Attachment Amendment

Amendment

AMENDMENT submitted by Denali Telecom LLC

Conforming Amendment

2002-09-16

This document pretains to SAT-AMD-20020916-00195 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2002091600195_287497

DOCKET iLE copy ORIG INAL Law OrFices PIERSON & BURNETT, LLP 517 S. Washington Street, Alexandria, VA 22314 Tel: 703 683 3044 Fax: 703 683 2044 September 16, 2002 Via Hand Delivery RECEIVED Mr. William F. Caton Deputy Secretary SEP 1 6 2002 Federal Communications Commission FEDERAL COMMUNICATIONS COMMISSION gi?t:{lals;achusetts Avenue, NE mt)mcs F THE SECRETARY Washington, DC 20002 Attn: International Bureau — Satellite Division 02—123) Ladies and Gentlemen: Enclosed on behalf of Denali Telecom, LLC is the Conforming Amendment to the above—referenced application filed in response to the amended rules as proposed in The Establishment ofPolicies and Service Rulesfor the Non—Geostationary Satellite Orbit, Fixed Satellite Service in the Ku—Band (IB Docket No. 01—96; FCC 02—123; Adopted April 18, 2002; Released April 26, 2002). Accompanying this amendment is an FCC Form 312. In accordance with the Commission‘s rule 47 CFR §1.1114(a), no fee is required for this application, as it is filed for the sole purpose of modifying a pending application for authorization in order to comply with new or additional requirements imposed by the Commission. Should any questions arise with regard to this filing, kindly communicate with the undersigned. Yours very truly, Attorneys for Denali Telecom Enclosures Original + nine copies

Before the FEDERAL COMMUNICATIONS COMMISSION Washington, D.C. 20554 In the Matter of The Establishment of Policies and Service Rules for the Non—Geostationary FiE Nos. IB Docket No. 01—96; Satellite Orbit, Fixed Satellite Service in the Ku—Band And DenaL TELECOM, LLC Conforming Amendment to Application and, 160—SAT—P/LA—97(13) For Authority to Launch and Operate the Pentriad Satellite System To: Chief, Satellite Policy Branch CONFORMING AMENDMENT Denali Telecom, LLC ("Denali"), by its attorneys and pursuant to the Commission‘s adoption of new service rules in its Report and Order, IB Docket No. 01—96, released April 26, 2002, hereby submits its conforming amendment in the above—captioned application proceeding as called for by the Commission. ‘ On September 26, 1997, Denali filed an application for authority ‘ "Policies and Service Rules for the Non—Geostationary Satellite Orbit, Fixed Satellite Service in the Ku—Band," 67 Fed Reg. 55,508 (Aug. 16, 2002) (to be codified at 47 C.F.R. Part 25), per In the Matter of The Establishment ofPolicies and Service Rulesfor the Non—Geostationary Satellite Orbit, Fixed Satellite Service in the Ku—Band, TB Docket No. 01—96, Adopted April 18, 2002, Released April 26, 2002; ECC 02—123.

to construct and operate the Pentriad satellite system.2 The Pentriad satellite system proposed by Denali will operate in quasi—geostationary highly elliptical orbits ("HEO"), and utilize the Ku—band for space—to—Earth transmission." The Commission has proposed to amend Section 25.146 Licensing and operating authorization provisions for the non—geostationary satellite orbit fixed—satellite service (NGSO FSS) in the bands 10.7 GHz to 14.5 GHz, and has requested the applicants to this licensing proceeding to submit conforming amendments to their respective applications. Denali, as an applicant affected by the proposed rule changes, provides the following additional information to satisfy the proposed amended regulation: \ (1) A demonstration that the proposed system is capable ofprovidingfixed—satellite services on a continuous basis throughout thefifty states, Puerto Rico, and the U.S. Virgin Islands, U.S.; and (2) A demonstration that the proposed system be capable ofprovidingfixed—satellite services to all locations asfar north as 70 deg. latitude and asfar south as 55 deg. latitudefor at least 75 percent ofevery 24—hour period. In order to comply with the Commission‘s requirement to provide for global coverage of services in the Ku—band, Denali amends its current application with the addition ofthe Southern * See, In re Application ofDenali Telecom LLC, Consolidated System Proposalfor Authority to Launch and Operate Thirteen Satellites in the Pentriad System, an International Joint Venture Constellation of Thirteen Satellites Operating in Linked Molniya Highly—Elliptical Orbits in the International Fixed—Satellite Service and the Mobile Satellite Service (filed September 26, 1997), FCC File No. 160—SAT—P/LA—97(13). * Denali‘s application requests authority to construct and operate satellites in the international Pentriad system. The satellites will operate in linked Molniya highly elliptical orbits, and will provide international Fixed—Satellite services in the Ku—band (11.7—12.7 GHz) to users in the Northern and Southern Hemispheres. The Pentriad system will be the first commercial Western use oflinked Molniya highly elliptical orbits.

