Narrative and Tech App

0184-EX-ML-2013 Text Documents

Panasonic Avionics Corporation

2013-09-30ELS_141853

Before the FEDERAL COMMUNICATIONS COMMISSION Washington, DC 20554 In the Matter of ) Application of Panasonic Avionics ) Call Sign WF2XMD Corporation To Modify Experimental ) File No. __________ License To Replace Two Satellites as ) Authorized Points of Communication ) ) APPLICATION FOR EXPERIMENTAL LICENSE MODIFICATION Panasonic Avionics Corporation (“Panasonic”), licensee of the “eXConnect” Ku-band aeronautical mobile-satellite system (“AMSS”) (“eXConnect System”), seeks to modify its experimental license1 by replacing two satellites as authorized points of communication on its existing authorization. Panasonic seeks to replace two currently-authorized satellites which are no longer utilized for eXConnect operations, Horizons-1 and Galaxy 19, with two other satellites, Satmex 8 and SES-6, with which Panasonic must conduct testing and demonstration for FAA certification and other purposes. The proposed operations are consistent with the coordinated parameters of the requested satellites, the Federal Communication Commission’s (“Commission” or “FCC”) two-degree spacing rules and the Commission’s rules and policies recently adopted for Ku- 1 See ELS File No. 0210-EX-RR-2013, Call Sign WF2XMD (granted July 12, 2011). Panasonic subsequently modified this authorization to confirm compliance with ITU regulations and other applicable regulatory requirements. ELS File No. 0143-EX-ML-2012 (granted August 21, 2012). Panasonic then renewed this authorization. ELS File No. 0210-EX-RR-2013 (granted June 7, 2013) (“Experimental License”). -1-

band earth stations aboard aircraft (“ESAAs”).2 For the reasons described herein, grant of the proposed experimental license modification would serve the public interest. I. DESCRIPTION OF EXPERIMENTAL OPERATIONS Panasonic currently is authorized under its experimental license to operate twenty aircraft earth stations (“AESs”) of two types – ten Mitsubishi Electronics Company (“MELCO”) reflector terminals and ten Aura LE terminals3 – with the following four satellite points of communication: Horizons-1, Telstar 14, Galaxy 17 and Galaxy 19.4 Panasonic requires the ability to access Satmex 8 and SES-6 satellites points of communications to address certification testing and integration issues associated with operations onboard foreign-registered aircraft on flights to and from the United States. Access to Satmex 8 and SES-6 would substitute for Horizons-1 and Galaxy 19; therefore, there is no increase in the potential for interference because Panasonic seeks authority to communicate using the same number of terminals with the same number of satellite points of communication. Concurrent herewith, Panasonic is filing an application to modify its commercial aeronautical mobile-satellite service (“AMSS”) blanket license to add Satmex 8 and SES-6, as 2 See Revisions to Parts 2 and 25 of the Commission’s Rules to Govern the Use of Earth Stations Aboard Aircraft Communicating with Fixed-Satellite Service Geostationary-Orbit Space Stations Operating in the 10.95-11.2 GHz, 11.45-11.7 GHz, 11.7-12.2 GHz and 14.0-14.5 GHz Frequency Bands; Service Rules and Procedures to Govern the Use of Aeronautical Mobile Satellite Service Earth Stations in Frequency Bands Allocated to the Fixed Satellite Service, IB Docket Nos. 12-376 & 05-20, Notice of Proposed Rulemaking and Report and Order, FCC 12- 161 (rel. Dec. 28, 2012) (“ESAA Order”). 3 The Aura LE terminal, previously manufactured by EMS Technologies, is now manufactured by Panasonic Avionics. The design and operational characteristics of the terminal have not changed. 4 See Experimental License at 1. -2-

