Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20080509-00101 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2008050900101_641012

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: NEW DAWN 6/30/2011 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 9/30/2008 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 11/30/2010 39 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: 1/1/2011 3/31/2011 1872 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) 5850 M 6550 M R Fixed Satellite Service 3625 M 4200 M T Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 10950 M 11200 M T Fixed Satellite Service 11450 M 11700 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: 32.8 E Replace Galaxy 11 and complement/augument Intelsat Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be 802 services N/S Station-Keeping provided (Optional): 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) 1 S Africa, Europe, Middle East 2 S Southern Africa 3 S Global

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) CHU R 28.2 18.2 0.15 0.15 30 N 1 540 0.9 -97 21 1 CVU R 28.2 18.2 0.15 0.15 30 N 1 540 0.9 -97 21 1 CHD T 27.5 21.5 0.15 0.15 30 N 1 2.4 34.7 42.9 CVD T 27.5 21.5 0.15 0.15 30 N 1 2.4 34.7 42.9 KHU R 31.5 25.5 0.15 0.15 30 N 02 504 4.5 -99 21 1 KVU R 31.5 25.5 0.15 0.15 30 N 90 2 504 4.5 -99 21 1 KHD T 31 25 0.15 0.15 30 N 02 2.1 93.3 50.7 KVD T 31 25 0.15 0.15 30 N 90 2 2.1 93.3 50.7 CMD R 22 18 0.15 0.15 N 3 10290 -18.1 -107.2 CMD R 5.1 1.1 0.15 0.15 N 3 3254 -30 -95.3 CMD R -2.3 -6.3 0.15 0.15 N 3 2150 -35.6 -89.7 TLM T 20.4 16.4 0.15 0.15 N 3 2.3 0.07 9.1 TLM T 5.8 1.8 0.15 0.15 N 3 4.1 4.3 12.1 TLM T -0.4 -4.4 0.15 0.15 N 3 1.6 7.6 8.4 UPC T 20.4 17.8 0.15 0.15 N 3 2 0.32 15.4 UPK T 20.4 17.8 0.15 0.15 N 3 2 0.63 18.4 UPKL T 20.4 17.8 0.15 0.15 N 3 2 0.63 18.4

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) CHU R C 32.8 CHUP.gxt CVU R C 32.8 CVUP.gxt CHD T C 32.8 CHDN.gxt -152 -150.3 -150.1 -150 -149.9 CVD T C 32.8 CVDN.gxt -152 -150.3 -150.1 -150 -149.9 KHU R C 32.8 KHUP.gxt KVU R C 32.8 KVUP.gxt KHD T C 32.8 KHDN.gxt -150 -147.5 -145 -142.5 -142.1 KVD T C 32.8 KVDN.gxt -150 -147.5 -145 -142.5 -142.1 CMD R C 32.8 CMDG.gxt CMD R C 32.8 CMDW.pdf CMD R C 32.8 CMDO.pdf TLM T C 32.8 TLMG.gxt -172.9 -172.8 -172.7 -172.6 -172.5 TLM T C 32.8 TLMW.pdf -169.9 -169.8 -169.7 -169.6 -169.5 TLM T C 32.8 TLMO.pdf -173.6 -173.5 -173.4 -173.3 -173.2 UPC T C 32.8 UPCR.gxt -155.8 -155.7 -155.6 -155.5 -155.4 UPK T C 32.8 UPKR.gxt -152.8 -152.7 -152.6 -152.5 -152.4 UPKL T C 32.8 UPKL.gxt -152.8 -152.7 -152.6 -152.5 -152.4