Operation Configuration ("SOC") —— covering the Earth‘s Southern Hemisphere. The SOC will service areas at 30 deg. west longitude (over the southern Atlantic Ocean) and 150 deg. east longitude (over Australia), and thus will be able to provide greater service capacity —— greater than what would have been available from its initial constellation design contained in the Denali application —— available to all Southern Hemisphere continents, including Antarctica. (See Exhibits 1 and 2 to the FCC Form 312 for Southern Hemisphere Service Area coverage). This Pentriad system design continues to allow for the implementation of multiple systems in other Molniya orbits by maintaining spatial diversity between the operational ares of the satellites (geosynchronous satellites at zero degrees Latitude plus or minus five degrees North and South and the Pentriad HEO satellites operating between 55 degrees South Latitude and 70 degrees North Latitude). Thus there is maintained an effective separation between GEO satellites and tie operational are ofthe Denali HEO satellites. Services will be initiated in three phases: (1) an Initial Operation Configuration ("IOC:") in the Northern Hemisphere; (2) a Full Operation Configuration ("FOC") in the Northern Hemisphere; and (3) a Southern Operation Configuration ("SOC") in the Southern Hemisphere. Denali is ready to proceed with the construction of the Pentriad system, so that the first three Pentriad spacecraft can be launched into an IOC to meet milestone dates (as to be specified by the Commission‘s authorization) to provide broadband services to North America and North Asia, and for subsequent deployment of the remainder ofthe constellation to follow for services to the Southern Hemisphere. In the Southern Hemisphere, three satellites (Flight Models 13 to 15) will be launched into three distinct Molniya orbits (63 degree inclination) with 12.0 hour orbital periods. These satellites will be used to provide service to South America, Africa and Australia. The Southern Hemisphere coverage will be deployed after the IOC ofthe Northern Hemisphere. The FOC of the Northern Hemisphere will follow the Southern Hemisphere deployment. In the FOC, all operational Pentriad satellites (Flight Models 1 through 15) will operate in six orbital planes. The three Northern and Southern orbital planes will be separated by one hundred twenty degrees (120°) around the equator ofthe Earth. The three operational satellites in each orbital plane will be spaced evenly in their respective plane. Operating together, the nine

operational satellites will provide continuous twenty—four (24) hour broadband coverage to five overlapping service areas in the Northern Hemisphere, while the three Southern Hemisphere satellites will provide services to the southern areas for at least 75 percent of every 24—hour period. In—orbit spares (Flight Models 16—20) also will be launched into Molniya orbits with periods ofapproximately 9.6 hours. One satellite will orbit in each ofthe five orbital planes utilized by the operational satellites. Ifthere is a failure of an operational satellite, the spare orbiting in the same plane will perform an orbital maneuver to change the orbital period to 14.4 hours and to maneuver into the same orbital phase as the failed satellite, to reconstitute full service by the system. In the worst case scenario, the replacement satellite will require 28.8 hours to regjace a failed satellite and an additional 14.4 hour orbital period will be required to stabilize the orbit of the newly—operational spare. The total satellite outage during a worst case will be 43.2 hours, with single service outages of only eight hours in three separate service areas. (3) Sufficient information on the NGSO FSS system characteristics to properly model the system in computer sharing simulations, including, at a minimum, NGSO hand—over and satellite switchingfitrategies, NGSO satellite beam patterns, NGSO satellite antenna patterns and NGSO earth station antenna patterns. In particular, each NGSO FSS applicant must explain the switchingprotocols it used to avoid transmitting while passing through the geostationary satellite orbit arc, or provide an explanation as to how the power—flux density limits in Section 25.208 are met without using geostationary satellite orbit are avoidance. In addition, each NGSO FSS applicant mustprovide the orbitalparameters contained in Section A.3 ofAnnex 1 to Resolution 46. Further, each NGSO FSS applicant mustprovide a sufficient technical showing to demonstrate that the proposed non—geostationary satellite orbit system meets the power—flux density limits contained in Section 25.208, as applicable. Denali‘s original application contained the information requested of this proposed addition to the Commission‘s rules.* The Pentriad system does not require, and Denali does not request, * See sections 3.3 and 4.2 of Denali‘s application, supra note 2. 4