well as other satellites, as authorized points of communication.5 However, during the pendency of that application, there is a near-term need to access the proposed satellites for limited certification and network integration purposes. Panasonic will conduct operations with Satmex 8 and SES-6 consistent with its existing experimental authority6 and incorporates by reference the technical information submitted in that proceeding. That technical information, as well as the detailed information filed in connection with Panasonic’s recent Authorization7 and pending Modification Application,8 demonstrates the non-interfering operations of the eXConnect terminals and consistency with Ku-band AES licensing policies. Other than substituting access to Satmex 8 and SES-6 for Horizons 1 and Galaxy-19 as proposed herein, Panasonic seeks no changes to its existing experimental authority. 5 See Application of Panasonic Avionics Corporation To Modify AMSS License To Permit Operation of Up to 2000 Technically Identical Aeronautical Mobile-Satellite Service (“AMSS”) Aircraft Earth Stations (“AESs”) in the 14.0-14.5 GHz and 10.7-12.75 GHz Frequency Bands, Call Sign E100089, File No. SES-MFS-20130930-00845 (filed Sept. 30, 2013) (“Modification Application”). 6 Id. 7 Radio Station Authorization to Panasonic Avionics Corporation, File No. SES-MFS-20120913- 00818, Call Sign: E100089 (July 24, 2013) (granting authority to Panasonic to operate up to 50 (.68 cm antennas) MELCO remote terminals in CONUS, AK, HI and U.S. Territories and operate up to 2000 (.89 M. antennas) remote AURA LE remote terminals) (“Authorization”); Radio Station Authorization to Panasonic Avionics Corporation, File No. SES-AFS-20130220- 00189, Call Sign: E100089 (July 24, 2013) (granting authority to Panasonic to operate up to 15 (.68 cm antennas) MELCO remote terminals in CONUS, AK, HI and U.S. Territories and operate up to 2000 (.89 M. antennas) remote AURA LE remote terminals) (“Authorization”); Satellite Communications Services Information re: Actions Taken, Public Notice, Report No. SES-01573 (July 31, 2013). 8 Extensive technical information is available in the record of Panasonic’s pending commercial license modification. See Modification Application at Technical Appendix. -3-

II. SATELLITE POINTS OF COMMUNICATION Panasonic seeks authority for the Aura LE terminal to communicate with Satmex 8 and SES-6 satellites, and for the MELCO terminal to communicate with SES-6. In addition, Panasonic seeks to remove Horizons-1 and Galaxy 19 points of communication from its experimental license because Panasonic no longer utilizes these two satellites for eXConnect operations. Panasonic, therefore, need not conduct further demonstration or certification testing with these satellites. Panasonic proposes to modify its existing experimental license by listing the following satellites as authorized points of communication:  Galaxy 17 at 91°W  Telstar 14R at 63°W  Satmex 8 at 116.8°W  SES-6 at 40.5°W Panasonic will access these satellites within parameters consistent with its existing experimental license. Accordingly, grant of the requested license modification would not increase the potential for interference from Panasonic’s experimental operations. Satmex 8 is a Mexico-licensed satellite included on the Commission’s Permitted Space Station List for Fixed Satellite Service (“FSS”).9 SES-6, which successfully launched in June 2013,10 is a Netherlands-licensed space station included on the Permitted Space Station List for 9 Satelites Mexicanos S. A. de C. V. Petition for Declaratory Ruling to add the Satmex 8 satellite to the Permitted Space Station List, File No. SAT-PPL-20120823-00140 (Call Sign S2873) (granted Dec 6, 2012). 10 Letter from Daniel C.H. Mah, Regulatory Counsel for New Skies Satellites B.V., to Marlene H. Dortch, Sec’y of the Fed. Commc’ns Comm’n (June 13, 2013) in File No. SAT-PPL-2012- 0717-00117 (Call Sign S2870). -4-