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) UC1 72000 R 5890 L C CC001 121.4 UC1 CHUP DC1 CVDN UC3 36000 R 5950 L C CC003 121.4 UC3 CHUP DC3 CVDN UC5 36000 R 5990 L C CC005 121.4 UC5 CHUP DC5 CVDN UC7 72000 R 6050 L C CC007 121.4 UC7 CHUP DC7 CVDN UC9 72000 R 6130 L C CC009 121.4 UC9 CHUP DC9 CVDN UC11 72000 R 6220 L C CC011 121.4 UC11 CHUP DC11 CVDN UC13 72000 R 6300 L C CC013 121.4 UC13 CHUP DC13 CVDN UC15 72000 R 6380 L C CC015 121.4 UC15 CHUP DC15 CVDN UC17 36000 R 6450 L C CC002 121.4 UC2 CVUP DC2 CHDN UC19 36000 R 6490 L C CC004 121.4 UC4 CVUP DC4 CHDN UC21 36000 R 6530 L C CC006 121.4 UC6 CVUP DC6 CHDN UC2 72000 R 5890 R C CC008 121.4 UC8 CVUP DC8 CHDN UC4 72000 R 5970 R C CC010 121.4 UC10 CVUP DC10 CHDN UC6 72000 R 6050 R C CC012 121.4 UC12 CVUP DC12 CHDN UC8 72000 R 6130 R C CC014 121.4 UC14 CVUP DC14 CHDN UC10 72000 R 6220 R C KK001 131.7 UK001 KHUP DK001 KVDN UC12 72000 R 6300 R C KK003 131.7 UK003 KHUP DK003 KVDN UC14 72000 R 6380 R C KK005 131.7 UK005 KHUP DK005 KVDN UC16 36000 R 6450 R C KK007 131.7 UK007 KHUP DK007 KVDN UC18 36000 R 6490 R C KK009 131.7 UK009 KHUP DK009 KVDN UC20 36000 R 6530 R C KK011 131.7 UK011 KHUP DK011 KVDN DC1 72000 T 3665 R C KK013 131.7 UK013 KHUP DK013 KVDN DC3 36000 T 3725 R C KK015 131.7 UK015 KHUP DK015 KVDN DC5 36000 T 3765 R C KK017 131.7 UK017 KHUP DK017 KVDN DC7 72000 T 3825 R C KK019 131.7 UK019 KHUP DK019 KVDN DC9 72000 T 3905 R C KK021 131.7 UK021 KHUP DK021 KVDN DC11 72000 T 3995 R C KK023 131.7 UK023 KHUP DK023 KVDN DC13 72000 T 4075 R C KK002 131.7 UK002 KVUP DK002 KHDN DC15 72000 T 4155 R C KK004 131.7 UK004 KVUP DK004 KHDN DC2 72000 T 3665 L C KK006 131.7 UK006 KVUP DK006 KHDN

DC4 72000 T 3745 L C KK008 131.7 UK008 KVUP DK008 KHDN DC6 72000 T 3825 L C KK010 131.7 UK010 KVUP DK010 KHDN DC8 72000 T 3905 L C KK012 131.7 UK012 KVUP DK012 KHDN DC10 72000 T 3995 L C KK014 131.7 UK014 KVUP DK014 KHDN DC12 72000 T 4075 L C KK016 131.7 UK016 KVUP DK016 KHDN DC14 72000 T 4155 L C KK018 131.7 UK018 KVUP DK018 KHDN UK001 36000 R 14025 H C KK020 131.7 UK020 KVUP DK020 KHDN UK003 36000 R 14065 H C KK022 131.7 UK022 KVUP DK022 KHDN UK005 36000 R 14105 H C KK024 131.7 UK024 KVUP DK024 KHDN UK007 36000 R 14145 H C CK002 125.5 UC3 CHUP DK002 KHDN UK009 36000 R 14185 H C CK004 125.5 UC5 CHUP DK004 KHDN UK011 36000 R 14225 H C CK017 126.2 UC17 CHUP DK014 KHDN UK013 36000 R 14275 H C CK019 126.2 UC19 CHUP DK016 KHDN UK015 36000 R 14315 H C CK021 126.2 UC21 CHUP DK018 KHDN UK017 36000 R 14355 H C CK016 126.2 UC16 CVUP DK020 KHDN UK019 36000 R 14395 H C CK018 126.2 UC18 CVUP DK022 KHDN UK021 36000 R 14435 H C CK020 126.2 UC20 CVUP DK024 KHDN UK023 36000 R 14475 H C KC003 127.3 UK002 KVUP DC3 CVDN UK002 36000 R 14025 V C KC005 127.3 UK004 KVUP DC5 CVDN UK004 36000 R 14065 V C UK006 36000 R 14105 V C UK008 36000 R 14145 V C UK010 36000 R 14185 V C UK012 36000 R 14225 V C UK014 36000 R 14275 V C UK016 36000 R 14315 V C UK018 36000 R 14355 V C UK020 36000 R 14395 V C UK022 36000 R 14435 V C UK024 36000 R 14475 V C DK001 36000 T 10975 V C DK003 36000 T 11015 V C DK005 36000 T 11055 V C DK007 36000 T 11095 V C DK009 36000 T 11135 V C DK011 36000 T 11175 V C DK013 36000 T 11475 V C DK015 36000 T 11515 V C DK017 36000 T 11555 V C