an exclusive allocation of frequency spectrum in the Ku—band. The Pentriad system employs a novel system design that allows for multiple uses of the frequency spectrum. Because of the operational service arc of the satellites, Pentriad can operate, without interference, with satellites in the geostationary/ geosynchronous orbit using the same frequencies in both the Northern and Southern hemispheres coverage areas. The Northern and Southern Hemisphere Orbital Parameters (Exhibit 3) and the Link Budget (Exhibit 4) are appended to the FCC Form 312. Antenna Patterns for the Pentriad System data service are depicted for IOC (Exhibit 5) and FOC & SOC (Exhibit 6), with center position of Washington, D.C., and also appended to the FCC Form 312. (4) A description ofthe design and operational strategies that it will use, ifany, to mitigate orbital debris. Each applicant must submit a casualty risk assessmentifplannedpost— mission disposal involves atmospheric re—entry ofthe spacecraft. The Pentriad System is designed to meet the requirements outlined in the USG Space Debris Mitigation Requirements. The communications payloads ofthe Pentriad design do not involve thé planned release ofany operational debris following the launch phase of operations. Denali also confirms that spacecraft shielding, placement of components, and use of redundant systems has been assessed to limit the probability that an operating spacecraft in the Pentriad system will become a source ofdebris through collisions with man—made objects or meteors. Denali further has assessed and will limit the probability ofaccidental explosion during and after completion of mission operations. The assessment was based on possible failure modes that could result in explosions, and operational procedures will be adopted to limit the probability they will occur. In addition, all sources of stored energy onboard the Pentriad spacecraft will have been depleted or contained in a "safed" mode when no longer required for mission operations or post— mission disposal. Denali has estimated that its Pentriad system design and spacecraft mission profiles will limit the probability of collision with known large objects during the constellation‘s orbital

lifetime. Denali‘s disclosure ofthe parameters (including the number of space stations, the number and inclination of orbital planes, orbital period, apogee, perigee the argument ofperigee, and right ascension ofthe ascending nodes) used by the Pentriad system may assist third parties in identifying potential problems that may be the result of proposed operations, and lends itselfto coordination between Denali and other operators located in similar orbits. Denali will be prepared to disclose the accuracy with which these orbital parameters will be maintained. As a result ofthe perigee ofthe Northern hemisphere Pentriad satellites being over the vast Southern hemisphere oceans, atmospheric reentry is favored for spacecraft disposal at the end of mission life. For the Southern hemisphere satellites, the perigee will be over the northern hemisphere. For these Southern hemisphere satellites, Denali will perform a maneuver out ofthe Mo]n\iya plane that will cause the perigee to precess into the Southern hemisphere, at which time the s;acecrafi will deorbit and enter the atmosphere into the southern oceans. The spacecraft will be designed to eliminate and minimize debris released during normal operations by including sufficient fuel onboard each spacecraft to perform a deorbit burn, thereby hastening reentry and being presented with a risk ofhuman casualty less than 1 in 10,000. Such calculation is predicated on results from the NASA Safety Standard guidance for computing casualty risk." Respectfully submitted, co C A © — By T y Dennis J. Burnett, President David L. Lihani Pentriad North America, Inc. B. Elsa Woodall Manager of Denali Telecom, LLC Pierson & Burnett, L.L.P. 1667 K Street, N.W., Suite 801 517 S. Washington Street Washington, D.C. 20006 Alexandria, VA 22314 (202) 466—3044 (703) 683—3044 Attorneys for Denali Telecom, LLC * "Guidelines and Assessment Procedures for Limiting Orbital Debris," NASA Safety Standard, NSS 1740.14, August 1995, [updated as NASA—STD—8719.14].

Certification that Conforming Amendment to the Application is True, Complete and Correct Denali acknowledges thatall of the statements in this Conforming Amendment to its Application and in the exhibits and associated attachments are considered material representations, and thatall the exhibits and attachments are a material part hereof, and are incorporated herein as if set out in full in the Application. - The undersigned certifies individually and for Denali that the statements made in this Conforming Amendment to its Application are true, complete, and correct to the best of his knowledge and belief, and are made in good faith. Denali Telecom, LLC [ President, Rentriad North America, Inc. Manager of Denali Telecom, LLC 16 September 2002

€ED 2 HE OMAE LR END DRRD D2R REIEL DITE® &0 TA TS C SV CE E.0 P E N T R I A D Ihereby certify that I amthe technically qualified person responsible for preparation of the engineering information contained in this Conforming Amendment to the Application, that I amfamiliar with Part 25 of the Commission‘s Rules, that I have either prepared or teviewed the engineering information submitted in this Conforming Amendment to the Application, and that it is complete and accurate to the best of my knowledée and belief, .. LLDYAH Dr. Barton Huxtable User Systems, Incorporated Dated: 16 September 2002 (.

CERTIFICATE OF SERVICE 1 hereby certify that on the sixteenth day of September 2002, a true and correct copy of the foregoing Comments was sent via first—class mail, postage prepaid, or was hand— delivered, to each of the following: Ms. Jennifer Gilsenan Chief, Policy Branch, Satellite Division International Bureau Federal Communications Commission 445 12"" Street, SW Washington, DC 20554 Mr. Fern Jarmulnek Deputy Chief, Satellite Division International Bureau Federal Communications Commission 445 12"" Street, SW Washington, DC 20554 Mr. Karl A. Kensinger Special Advisor, Satellite Division International Bureau Federal Communications Commission 445 12"" Street, SW Washington, DC 20554 Mr. Thomas Tycz Division Chief Satellite Division— International Bureau Federal Communications commission 445 12" Street, SW Washington, DC 20554 Mr. Donald Abelson Bureau Chicef, International Bureau Federal Communications Commission 445 12"" Street, SW Washington, DC 20554

Mr. John Martin Senior Engineer Satellite Division International Bureau Federal Communications Commission 445 12th Street, SW Washington, DC 20554 Ms. Cassandra Thomas Deputy Chief, Satellite Division International Bureau Federal Communications Commission 445 12"" Street, SW Washington, DC 20554 s «_ TZ[PR omas J. Mackie Law erk, Pierson & Burnett, LLP Dated: September 16, 2002

APPENDIX 1 FCC Form 312

FCCForm Main 312 * es michunter I FEDERAL COMMUNICATIONS COMMISSION Rrfegone fifin. U**"* 2C1 calSign APPLICATION FOR SATELLITE SPACE AND EARTH STATION AUTHORIZATIONS Fee Numbe &7 ce Number: APPLICANT INFORMATION 1. Legal Name of Applicant 2. Voice Telephone Number Denali Telecom, L.L.C. (703) 683 3044 3. Other Name Used for Doing Business (if any) 4. Fax Telephone Number (703) 683 2044 5. Mailing Street Address or P.O. Box _ 6. City . 517 South Washington Street Alexandria . 7. State / Country (if not U.S.A.) 8. Zip Code AtteNtion: Dennis J. Burnett virginia 22314 9. Name of Contact Representative (If other than applicant) 10, Voice Telephone Number David L. Lihani (703) 683 3044 11. Firm or (.:ompany Name 12. Fax Telephone Number Pierson & Burnett, L.L.P. (703) 683 2044 13. Mailing Street Address or P.O. Box 14. City 517 South Washington Street Alexandria , R , 15. State / Country (if not U.S.A) 16. Zip Code aTrention: David L. Lihani virginia 22314 CLASSIFICATION OF FILING 17. Place an "X" in the box next to the classification that applies to this filing for both questions a. and b. Mark only one b ox for 1 7a and only one box for 17b. D b1. Application for License of New Station D b6. Transfer of Control of Licenseor Registration D‘L Earth Station . b2. Application pp for Registration TsoinecE, of New Station Mecoive‘Ouly ificati of Minor b7. Notification i ificati Modification b3. Amendment to a Pending Application b8. Application for License of New Receive—Only Station Using Non—U.S. Licensed Satellite 22. Space Station |__| b4. Modification ofLicense or Registration b9. Letter ofIntent to Use Non—U.S. Licensed Satellite to Provide Service in the United States D b5. Assignment of License or Registration D b10. Other (Please Specify): 18. If this filing is in reference to an existing station, enter: 19.If this filing is an amendment to a pending application enter: Call sign ofstation: (a) Date pending application was filed: (b) File numberof pending application: 9/26/97 160—SAT—P/LA —97/13 FCC 312. Main Form — Page 1 February, 1998