FSS.11 In support of this application, Panasonic is submitting letters from the operators of Satmex 8 and SES-6 to Panasonic confirming that the proposed Ku-band AMSS operations are consistent with each operators’ coordination agreements and will not result in unacceptable interference to other satellite operations.12 eXConnect terminals have operated with satellites around the world without a single reported case of interference. Panasonic does not seek to extend the term of its existing authorization or add to the number of terminals.13 Panasonic seeks to ensure its authority to address certification, integration and implementation issues while it actively pursues full commercial licensing.14 Given that the subject terminals installed on foreign aircraft already communicate with the above-referenced satellites outside U.S. airspace without causing interference, no material concerns would be raised by adding these satellites to Panasonic’s existing experimental license authorization. Panasonic’s track record of non-interfering operations further establish that authority for the proposed experimental operations can be granted expeditiously as requested herein. 11 New Skies Satellites B.V., Request for U.S. Market Access for SES-6, Petition, File No. SAT- PPL-2012-0717-00117 (Call Sign S2870) (granted July 17, 2013); Policy Branch Information Actions Taken, Public Notice, Report No. SAT-00962, File No. SAT-PPL-2012-0717-00117 (Call Sign S2870) (July 19, 2013). 12 See Attached Technical Appendix. 13 Because the eXConnect network is a TDMA-based system, Panasonic would note that only one terminal ever transmits at one particular time. 14 See Modification Application. -5-

IV. CONCLUSION Grant of the license modification application would enable Panasonic to address certification and implementation issues and further develop its eXConnect System for U.S. and foreign-registered aircraft operating on flights to and from the United States. Panasonic respectfully requests that the Commission expeditiously grant the proposed experimental license modification in order to facilitate the continued implementation of in-flight connectivity offerings to passengers and crews onboard foreign-registered aircraft. -6-

ATTACHMENT 1 Technical Appendix

Technical Appendix Contents Summary Satmex 8 Coverage Map 1-1 Link Budget 1-2 Coordination Letter 1-3 Emissions Designators 1-4 SES-6 Coverage Map 2-1 Link Budget for Aura LE 2-2 Coordination Letter 2-3 Emissions Designators for PPA (Aura LE) 2-4 Link Budget for MELCO 2-5 Link Budget for MELCO 2-6 Emissions Designators for MELCO 2-7

