Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20080523-00112 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2008052300112_643925

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: ECHOSTAR-85W N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 24 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: 864 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 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: 84.9 W The nominal 85° W.L. location was selected because Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be the C-band frequencies at the slot recently became N/S Station-Keeping provided (Optional): available for re-assignment. The 84.9° W.L. locati on d. Toward West: Degrees E/W 0.05 Degrees Tolerance: was selected in order to to avoid an overlap of the g. Westernmost: e. Toward East: 0.05 Degrees station-keeping volume of other satellites that operate 0.05 Degrees h. Easternmost: nominally at 85° W.L. 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 CONUS + portions of Canada and Mexico SA2 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) RXH R 32.1 26.1 0.12 0.1 30 Y 0 SA1 615 4.2 -102 20 1 RXV R 32.1 26.1 0.12 0.1 30 Y 90 SA1 615 4.2 -102 20 1 TXH T 30.7 24.7 0.12 0.1 30 Y 0 SA1 2.2 15.1 42.5 TXV T 30.7 24.7 0.12 0.1 30 Y 90 SA1 2.2 15.1 42.5 OMN R 4 -2 0.12 0.1 30 Y 0 SA2 9250 -35.7 OMN R 4 -2 0.12 0.1 30 Y 90 SA2 9250 -35.7 OMN T 4 -2 0.12 0.1 30 Y 0 SA2 4.3 5 11 OMN T 4 -2 0.12 0.1 30 Y 90 SA2 4.3 5 11

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) RXH R C -84.9 RXH.gxt RXV R C -84.9 RXV.gxt TXH T C -84.9 TXH.gxt -165.1 -164.4 -163.5 -162.5 -161.4 TXV T C -84.9 TXV.gxt -165.1 -164.4 -163.5 -162.5 -161.4 OMN T C -84.9 -169 -169 -169 -169 -169 OMN T C -84.9 -169 -169 -169 -169 -169

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) U0001 36000 R 5945 V C T0001 119 U0001 RXV D0001 TXH U0003 36000 R 5985 V C T0003 119 U0003 RXV D0003 TXH U0005 36000 R 6025 V C T0005 119 U0005 RXV D0005 TXH U0007 36000 R 6065 V C T0007 119 U0007 RXV D0007 TXH U0009 36000 R 6105 V C T0009 119 U0009 RXV D0009 TXH U0011 36000 R 6145 V C T0011 119 U0011 RXV D0011 TXH U0013 36000 R 6185 V C T0013 119 U0013 RXV D0013 TXH U0015 36000 R 6225 V C T0015 119 U0015 RXV D0015 TXH U0017 36000 R 6265 V C T0017 119 U0017 RXV D0017 TXH U0019 36000 R 6305 V C T0019 119 U0019 RXV D0019 TXH U0021 36000 R 6345 V C T0021 119 U0021 RXV D0021 TXH U0023 36000 R 6385 V C T0023 119 U0023 RXV D0023 TXH U0002 36000 R 5965 H C T0002 119 U0002 RXH D0002 TXV U0004 36000 R 6005 H C T0004 119 U0004 RXH D0004 TXV U0006 36000 R 6045 H C T0006 119 U0006 RXH D0006 TXV U0008 36000 R 6085 H C T0008 119 U0008 RXH D0008 TXV U0010 36000 R 6125 H C T0010 119 U0010 RXH D0010 TXV U0012 36000 R 6165 H C T0012 119 U0012 RXH D0012 TXV U0014 36000 R 6205 H C T0014 119 U0014 RXH D0014 TXV U0016 36000 R 6245 H C T0016 119 U0016 RXH D0016 TXV U0018 36000 R 6285 H C T0018 119 U0018 RXH D0018 TXV U0020 36000 R 6325 H C T0020 119 U0020 RXH D0020 TXV U0022 36000 R 6365 H C T0022 119 U0022 RXH D0022 TXV U0024 36000 R 6405 H C T0024 119 U0024 RXH D0024 TXV D0001 36000 T 3720 H C TC1 CMD1 RXH D0003 36000 T 3760 H C TC2 CMD2 RXV D0005 36000 T 3800 H C TC3 CMD1 OMNRH D0007 36000 T 3840 H C TC4 CMD2 OMNRV D0009 36000 T 3880 H C TM1 TLM1 TXV D0011 36000 T 3920 H C TM2 TLM2 TXH

D0013 36000 T 3960 H C TM3 TLM1 OMNTV D0015 36000 T 4000 H C TM4 TLM2 OMNTH D0017 36000 T 4040 H C D0019 36000 T 4080 H C D0021 36000 T 4120 H C D0023 36000 T 4160 H C D0002 36000 T 3740 V C D0004 36000 T 3780 V C D0006 36000 T 3820 V C D0008 36000 T 3860 V C D0010 36000 T 3900 V C D0012 36000 T 3940 V C D0014 36000 T 3980 V C D0016 36000 T 4020 V C D0018 36000 T 4060 V C D0020 36000 T 4100 V C D0022 36000 T 4140 V C D0024 36000 T 4180 V C CMD1 1000 R 5926 H T CMD2 1000 R 6424 V T TLM1 300 T 3701 V T TLM2 300 T 4199 H 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 445KG7W 445 4 512 0.691 5.7 17.9 D2 1M78G7W 1778 4 2048 0.691 5.7 17.9 D3 6M33G7W 6330 4 8448 0.801 5.8 18 D4 36M0G7W 36000 8 58200 0.641 7.5 19.7 D5 36M0G7W 36000 4 50400 0.841 6.5 18.7

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) A1 1M00F2D 1000 1 10 22.2 A2 300KG2D 300 1 9 21.2

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) T0001 T0024 D1 72 500 LB1.doc 47.5 -0.6 5.4 14.5 20.5 -162.4 22.4 T0001 T0024 D2 18 2000 LB2.doc 51.3 0 6 19.2 25.2 -163.8 23.5 T0001 T0024 D3 5 7200 LB3.doc 47.5 6.7 12.7 22.2 28.2 -166.3 26.7 T0001 T0024 D4 1 LB4.doc 53.5 19.5 25.5 36.5 42.5 -159.5 22.4 T0001 T0024 D5 1 LB5.doc 53.5 19.5 25.5 36.5 42.5 -159.5 22.4 TC1 TC2 A1 1 CMD Refl.doc 53.5 -8.6 -2.6 TC3 TC4 A1 1 CMD Omni.doc 53.5 20.9 26.9 TM1 TM2 A2 1 TLM Refl.doc 11 17 -163.2 26.2 TM3 TM4 A2 1 TLM Omni.doc 5 11 -169 33.3

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: 530 Echostar Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Cheyenne Laramie WY 82007 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 307-633-5460 Remote Control (TT C) Location(s): S14a: Street Address: 801 North Dish Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Gilbert Maricopa AZ 85223 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 480-558-2778

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 920 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1160 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2080 14.7 0.87 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 365 1.8 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 24 3.8 0.74 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): 1510 1510 1510 1510 Bus (Watts): (b): (g): (l): (q): 930 580 930 580 Total (Watts): (c): (h): (m): (r): 2440 2090 2440 2090 Solar Array (Watts): (d): (i): (n): (s): 3600 3045 2800 2490 Depth of Battery (e) (j) (o) (t) Discharge (%): 75 % 75 % 75 % 75 % 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: 2008-05-28 11:51:03
Document Modified: 2008-05-28 11:51:03
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC