Exhibit

0597-EX-ST-2004 Text Documents

Intelsat LLC

2004-10-13ELS_67617

Intelsat LLC Experimental STA Request File No. 0597-EX-ST-2004 Page 1 EXHIBIT By this application, Intelsat LLC seeks special temporary authority (“STA”) for a 30-day period commencing November 1, 2004, to test a prototype interface for a satellite system. In support of this request, the following information is provided: Applicant: Intelsat LLC ATTN: Susan Crandall 3400 International Drive, N.W. Washington, DC 20008 Telephone: (202) 944-7848 Facsimile: (202) 944-7860 Intelsat Control Point of Contact: Michel B. Nakhla Intelsat LLC 22021 Comsat Drive Clarksburg, Maryland 20871 Telephone: (301) 944-7941 Cell: (202) 445-0987 Legal Contacts: Jennifer Hindin, Esq. Kurt E. DeSoto, Esq. Wiley Rein & Fielding LLP 1776 K Street, N.W. Washington, DC 20006 Telephone: (202) 719-7000 Fax: (202) 719-7049 jhindin@wrf.com kdesoto@wrf.com Purpose of STA: The experimental STA is requested to enable Intelsat to test a prototype interface between a satellite modem and an antenna. The antenna to be used — an AL 7104 System manufactured by Orbit CT&T Inc. — is described in the attached materials. The interface program will allow the antenna to track to a desired satellite upon a certain command from the modem based on geographic location coordinates. This feature on the modem can potentially be used for mobile applications. Dates of Operation: November 1 – December 1, 2004

Intelsat LLC Experimental STA Request File No. 0597-EX-ST-2004 Page 2 Place of Operation: Clarksburg Teleport, Intelsat Global Services Corporation 22021 Comsat Drive Clarksburg, Maryland 20871 North Latitude 39 deg 12 min 55.0 sec West Longitude 077 deg 16 min 30.0 sec Datum: NAD83 Number of Units: 1 fixed base transmit/receive earth station accessing satellites Intelsat 905 and 903 at 325.5 and 335.5 degrees East. Technical Specifications: Frequencies: 10950-11200 MHz (Receive) 11450-11700 MHz (Receive) 14000-14500 MHz (Transmit) Transmit Power Levels: Effective Isotropic Radiated Power (EIRP): 53.2 dBW - Maximum Transmitter Power Output (TPO): 6 Watts Effective Radiated Power (ERP): 96229.261 Watts – Peak Necessary Bandwidth: Not greater than 598 kHz Modulation: Digital QPSK Emission Designator: 598KG7W Other emission modes may be utilized, but in no event will the emissions extend beyond the frequency bands requested. All power levels will comply with the limits set forth in the FCC’s rules, including those relating to human exposure to radiation. See attached report. Antenna Information: The antennas will not extend more than 6 meters above the ground or, if mounted on an existing building, will not extend more than 6 meters above the building. If the antennas are mounted on an existing structure other than a building, they will be installed in accordance with FAA and FCC rules and regulations.

Intelsat LLC Experimental STA Request File No. 0597-EX-ST-2004 Page 3 Equipment To Be Used: The development and live-via-satellite testing of this feature will require the use of a transmit/receive antenna that will be installed at Intelsat’s teleport at Clarksburg, Maryland, and will have access to two of Intelsat’s satellites at orbital locations 325.5 and 335.5 degrees East. The testing and development will be done at Intelsat’s facilities and under Intelsat’s control. Restrictions on Operation: Intelsat recognizes that the operation of any equipment under experimental authority must not cause harmful interference to authorized facilities. It therefore will coordinate its activities with any licensees in the proposed bands in accordance with FCC requirements. Should interference occur, Intelsat will take immediate steps to resolve the interference, including if necessary arranging for the discontinuance of operation. Intelsat does not propose to market, sell, or lease any prototype equipment to end-users. After the experimentation ceases, Intelsat would recall and recover any device that are not in compliance with FCC regulations. If any different treatment becomes necessary during the course of its experimentation, Intelsat will seek separate and additional authority from the agency. In addition, Intelsat will advise entities testing the equipment that permission to operate has been granted under experimental authority issued to Intelsat, that such operation is strictly temporary, and that the equipment may not cause harmful interference. Intelsat proposes to label the equipment or associated written information as follows: FCC STATEMENT Permission to operate this device has been granted under experimental authority issued by the Federal Communications Commission to Intelsat LLC is strictly temporary and may be cancelled at any time. Operation is subject to the condition that it not cause harmful interference. This device is not, and may not be, offered for sale or sold until the approval of the FCC has been obtained. Thus, the user does not hold a property right in the device and may be required to return the device.