Satmex 8 Coverage Map

Satmex 8 Link Budget Forward Link Budget Return Link Budget eXConnect Terminal eXConnect Terminal Site Maine Site Maine Antenna Type AURA LE Antenna Type AURA LE Lat 44.5 deg Lat 44.5 deg Lon -69.2 deg Lon -69.2 deg EIRP max 42.9 dBW EIRP max 42.9 dBW G/T 10.1 dB/K G/T 10.1 dB/K Satellite Satellite Name SM8 Name SM8 Longitude -116.8 deg Longitude -116.8 deg Hub Earth Station Hub Earth Station Site Brewster Site Brewster Lat 48.1 deg Lat 48.1 deg Lon -119.8 deg Lon -119.8 deg EIRP max 77.0 dBW EIRP max 77.0 dBW G/T 37.4 dB/K G/T 37.4 dB/K Signal Signal Waveform DVB-S2 iDX2 Waveform iDirect Modulation QPSK Modulation BPSK Bits per symbol 2 Bits per symbol 1 Spread Factor 1 Spread Factor 2 Coding Rate 0.83 Coding Rate 0.67 Overhead Rate 0.93 Overhead Rate 0.72 Channel Spacing 1.20 Channel Spacing 1.20 Spectral Efficiency (Rate/Noise BW) 1.56 bps/Hz Spectral Efficiency (Rate/Noise BW) 0.24 bps/Hz Data Rate 4.67E+07 bps Data Rate 1.61E+06 bps Information Rate (Data + Overhead) 5.00E+07 bps Information Rate (Data + Overhead) 2.22E+06 bps Symbol Rate 3.00E+07 Hz Symbol Rate 3.34E+06 Hz Chip Rate (Noise Bandwidth) 3.00E+07 Hz Chip Rate (Noise Bandwidth) 6.67E+06 Hz Occupied Bandwidth 3.60E+07 Hz Occupied Bandwidth 8.00E+06 Hz Power Equivelent Bandwidth 3.60E+07 Hz Power Equivelent Bandwidth 8.34E+04 Hz C/N Threshold 5.6 dB C/N Threshold -1.2 dB Uplink Uplink Frequency 14.250 GHz Frequency 14.250 GHz Back off 3.9 dB Back off 0.0 dB EIRP Spectral Density 34.3 dBW/4kHz EIRP Spectral Density 10.7 dBW/4kHz Slant Range 38211 km Slant Range 39503 km Space Loss, Ls 207.2 dB Space Loss, Ls 207.5 dB Pointing Loss, Lpnt 0.0 dB Pointing Loss, Lpnt 0.1 dB Atmosphere / Weather Loss, La 1.0 dB Atmosphere / Weather Loss, La 0.0 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB Transponder G/T @ Hub 4.0 dB/K Transponder G/T @ Terminal 5.0 dB/K Thermal Noise, C/No 97.6 dBHz Thermal Noise, C/No 68.9 dBHz C/(No+Io) 97.1 dBHz C/(No+Io) 68.4 dBHz Satellite Satellite Flux Density -90.5 dBW/m2 Flux Density -120.2 dBW/m2 SFD @ Hub -88.2 dBW/m2 SFD @ Terminal -89.2 dBW/m2 Small Signal Gain (IBO/OBO) 1.3 dB Small Signal Gain (IBO/OBO) 1.3 dB OBO 1.0 dB OBO 29.7 dB Downlink Downlink Frequency 12.000 GHz Frequency 12.000 GHz Transponder Sat. EIRP @ Beam Peak 51.7 dBW Transponder Sat. EIRP @ Beam Peak 51.7 dBW Transponder Sat. EIRP @ Terminal 50.9 dBW Transponder Sat. EIRP @ Hub 48.9 dBW DL PSD Limit 14.5 dBW/4kHz DL PSD Limit 14.5 dBW/4kHz DL