TYPE OF SERVICE 20. NATURE OF SERVICE: This filing is for an authorization to provide or use the following type(s) of service(s): Place an “X" in the box(es) next to all that apply. . a. Fixed Satellite ¢. Radiodetermination Satellite e. Direct to Home Fixed Satellite . b. Mobile Satellite d. Earth Exploration Satellite £. Digital Audio Redio Service Dg. Other (please specify) 21. STATUS; Place an "X"in the box next to the applicable status, Mark only one box. 22. If earth stition npfilicam, place an "X"in the box(es) next to all that apply. D a. Common Carrier @b. Non—Common Carrier Da. Using U.S. licensed satellites Dh Using Non—U.S. licensed satellites 23. If applicant is providing INTERNATIONAL COMMON CARRIER service, see instructions regarding Sec, 214 filings. Mark only one box. Are these facilities: Da. Connected to the Public Switched Network D Not connected to the Public Switched Network 24. FREQUENCY BAND(S): Place an "X" in the box(es) next to all applicable frequency band(s). a. C—Band (4/6 GHz) . X |b. Ku—Band (12/14 GHz) I }: Other (Please specify) TYPE OF STATION 25. CLASS OF STATION: Place an "X" in the box next to theclass of station that applies. Mark only one box. f. Other [___I.. Fixed Earth Station D Temporary—Fixed Earth Station D 12/14 GHz VSAT Network D Mobile Earth Station [B Space Station (Specify) If space station applicant, go to Question 27. 26. TYPE OF EARTH STATION FACILITY Mark only one box. D a. Transmit/Receive D Transmit—Only D Receive—Only PURPOSE OF MODIFICATION OR AMENDMENT 27. The purpose of this proposed modification or amendment is to: Placean "X" in the box(es) next to all that apply. a —— authorizationto add new emission designator and related service b —— authorization to change emission designator and related service ¢ —— authorization to increase EIRP and EIRP density d —— authorization to replace antenna e —— authorization to add antenna f —— authorization to relocate fixed station & —— authorization to change assigned frequency(ies) h —— authorization to add Points of Communication (satellites & countries) i —— authorization to change Points of Communication (satellites & countries) j —— authorization for facilities for which environmental assessmentand radiation hazard reporting is required k —— Other (Please Specify) Conforming Amendment to~ new PCC rules for Ku—band NGNn P ie ENVIRONMENTAL POLICY 28. Would a Commission grant of an: salin this application or amendment have a significant environmen as defined 47 CFR 1.1307? If YES, submit the sv.nemegnrlaas requl)r’epdnl’)'))'oSecums 1. l%%s and L.1311 of theCommmxons rules, 47 C.FR. 5}lI 08and L.1311,‘;ys an exhibit to this application. D YES M No FCC 312, Main Form — Page 2 February, 1998

