54000 T 11852 H C K0013 118 KU013 K1UH KD013 K1DV KD004 54000 T 11913 H C K0014 118 KU014 K1UH KD014 K1DV KD005 54000 T 11974 H C K0015 118 KU015 K1UH KD015 K1DV KD006 54000 T 12035 H C K0016 118 KU016 K1UH KD016 K1DV KD007 54000 T 12096 H C K0017 113 KU006 K2UV KD006 K2DH KD008 54000 T 12157 H C K0018 113 KU008 K2UV KD006 K2DH KD009 54000 T 11743 V C TC1 TC1 C4UV KD010 54000 T 11804 V C TC2 TC2 OMNIH KD011 54000 T 11865 V C TM1 TM1 C4DH KD012 54000 T 11926 V C TM2 TM2 C4DH KD013 54000 T 11987 V C TM3 TM3 OMNIV KD014 54000 T 12048 V C TM4 TM4 OMNIV KD015 54000 T 12109 V C BCN1 BCN1 K1DH KD016 54000 T 12170 V C BCN2 BCN2 K1DV TC1 600 R 5935 V T

TC2 600 R 6415 H T TM1 350 T 3700.6 H T TM2 350 T 3701.1 H T TM3 350 T 3700.6 V T TM4 350 T 3701.1 V T BCN1 25 T 11701 H T BCN2 25 T 11701 V 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) D1 146KG7W 145.9 4 128 0.5 5.9 18.1 D2 1M56G7W 1556.5 4 2048 0.75 8.2 20.4 D3 5M56G7W 5563.2 4 7320 0.75 8.2 20.4 D4 36M0G7W 36000 4 41468 0.691 6.1 18.3

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) A1 36M0F9F 36000 TV/FM 1 NTSC 12.8 1.29 12 26

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) C0001 C0012 D1 180 200 146k C1-C1.do 47.5 -7.5 -1.5 7.4 13.4 -164.6 24.6 C0001 C0012 D2 17 2100 1.56M C1-C1.d 47.5 2.8 8.8 17.7 23.7 -164.5 28.5 C0001 C0012 D3 4 7500 5.56M C1-C1.d 47.5 8.6 14.6 23.5 29.5 -164.3 28.5 C0001 C0012 D4 1 36M C1-C1.doc 53.5 16 22 34.7 40.7 -161.2 24.6 C0001 C0012 A1 1 TV C1-C1.doc 2000 53.5 19.3 25.3 35.3 41.3 -148 28.5 C0013 C0018 D1 360 200 146k C4-C4.do 47.5 -5.5 -0.5 9.8 15.8 -162.1 24.6 C0013 C0018 D2 34 2100 1.56M C4-C4.d 47.5 4.8 10.8 20.1 26.1 -162.1 28.5 C0013 C0018 D3 8 7500 5.56M C4-C4.d 47.5 10.6 16.6 25.9 31.9 -161.8 28.5 C0013 C0018 D4 2 36000 36M C4-C4.doc 53.5 14.5 20.5 35.3 41.3 -160.5 24.6 C0013 C0018 A1 2 36000 TV C4-C4.doc 2000 53.5 18.8 24.8 35.5 41.5 -147.7 28.5 C0019 C0022 D1 180 200 146k C1-C2.do 47.5 -7.5 -1.5 6.8 12.8 -165.1 24.6 C0019 C0022 D2 17 2100 1.56M C1-C2.d 47.5 2.8 8.8 17.1 23.1 -165.1 28.5 C0019 C0022 D3 4 7500 5.56M C1-C2.d 47.5 8.6 14.6 22.9 28.9 -164.9 28.5 C0019 C0022 D4 1 36M C1-C2.doc 53.5 16 22 34.1 40.1 -161.8 24.6 C0019 C0022 A1 1 TV C1-C2.doc 2000 53.5 20.1 26.1 34.7 40.7 -150.7 28.5 C0027 C0030 D1 180 200 146k C2-C2.do 47.5 -4.5 1.5 6.8 12.8 -165.1 24.6 C0027 C0030 D2 17 2100 1.56M C2-C2.d 47.5 5.8 11.8 17.1 23.1 -165.1 28.5 C0027 C0030 D3 4 7500 5.56M C2-C2.d 47.5 11.6 17.6 22.9 28.9 -164.9 28.5 C0027 C0030 D4 1 36M C2-C2.doc 53.5 19 25 34.1 40.1 -164.9 24.6 C0027 C0030 A1 1 TV C2-C2.doc 2000 53.5 21.5 27.5 34.6 40.6 -148.7 28.5 C0035 C0038 D1 180 200 146k C3-C2.do 47.5 -4.5 1.5 6.8 12.8 -165.1 24.6 C0035 C0038 D2 17 2100 1.56M C3-C2.d 47.5 5.8 11.8 17.1 23.1 -165.1 28.5 C0035 C0038 D3 4 7500 5.56M C3-C2.d 47.5 11.6 17.6 22.9 28.9 -164.9 28.5 C0035 C0038 D4 1 36M C3-C2.doc 53.5 19 25 34.1 40.1 -161.8 24.6 C0035 C0038 A1 1 TV C3-C2.doc 2000 53.5 21.5 27.5 34.6 40.6 -148.7 28.5 K0001 K0016 D1 270 200 146k K1-K1.do 43.2 -6.3 -0.3 17.7 23.7 27.3 K0001 K0016 D2 25 2100 1.56M K1-K1.d 51.2 2.2 8.2 28.1 34.1 29.2 K0001 K0016 D3 7 7500 5.56M K1-K1.d 53 6.2 12.2 33.9 39.9 29.2 K0001 K0016 D4 1 36M K1-K1.doc 54.7 16.5 22.5 45.7 51.7 21.3

K0001 K0016 A1 1 TV K1-K1.doc 2000 54.7 21.3 27.3 45.7 51.7 28.7 K0017 K0018 D1 270 200 146k K2-K2.do 43.2 -6.3 -0.3 18 24 27.3 K0017 K0018 D2 25 2100 1.56M K2-K2.d 51.2 3.8 9.8 28.1 34.1 29.2 K0017 K0018 D3 7 7500 5.56M K2-K2.d 53 9.2 15.2 35.1 41.1 29.2 K0017 K0018 D4 1 36M K2-K2.doc 54.7 16.3 22.3 46.7 52.7 21.3 K0017 K0018 A1 1 TV K2-K2.doc 2000 54.7 20.3 26.3 46.1 52.1 28.7

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

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 1278 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1513 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2791 7 0.9 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 402 3.14 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 32.9 21 0.765 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): 2470 2454 2470 2454 Bus (Watts): (b): (g): (l): (q): 673 523 544 462 Total (Watts): (c): (h): (m): (r): 3143 2977 2998 2932 Solar Array (Watts): (d): (i): (n): (s): 4288 3954 3519 3256 Depth of Battery (e) (j) (o) (t) Discharge (%): 73.7 % % 73.7 % % 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: 2006-08-23 09:43:29
Document Modified: 2006-08-23 09:43:29
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