PSD @ Beam Peak 11.9 dBW/4kHz DL PSD @ Beam Peak -10.2 dBW/4kHz Carrier EIRP @ Beam Peak 50.7 dBW Carrier EIRP @ Beam Peak 22.0 dBW Carrier EIRP @ Terminal 49.9 dBW Carrier EIRP @ Hub 19.3 dBW Slant Range 39503 km Slant Range 38211 km Space Loss, Ls 205.9 dB Space Loss, Ls 205.7 dB Pointing Loss, Lpnt 0.1 dB Pointing Loss, Lpnt 0.0 dB Atmosphere / Weather Loss, La 0.0 dB Atmosphere / Weather Loss, La 1.2 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB PCMA Loss 0.0 dB PCMA Loss 0.0 dB Thermal Noise, C/No 82.6 dBHz Thermal Noise, C/No 78.3 dBHz C/(No+Io) 82.4 dBHz C/(No+Io) 77.8143 dBHz End to End End to End End to End C/(No+Io) 82.2 dBHz End to End C/(No+Io) 67.9 dBHz Implementation Loss 1.5 dB Implementation Loss 0.0 dB End to End C/N w/ Imp Loss 5.9 dB End to End C/N w/ Imp Loss -0.3 dB Link Margin 0.3 dB Link Margin 0.9 dB

SATMEX REACHING HIGhER September 26, 2013 Mark DeFazio Manager, GCS Regulatory and Business Operations Panasonic Avionics Corporation 26200 Enterprise Way Lake Forest, CA 92630 Re: Certification of Conformance with Satellite Operator Coordination Agreements Dear Mr. DeFazio: You have requested that Satelites Mexicanos S. A. de C.V. ("Satmex") confirm it has reviewed the technical characteristics of Panasonic Avionics Corporation‘s ("Panasonic") Ku—band aeronautical mobile—satellite service ("AMSS") operations with the Satmex 8 satellite at 116.8° W.L., using the "North American" beam of this satellite. You have further requested that Satmex certify that such operations are consistent with Satmex‘s coordination agreements and will not result in unacceptable interference to other satellite operations within +/— 6 degrees of Satmex 8. As set forth in materials submitted to the U.S. Federal Communications Commission ("FCC"), the basic characteristics of the Panasonic phased—array ("PPA") aircraft earth station ("AES") terminal (referred to previously as the "Aura LE" terminal) for operation with the Satmex 8 satellite include: Antenna Dimensions 0.89 m (0.17m in height) Type of Antenna Dual panel waveguide feed phased array SSPA Rated Output Power 16 watts Bandwidth Receive: 11.7 GHz to 12.2 GHz Transmit: 14.0 GHz to 14.5 GHz Transmit Gain 37 dBi at 14.25 GHz EIRP 48 dBW Transmit Polarization Linear: Horizontal or Vertical Receive G/T 10 to 14 dB/K Transmit Azimuth Beamwidth 1.5 degrees Transmit Elevation Beamwidth 4 degrees Pointing Accuracy 0.2 degrees (3—sigma, automatic cut—off at 0.35 degrees offset)