ALIEN OWNERSHIP 29. Is the applicant a foreign government or the representative of any foreign government? — DYES NO 30. Is the applicant an alien or the representative of an alien? ¢ DYES m NO 31, Is the applicant a corporation organized under the laws of any foreign government? I:IYES m NO 32. Is the applicant a corporation of which more than one—fifth of the capital stock is owned of record or DYES NO voted by aliens or their representatives or by aforeign government or representative thereof or by any corporation organized under the laws of a foreign country? 33. Is the applicant a corporation directly or indirectly controlled by any other corporation of which more than one—fourth of the cagtal stock is owned of recon‘flor voted by aliens, their representatives, or by a foreign DYES No government or representative thereof or by any corporation organized under the laws of a foreign country? 34. If any answer to questions 29, 30, 31, 32 and/or 33 is Yes, attach as an exhibit, the identification of the aliens or foreign entities, their nationality, their relationship to the applicant, and the percentage of stock they own or vote. BASIC QUALIFICATIONS 35. Does the applicant request any waivers or exemptions from any of the Commission‘s Rules? per 47 cfr 1,1114 (a) YES DNO If Yes, attach as an exhibit, copies of the requests for waivers or exceptions with supporting documents.—neyw rules compli@nce 36. Has the applicant or any party to this application had any FCC station authorization or license revoked or had any application for an initial, modification or renewal ogFCC station authorization, license, or construction DYES E No permit denied by the Commission? If Yes, attach as an exhibit, an explanation of the circumstances. 37. Has the applicant, or any party to this application, or any party directly or indirectly controlling the applicant ever been convicted of a felony by any state or federal court? If Yes, attach as an exhibit, an explanation of the circumstances. D YES E No 38. Has any court finally adjudged the applicant, or any person directly or indirectly controlling the applicant, guilty of unlawfully DYES E No mono?olizing or attempting unlawfully to monopolize radio communication, directly or indirectly, through control of manufacture or sale of radio apparatus, exclusive traffic arrangement or any other means or unfair methods of competition? If Yes, attach as an exhibit, an explanation of the circumstances. 39. Is the applicant, or any person directly or indirectly controlling the applicant, currently a party in any pending matter refc to in the preceeding two items? If Yes, attach as an exhibit, an explanation of the circumstances. DYES B No 40. If the applicant is a cor?oration and is applying for a space station license, attach as an exhibit the names, addresses, and citizenship of thosesee 160—SAT—P/LA— stockholders owning of record and/or voting 10 percent or more of the Filer‘s voting stock and the percentages so held. In the case of fiduciary 97 13 control, indicate the beneficiary(ies) or class of beneficiaries. Also list the names and addresses of the officers and directors of the Filer. 41. By checking Yes, the undersigned certifies, that neither the applicant nor any other party to the application is subject to a denial of © Federal benefits that includes FCC benefits pursuant to Section 5301 of the Anti—Drug Act of 1988, 21 U.8.C. Scetion 862, becase [xyes [no of a conviction for possession or distribution of a controlled substance. See 47 CFR 1.2002(b) for the meaningof "party to the application" for these purposes. 42a. Does the applicant intend to use a non—U.S. licensed satellite to provide service in the United States? DYES L—XI NO If yes, answer 42b and attach an exhibit providing the information specified in 47 C.F.R. § 25.137, as appropriate. If no, proceed to question 43. 42b. What administration has licensed oris in the process of licensing the space station? If no license will USA be issued, what administration has coordinated or is in the process of coordinating the space station? FCC 312, Main Form — Page 3 February, 1998

43. Description. (Summarize the nature of the application and the services to be provided). The FCC required this conforming amendment from Applicant in order to comply with the commission‘s adopted rules in Report & Order (IB Docket No. 01—96, PCC 02—123, adopted April 18, 2002 and released Aprill—26,2002) concerning (a) required coverage latitude on Earth (b) orbital parameters and cli;ra; cteristics and (c) disclosure of orbital debris mitigation plans, prior to receiving FCC authorization to operate Exhibit No. Identify all exhibits that are attached to this Pentriad System S : Denali Telecom, LLC Pentriad Denali Telecom, LLC Pentriad Link Bu Denali Telecom, LLC I0C Antenna Pa Dena Telecom, LLC _FOC & S anten CERTIFICATION The Applicant waives any claim to the use of any particular frequency or of the electromagnetic spectrum as against the regulatory power of the United States because of the previous use of the same, whether by license or otherwise, and requests an authorization in accordance with this application. The applicant certifies that grant of this appfication would not cause the applicant to be in violation of the s'F:ctrum aggregation limit in 47 CFR Part 20. All statements made in exhibits are a material part hereof and are incorporated herein as if set out in full in this application. The undersigned, individually and for the applicant, hereby certifies that all statements made in this application and in all attached exhibits are true, complete and correct to the best of his or her knowledge and belief, and are made in good faith. 44. Applicantis a (an): (Place an "X" in the box next to applicable response.) m A faas & ; . — £. Other Da. Individual D b. Unincorporated Association Dc. Partnership D d. Corporation D e. Governmental Entity (P1easerré';l;"e%fy) L.L.C. 45. Typed Name of Person Signing 46. Title of Person Signing .s 3. Manager, Denali Telecom, Dennis J. s T ; L.L.C L.L.C. Burnett President, Pentriad North America, Inc. 47. Signature " 48. Date _ . (G TL WILLFUL FA STATEMENTS MADE ON THIS FORM ARE PUNISHABLE BY FINE AND/OR IMPRISONMENT .S. Code, Titl 18, Section 1001), AND/OR REVOCATION OF ANY STATION AUTHORIZATION (U.S. Code, Title 47, ection 312(a)(1 )» /OR FORFEITURE (U.S. Code, Title 47, Section 503). FCC 312, Main Form — Page 4 February, 1998