DK019 36000 T 11595 V C DK021 36000 T 11635 V C DK023 36000 T 11675 V C DK002 36000 T 10975 H C DK004 36000 T 11015 H C DK006 36000 T 11055 H C DK008 36000 T 11095 H C DK010 36000 T 11135 H C DK012 36000 T 11175 H C DK014 36000 T 11475 H C DK016 36000 T 11515 H C DK018 36000 T 11555 H C DK020 36000 T 11595 H C DK022 36000 T 11635 H C DK024 36000 T 11675 H C CMD1 1000 R 6170 R T CMD2 1000 R 6175 L T CMD3 1000 R 6175 R T TLM1 500 T 3944 R T TLM2 500 T 3945 R T TLM3 500 T 3944 L T TLM4 500 T 3945 L T TLM5 500 T 3944 R T TLM6 500 T 3945 R T UPC1 25 T 3626 R T UPC2 25 T 11196 R T UPC3 25 T 11699 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) 1 72M0G7W 60266 4 73726 0.75 6.1 11.5 2 36M0G7W 30133 4 36863 0.75 6.1 20.5 3 10M3G7W 6771.1 4 6000 0.5 3.9 17.7 4 100KG7W 75.4 4 64 0.5 3 17.3 5 1M45G7W 1229 2 512 0.5 3.4 14.6 6 400KG7W 307 2 128 0.5 3.4 14.7

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) 1 36M0F3F 36000 TV/FM 1 PAL 15.6 1.5 10 22

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) KK001 KK024 1 1 NEW DAWN LI 4000 58.1 17.8 23.8 44.7 50.7 -141.4 24.5 KK001 KK024 2 1 NEW DAWN S 58.1 17.8 23.8 41.5 47.5 -153.4 24.5 KK001 KK024 3 3 10300 NEW DAWN S 58.1 -2.5 3.5 36 42 -152.4 21.8 KK001 KK024 4 337 100 NEW DAWN S 58.1 -20 -16.7 15.9 21.9 -153 21.8 KK001 KK024 5 21 1450 NEW DAWN S 58.1 -10.7 -4.7 27.9 33.9 -153.1 21.8 KK001 KK024 6 90 400 NEW DAWN S 46.4 -8.5 -2.5 18.4 24.4 -156.6 34.1 CK002 CK021 1 1 NEW DAWN S 4000 58.4 15.5 25.5 37.6 43.6 -148.5 32.6 CK002 CK021 2 1 NEW DAWN S 58.4 15.5 25.5 37.6 43.6 -157.3 26.2 CK002 CK021 3 3 10300 NEW DAWN S 51 11.8 21.8 36.3 42.3 -152.1 18.3 CK002 CK021 4 330 100 NEW DAWN S 51 -8.5 1.5 16 22 -152.9 18.3 KC003 KC005 1 1 NEW DAWN S 4000 58 17.9 23.9 36.9 42.9 -149.2 23.2 KC003 KC005 2 1 NEW DAWN S 58 17.9 23.9 36.9 42.9 -158 20.5 KC003 KC005 3 2 10300 NEW DAWN S 58 2.4 8.4 29.7 35.7 -158.7 18.7 KC003 KC005 4 235 100 NEW DAWN S 58 -17.6 -11.6 9.7 15.7 -159.2 18.7 CC003 CC005 1 1 NEW DAWN S 4000 52.5 19.4 25.4 36.9 42.9 -149.2 25.8 CC003 CC005 2 1 NEW DAWN S 50.7 17.2 23.2 36.9 42.9 -158 20.5 CC003 CC005 3 2 10300 NEW DAWN S 50.7 10 16 29.4 35.4 -159 18.7 CC003 CC005 4 274 100 NEW DAWN S 50.7 -10.4 4.4 9 15 -159.9 18.7 CC001 CC015 1 2 36000 NEW DAWN S 4000 51 19.9 25.9 32.7 38.7 -153.4 29.4 CC001 CC015 1 1 NEW DAWN S 51 17.9 23.9 36.9 42.9 -161 23.6 CC001 CC015 3 5 10300 NEW DAWN S 51 11.5 17.5 26.2 32.2 -162.2 19.2 CC001 CC015 4 573 100 NEW DAWN S 51 -8.9 -2.9 5.8 11.8 -163.1 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): Yes Remote Control (TT C) Location(s): S14a: Street Address: 3400 International Drive, N.W. S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Washington, D.C. DC 20008 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 202-944-7701

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 2248 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3140 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5388 22.5 0.95 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 810 5.2 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 74.5 7.5 0.8 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): 7950 7950 7950 7950 Bus (Watts): (b): (g): (l): (q): 930 890 930 890 Total (Watts): (c): (h): (m): (r): 8880 8840 8880 8840 Solar Array (Watts): (d): (i): (n): (s): 11960 10560 11390 10060 Depth of Battery (e) (j) (o) (t) Discharge (%): 52.1 % % 69.6 % % 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: 2008-05-13 10:55:18
Document Modified: 2008-05-13 10:55:18
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