SATMEX REACHING HIGMER We understand that the PPA AES terminal is designed to comply with the FCC‘s rules and policies governing Ku—band earth stations aboard aircraft ("ESAAs") adopted in new Section 25.227 of the rules.‘ In addition, the PPA AES terminal has operated without interference under various FCC experimental and commercial authorizations." The PPA AES terminal avoids interference to other satellite operations by limiting off—axis EIRP spectral density towards orbital slots 118.7° and 114.9° to no more than 27 dBW/ MHz, through various means, including: (i) limiting transmit power spectral density by controlling the transmit power of the terminal and using spread spectrum technology (selecting appropriate carrier bandwidths and spread factors); (ii) controlling the off—axis gain of the antenna along the GSO by inhibiting transmissions when the skew angle exceeds a specified threshold; and (iii) controlling pointing error and inhibiting transmissions when the pointing offset exceeds the specified threshold of 0.35 degrees. When operating as described in the materials submitted to the FCC and with the associated off— axis EIRP density envelope for the Satmex 8 satellite (which is consistent with the Commission‘s two—degree spacing requirements), Panasonic‘s proposed operations comply with the off—axis EIRP density level requirements necessary to protect potentially affected satellites up to and including 6° off—axis from the Satmex 8 satellite (including the satellites in applicable coordination agreements) and it is not expected to cause unacceptable interference into these adjacent satellites. The skew angle is constantly monitored by the antenna control system and the aircraft transmission will be muted in the event the skew angle of +/—35° is exceeded. Satmex understands that the maximum downlink satellite EIRP density of 13.0 dBW/A4kHz, the operational level of the Ku—band AMSS network operated by Panasonic, is routinely used without causing unacceptable interference to adjacent satellite operations. Satmex understands that the maximum uplink off—axis EIRP spectral density limit of —50 + (29— 25 * Log1O0(theta)) dBW/Hz with a maximum uplink EIRP of 48dBW up to a 1668ksps carrier, where theta is the off—axis angle, is the operational level of the Ku—band AMSS network operated by Panasonic, and is routinely used without causing unacceptable interference to adjacent satellite operations. DE "A47 CER §25.2327. 2 See File Nos. SES—LIC—20100805—00992, SES—AMD—20100914—01163, SES—AMD—20101115— 01432, SES—AMD—20110325—00358; SES—AFS—20110405—00402, SES—STA—20110104—00005 (Call Sign: E100089) (granted Aug. 31, 201 1); ELS File Nos. 0210—EX—RR—2013 (granted July 12, 2011), 0143—EX—ML—2012 (granted August 21, 2012), 0210—EX—RR—2013 (granted June 7, 2013) (Call Sign WF2XMD).

SATME X REACHING HIGHER In view of the foregoing and consultations between Satmex engineering staff and Panasonic, Satmex hereby confirms the following: 1: Satmex is familiar with the technical characteristics of the PPA AES terminal. The proposed operations of the PPA AES terminal with the Satmex 8 satellite have the potential to receive harmful interference from adjacent satellite networks that may be unacceptable. The power density levels and associated off—axis gain performance of its PPA AES terminal that Panasonic provided to Satmex are consistent with the existing coordination agreements between Satmex and the adjacent satellite systems within 6° of orbital separation from the Satmex 8 satellite. Pursuant to the international regulation for the AMSS services, Satmex will include the power—density levels and associated off—axis gain performance of its PPA AES terminal of the proposed operations in all future coordination agreements for the Satmex 8 satellite. Operation of the PPA AES terminal will not cause unacceptable interference into other operations on Satmex 8, or adjacent satellites, and are otherwise in accordance with Satmex‘s technical requirements and applicable operational limitations, including coordinated off—axis EIRP density levels. Please let me know if you require any additional information regarding Panasonic‘s operation of the Ku—band PPA AMSS terminal with the Satmex 8 satellite. Sincerely, Hector Fortis SATMEX International and Regulatory Affairs