ORBIT COMMUNICATION LTD - Marine Division AL-7104-System Linear Ku-Band 1.2m Gregorian Offset Antenna Performance Antenna System Environmental Conditions Antenna Type Gregorian Offset Operating Temperature -25°C to 70°C Dish diameter 1.2m (48”) Storage Temperature -35°C to 75° C Random Size 2.35m (92.5”) Operating wind speed 100 Knots Freq. Operation Tx 14.0 to 14.5 GHz Rx 10.95 to 12.75 GHz Antenna Polarity Linear V/H Physical Antenna Gain Tx: 44.2dB @ 14.5GHz EMI/RFI MIL-STD-461 (Typical) Rx: 42.4dB @ 11.7GHz designed to meet System G/T (Typical) 19.6dB/K @ 20°EL Vibration CrossPol Isolation MIL-STD-167-1 35dB min designed to meet @ Tx Radome Loss Shock 0.6dB MIL-STD-901 (Typical) designed to meet 110/220 VAC, 50/60 Hz Elevation Travel ± 100° from zenith Power Requirements 800W (ADE), 200W (BDE) Azimuth Travel Continuous Weight (ADE) 355 Kg / 781 lb. Polarization Travel Continuous (including radome) Dynamic Accuracy 0.1° RMS Approvals Eutelsat Designed to meet FCC Designed to meet Ship Motion Gyro Compass Interface Roll ± 30° @ 8 sec NMEA 0183 RS422 or RS232 Pitch ± 15° @ 6 sec Step-by-Step Both Polarities Yaw ± 80° @ 50 sec Synchro 1:1; 1:36 Surge ± 0.2° g 1:60; 1:90 Sway ± 0.2° g 1:360 Heave ± 0.5° g Turning Rate 10°/sec Orbit CT&T Inc. (U.S.A) Orbit G.V. Ltd. (Europe – UK) Tel: (626) 961-6065 Tel: +44 (0) 23-8045-8478 Fax: (626) 961-6147 Fax:+44 (0) 23-8045-8902 info@orbitctt.com sales@orbitgv.com Note: for manuals click services on the home page

Radiation Hazard Report Page 1 of 4 Analysis of Non-Ionizing Radiation for a 1.2-Meter Earth Station System This report analyzes the non-ionizing radiation levels for a 1.2-meter earth station system. The analysis and calculations performed in this report comply with the methods described in the FCC Office of Engineering and Technology Bulletin, No. 65 first published in 1985 and revised in 1997 in Edition 97-01. The radiation safety limits used in the analysis are in conformance with the FCC R&O 96-326. Bulletin No. 65 and the FCC R&O specifies that there are two separate tiers of exposure limits that are dependant on the situation in which the exposure takes place and/or the status of the individuals who are subject to the exposure. The Maximum Permissible Exposure (MPE) limits for persons in a General Population/Uncontrolled environment are shown in Table 1. The General Population/Uncontrolled MPE is a function of transmit frequency and is for an exposure period of thirty minutes or less. The MPE limits for persons in an Occupational/Controlled environment are shown in Table 2. The Occupational MPE is a function of transmit frequency and is for an exposure period of six minutes or less. The purpose of the analysis described in this report is to determine the power flux density levels of the earth station in the far-field, near-field, transition region, between the subreflector or feed and main reflector surface, at the main reflector surface, and between the antenna edge and the ground and to compare these levels to the specified MPEs. Table 1. Limits for General Population/Uncontrolled Exposure (MPE) Frequency Range (MHz) Power Density (mW/cm2) 30-300 0.2 300-1500 Frequency (MHz)*(0.8/1200) 1500-100,000 1.0 Table 2. Limits for Occupational/Controlled Exposure (MPE) Frequency Range (MHz) Power Density (mW/cm2) 30-300 1.0 300-1500 Frequency (MHz)*(4.0/1200) 1500-100,000 5.0 Table 3. Formulas and Parameters Used for Determining Power Flux Densities Parameter Symbol Formula Value Units Antenna Diameter D Input 1.2 m Antenna Surface Area Asurface π D2 / 4 1.13 m2 Subreflector Diameter Dsr Input 22.5 cm Area of Subreflector Asr π Dsr 2/4 397.61 cm2 Frequency F Input 14250 MHz Wavelength λ 300 / F 0.021053 m Transmit Power P Input 6.00 W Antenna Gain (dBi) Ges Input 44.2 dBi Antenna Gain (factor) G 10Ges/10 26302.7 n/a Pi π Constant 3.1415927 n/a Antenna Efficiency η Gλ2/(π2D2) 0.82 n/a