Exhibit 1: Pentriad System Service Area: South America

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Exhibit 3: nenali Telecom.LLC Pentriad Orbital Parameters Initial Operating Capability Satellite Period Inclination|Eccentricity| Apogee Perigee Argument R. A. Mean (sidereal (degrees) Height Height |of Perigee|Ascending| Anomaly hrs) (km) (km) (deg) Node (degrees) (degrees) 1 20 324 2 12.0 63.435 0.7133 39129 1237 270 140 84 3 260 204 Final Operating Capability Satellite Period |Inclination|Eccentricity| Apogee Perigee Argument R. A. Mean {sidereal (degrees) Height Height |of Perigee|Ascending| Anomaly hrs) (km) (km) (deg) Node (degrees) (degrees) 1~ 0 4 20 120 5 240 2 40 6 14.4 63.435 0.5945 41449 5784 270 140 160 7 280 3 80 8 260 200 9 320 Spares 10 20 0 11 9.6 63.435 0.4687 27239 5784 270 140 60 12 260 120 Southern Hemisphere Service Satellite Period |inclination| Eccentricity| Apogee Perigee Argument R. A. Mean {sidereal {degrees) Height Height {of Perigee|Ascending| Anomaly hrs) (km) (km) (deg) Node (degrees) (degrees) 13 90 324 14 12.0 63.435 0.7133 39129 1237 90 210 84 15 330 204

Exhibit 4: Denali Telecom, LLC, Pentriad Link Budget —Link Budget 256K service to 20" tracking antenna; 24,000 home stations Downlink Uplink Geometry Range R 43000 43000 km Signal Carrier Frequency f 13 13 GHz Bit rate 0.262 0.262 Mbps Bandwidth BW 0.125 0.125 MHz Spectral ratio 2.1 2.1 bps / Hz E_at_h Free space loss bs 207.4 207.4 dB Atmospheric loss Latmo 1.5 1.5 dB Edge of coverage loss Leage 1.0 1.0 dB Otherlosses Lother 1.0 1.0 dB Total path loss Lp 210.9 210.9 dB Transmitter Power Pr 9.0 —7.0 dBw Aperture diameter Dr 2.000 0.500 m Efficiency 0.75 0.5 Pointing loss 1.0 1.0 dB Gain C 46.5 32.7 dBi EIRP 37.4 25.7 dBw Receiver System Noise Temperature Ts 650 650 K Aperture diameter Dr 0.500 2.000 m Efficiency 0.5 0.75 Pointing loss 1.0 1.0 dB Gain Gr 32.7 46.5 dBi g/t 4.5 18.3 dB/K Link Performance Energy per bit E, —195.0 ~193.0 dB J Noise spectral density No —200.5 —200.5 dB W/Hz Ep/No 5.5 7.5 Demodulation loss 1.5 1.5 dB Signal—to—noise ratio SNR 4.0 6.0 dB Minimum SNR 3.0 3.0 dB Link Margin 1.0 3.0 dB Received power Pr —140.8 —138.8 dB W Noise power N ~149.5 ~149.5 dB W Carrier—to—noise ratio CNR 8.7 10.7 dB Power flux density PFD 116.2 dB W/im*2/MHz (No attenuation, no pointing loss) KU_LINK to home (down}.

EANLDLC 5:; Denallr lelecom, LLC IOC Antenna Pattern for Ku—Band

Exhibit 6: Denali Telecom, LLC FOC & SOC antenna pattern for Ku—Band.


Document Created: 2002-10-01 10:13:07
Document Modified: 2002-10-01 10:13:07
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