Satmex 8 Emissions Designators Max EIRP Density Per Carrier (dBW/4kHz) Max EIRP per Carrier (dBW) Satellite and Beam Name Emission Designator Bandwdith (Hz) Tx/Rx Satmex-8 Tx 500KG7D 500,000 34.70 14.52 Satmex-8 Tx 9M00G7D 9,000,000 47.25 14.52 Satmex-8 Rx 1M20G7D 1,200,000 Satmex-8 Rx 36M0G7D 36,000,000 1-4

SES-6 Coverage Map Figure 1: SES-6 AE Coverage

Figure 2: SES-6 AW Coverage

SES-6 Link Budget Forward Link Budget Return Link Budget eXConnect Terminal eXConnect Terminal Antenna Type AURA LE Antenna Type AURA LE Lat 63.7 deg Lat 63.7 deg Lon -18.4 deg Lon -18.4 deg EIRP max 42.5 dBW EIRP max 42.5 dBW G/T 10.0 dB/K G/T 10.0 dB/K Satellite Satellite Name SES-6 Name SES-6 Longitude -40.5 deg Longitude -40.5 deg Hub Earth Station Hub Earth Station Site Cologne Site Cologne Lat 50.863 deg Lat 50.863 deg Lon 6.848 deg Lon 6.848 deg EIRP max 80.0 dBW EIRP max 80.0 dBW G/T 35.0 dB/K G/T 35.0 dB/K Signal Signal Waveform DVB-S2 iDX2 Waveform iDirect Modulation QPSK Modulation BPSK Bits per symbol 2 Bits per symbol 1 Spread Factor 1 Spread Factor 4 Coding Rate 0.67 Coding Rate 0.66 Overhead Rate 0.94 Overhead Rate 0.75 Channel Spacing 1.20 Channel Spacing 1.20 Spectral Efficiency (Rate/Noise BW) 1.26 bps/Hz Spectral Efficiency (Rate/Noise BW) 0.12 bps/Hz Data Rate 5.66E+07 bps Data Rate 8.27E+05 bps Information Rate (Data + Overhead) 6.00E+07 bps Information Rate (Data + Overhead) 1.10E+06 bps Symbol Rate 4.50E+07 Hz Symbol Rate 1.67E+06 Hz Chip Rate (Noise Bandwidth) 4.50E+07 Hz Chip Rate (Noise Bandwidth) 6.67E+06 Hz Occupied Bandwidth 5.40E+07 Hz Occupied Bandwidth 8.00E+06 Hz Power Equivelent Bandwidth 7.20E+07 Hz Power Equivelent Bandwidth 6.09E+05 Hz C/N Threshold 3.5 dB C/N Threshold -3.5 dB Uplink Uplink Frequency 14.250 GHz Frequency 14.250 GHz Back off 1.7 dB Back off 0.0 dB EIRP Spectral Density 37.8 dBW/4kHz EIRP Spectral Density 10.3 dBW/4kHz Slant Range 39858 km Slant Range 39969 km Space Loss, Ls 207.4 dB Space Loss, Ls 207.4 dB Pointing Loss, Lpnt 0.0 dB Pointing Loss, Lpnt 0.1 dB Atmosphere / Weather Loss, La 2.5 dB Atmosphere / Weather Loss, La 0.0 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB Transponder G/T @ Hub 1.0 dB/K Transponder G/T @ Terminal 3.0 dB/K Thermal Noise, C/No 98.1 dBHz Thermal Noise, C/No 66.6 dBHz C/(No+Io) 97.6 dBHz C/(No+Io) 66.1 dBHz Satellite Satellite Flux Density -87.2 dBW/m2 Flux Density -120.7 dBW/m2 SFD @ Hub -87.2 dBW/m2 SFD @ Terminal -89.2 dBW/m2 Small Signal Gain (IBO/OBO) 0.0 dB Small Signal Gain (IBO/OBO) 3.0 dB OBO 0.0 dB OBO 28.5 dB Downlink Downlink Frequency 12.000 GHz Frequency 12.000 GHz Transponder Sat. EIRP @ Beam Peak 49.2 dBW Transponder Sat. EIRP @ Beam Peak 49.2 dBW Transponder Sat. EIRP @ Terminal 49.0 dBW Transponder Sat. EIRP @ Hub 47.0 dBW DL PSD Limit 13.0 dBW/4kHz DL PSD Limit 13.0 dBW/4kHz DL PSD @ Beam Peak 8.7 dBW/4kHz DL PSD @ Beam Peak -11.5 dBW/4kHz Carrier EIRP @ Beam Peak 49.2 dBW Carrier EIRP @ Beam Peak 20.7 dBW Carrier EIRP @ Terminal 49.0 dBW Carrier EIRP @ Hub 18.5 dBW Slant Range 39969 km Slant Range 39858 km Space Loss, Ls 205.4 dB Space Loss, Ls 205.4 dB Pointing Loss, Lpnt 0.1 dB Pointing Loss, Lpnt 0.0 dB Atmosphere / Weather Loss, La 0.0 dB Atmosphere / Weather Loss, La 2.6 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB PCMA Loss 0.0 dB PCMA Loss 0.0 dB Thermal Noise, C/No 82.1 dBHz Thermal Noise, C/No 74.0 dBHz C/(No+Io) 81.9 dBHz C/(No+Io) 73.1616 dBHz End to End End to End End to End C/(No+Io) 81.8 dBHz End to End C/(No+Io) 65.3 dBHz Implementation Loss 1.5 dB Implementation Loss 0.0 dB End to End C/N w/ Imp Loss 3.7 dB End to End C/N w/ Imp Loss -2.9 dB Link Margin 0.2 dB Link Margin 0.6 dB Figure 1: SES-6 AE Link Budget