Radiation Hazard Report Page 2 of 4 1. Far Field Distance Calculation The distance to the beginning of the far field can be determined from the following equation: Distance to the Far Field Region Rff = 0.60 D2 / λ (1) = 41.0 m The maximum main beam power density in the far field can be determined from the following equation: On-Axis Power Density in the Far Field Sff = G P / (4 π Rff 2) (2) = 7.456 W/m2 = 0.746 mW/cm2 2. Near Field Calculation Power flux density is considered to be at a maximum value throughout the entire length of the defined Near Field region. The region is contained within a cylindrical volume having the same diameter as the antenna. Past the boundary of the Near Field region, the power density from the antenna decreases linearly with respect to increasing distance. The distance to the end of the Near Field can be determined from the following equation: Extent of the Near Field Rnf = D2 / (4 λ) (3) = 17.1 m The maximum power density in the Near Field can be determined from the following equation: Near Field Power Density Snf = 16.0 η P / (π D2) (4) = 17.406 W/m2 = 1.741 mW/cm2 3. Transition Region Calculation The Transition region is located between the Near and Far Field regions. The power density begins to decrease linearly with increasing distance in the Transition region. While the power density decreases inversely with distance in the Transition region, the power density decreases inversely with the square of the distance in the Far Field region. The maximum power density in the Transition region will not exceed that calculated for the Near Field region. The power density calculated in Section 1 is the highest power density the antenna can produce in any of the regions away from the antenna. The power density at a distance Rt can be determined from the following equation: Transition Region Power Density St = Snf Rnf / Rt (5) = 1.741 mW/cm2

Radiation Hazard Report Page 3 of 4 4. Region between the Main Reflector and the Subreflector Transmissions from the feed assembly are directed toward the subreflector surface, and are reflected back toward the main reflector. The most common feed assemblies are waveguide flanges, horns or subreflectors. The energy between the subreflector and the reflector surfaces can be calculated by determining the power density at the subreflector surface. This can be determined from the following equation: Power Density at the Subreflector Ssr = 4000 P / Asr (6) = 60.361 mW/cm2 5. Main Reflector Region The power density in the main reflector is determined in the same manner as the power density at the subreflector. The area is now the area of the main reflector aperture and can be determined from the following equation: Power Density at the Main Reflector Surface Ssurface = 4 P / Asurface (7) = 21.221 W/m2 = 2.122 mW/cm2 6. Region between the Main Reflector and the Ground Assuming uniform illumination of the reflector surface, the power density between the antenna and the ground can be determined from the following equation: Power Density between Reflector and Ground Sg = P / Asurface (8) = 5.305 W/m2 = 0.531 mW/cm2 7. Summary of Calculations Table 4. Summary of Expected Radiation levels for Uncontrolled Environment Calculated Maximum Radiation Power Density Level Region (mW/cm2) Hazard Assessment 1. Far Field (Rff = 41.0 m) Sff 0.746 Satisfies FCC MPE 2. Near Field (Rnf = 17.1 m) Snf 1.741 Potential Hazard 3. Transition Region (Rnf < Rt < Rff) St 1.741 Potential Hazard 4. Between Main Reflector and Ssr 60.361 Potential Hazard Subreflector 5. Main Reflector Ssurface 2.122 Potential Hazard 6. Between Main Reflector and Ground Sg 0.531 Satisfies FCC MPE

Radiation Hazard Report Page 4 of 4 Table 5. Summary of Expected Radiation levels for Controlled Environment Calculated Maximum Radiation Power Density Region Level (mW/cm2) Hazard Assessment 1. Far Field (Rff = 41.0 m) Sff 0.746 Satisfies FCC MPE 2. Near Field (Rnf = 17.1 m) Snf 1.741 Satisfies FCC MPE 3. Transition Region (Rnf < Rt < Rff) St 1.741 Satisfies FCC MPE 4. Between Main Reflector and Ssr 60.361 Potential Hazard Subreflector 5. Main Reflector Ssurface 2.122 Satisfies FCC MPE 6. Between Main Reflector and Ground Sg 0.531 Satisfies FCC MPE It is the applicant's responsibility to ensure that the public and operational personnel are not exposed to harmful levels of radiation. 8. Conclusions Based on the above analysis it is concluded that the FCC MPE guidelines have been exceeded (or met) in the regions of Table 4 and 5. The applicant proposes to comply with the MPE limits by one or more of the following methods. Means of Compliance Uncontrolled Areas This antenna will be located in a fenced area. The fenced are will be sufficient to prohibit the general public from having access the areas that exceed the MPE limits Since one diameter removed from the main beam of the antenna or ½ diameter removed from the edge of the antenna the RF levels are reduced by a factor of 100 or 20 dB. None of the areas exceeding the MPE levels will be accessible by the general public. Radiation hazard signs will be posted while this earth station is in operation. The applicant will ensure that no buildings or other obstacles will be in the areas that exceed the MPE levels. Means of Compliance Controlled Areas The earth station’s operational personnel will not have access to the areas that exceed the MPE levels while the earth station is in operation. The transmitters will be turned off during antenna maintenance. WRFMAIN 12256168.2


Document Created: 2004-10-13 09:41:13
Document Modified: 2004-10-13 09:41:13
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