Forward Link Budget Return Link Budget eXConnect Terminal eXConnect Terminal Antenna Type AURA LE Antenna Type AURA LE Lat 74.4 deg Lat 74.4 deg Lon -71.9 deg Lon -71.9 deg EIRP max 42.5 dBW EIRP max 42.5 dBW G/T 10.0 dB/K G/T 10.0 dB/K Satellite Satellite Name SES-6 Name SES-6 Longitude -40.5 deg Longitude -40.5 deg Hub Earth Station Hub Earth Station Site Cologne Site Cologne Lat 50.86 deg Lat 50.86 deg Lon 6.848 deg Lon 6.848 deg EIRP max 74.5 dBW EIRP max 74.5 dBW G/T 35.0 dB/K G/T 35.0 dB/K Signal Signal Waveform DVB-S2 iDX2 Waveform iDirect Modulation QPSK Modulation BPSK Bits per symbol 2 Bits per symbol 1 Spread Factor 1 Spread Factor 8 Coding Rate 0.33 Coding Rate 0.67 Overhead Rate 0.92 Overhead Rate 0.72 Channel Spacing 1.20 Channel Spacing 1.20 Spectral Efficiency (Rate/Noise BW) 0.61 bps/Hz Spectral Efficiency (Rate/Noise BW) 0.06 bps/Hz Data Rate 2.32E+07 bps Data Rate 4.03E+05 bps Information Rate (Data + Overhead) 2.53E+07 bps Information Rate (Data + Overhead) 5.56E+05 bps Symbol Rate 3.79E+07 Hz Symbol Rate 8.33E+05 Hz Chip Rate (Noise Bandwidth) 3.79E+07 Hz Chip Rate (Noise Bandwidth) 6.67E+06 Hz Occupied Bandwidth 4.55E+07 Hz Occupied Bandwidth 8.00E+06 Hz Power Equivelent Bandwidth 7.20E+07 Hz Power Equivelent Bandwidth 2.88E+05 Hz C/N Threshold -0.8 dB C/N Threshold -7.2 dB Uplink Uplink Frequency 14.250 GHz Frequency 14.250 GHz Back off 1.1 dB Back off 0.0 dB EIRP Spectral Density 33.7 dBW/4kHz EIRP Spectral Density 10.3 dBW/4kHz Slant Range 39858 km Slant Range 41170 km Space Loss, Ls 207.4 dB Space Loss, Ls 207.6 dB Pointing Loss, Lpnt 0.0 dB Pointing Loss, Lpnt 0.1 dB Atmosphere / Weather Loss, La 2.5 dB Atmosphere / Weather Loss, La 0.0 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB Transponder G/T @ Hub 0.0 dB/K Transponder G/T @ Terminal 0.0 dB/K Thermal Noise, C/No 92.2 dBHz Thermal Noise, C/No 63.3 dBHz C/(No+Io) 91.7 dBHz C/(No+Io) 62.8 dBHz Satellite Satellite Flux Density -92.1 dBW/m2 Flux Density -120.9 dBW/m2 SFD @ Hub -86.1 dBW/m2 SFD @ Terminal -86.2 dBW/m2 Small Signal Gain (IBO/OBO) 3.0 dB Small Signal Gain (IBO/OBO) 3.0 dB OBO 3.0 dB OBO 31.7 dB Downlink Downlink Frequency 12.000 GHz Frequency 12.000 GHz Transponder Sat. EIRP @ Beam Peak 48.1 dBW Transponder Sat. EIRP @ Beam Peak 47.0 dBW Transponder Sat. EIRP @ Terminal 47.0 dBW Transponder Sat. EIRP @ Hub 47.0 dBW DL PSD Limit 13.0 dBW/4kHz DL PSD Limit 13.0 dBW/4kHz DL PSD @ Beam Peak 5.3 dBW/4kHz DL PSD @ Beam Peak -17.0 dBW/4kHz Carrier EIRP @ Beam Peak 45.1 dBW Carrier EIRP @ Beam Peak 15.3 dBW Carrier EIRP @ Terminal 44.0 dBW Carrier EIRP @ Hub 15.3 dBW Slant Range 41170 km Slant Range 39858 km Space Loss, Ls 205.7 dB Space Loss, Ls 205.4 dB Pointing Loss, Lpnt 0.1 dB Pointing Loss, Lpnt 0.0 dB Atmosphere / Weather Loss, La 0.0 dB Atmosphere / Weather Loss, La 2.6 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB PCMA Loss 0.0 dB PCMA Loss 0.0 dB Thermal Noise, C/No 76.8 dBHz Thermal Noise, C/No 70.8 dBHz C/(No+Io) 76.6 dBHz C/(No+Io) 69.9147 dBHz End to End End to End End to End C/(No+Io) 76.5 dBHz End to End C/(No+Io) 62.0 dBHz Implementation Loss 1.5 dB Implementation Loss 0.0 dB End to End C/N w/ Imp Loss -0.8 dB End to End C/N w/ Imp Loss -6.2 dB Link Margin 0.0 dB Link Margin 1.0 dB Figure 2: SES-6 AW Link Budget

SES* 30 August 2013 Mark DeFazio Manager, GCS Regulatory and Business Operations Panasonic Avionics Corporation 26200 Enterprise Way Lake Forest, CA 92630 Re: Certification of Coordination for Operation with SES—6 Dear Mr. DeFazio: You have requested that New Skies Satellites B.V. ("New Skies," doing business as "SES") confirm it has reviewed the technical characteristics of Panasonic Avionics Corporation‘s ("Panasonic‘) Ku—band aeronautical mobile—satellite service ("AMSS") operations with the SES—6 satellite at 40.5° W.L., using the East Atlantic ("ATE") and West Atlantic ("ATW") Ku—band beams of this satellite. You have further requested that SES certify such operations have been included in and are consistent with SES‘s coordination agreements, and will not result in unacceptable interference to other satellite operations within +/— 6 degrees of SES—6. Given the location and coverage area of the SES—6 satellite, we understand that Panasonic seeks to operate in excess of the two—degree spacing levels adopted by the U.S. Federal Communications Commission ("FCC") for routine Ku—band earth station licensing! and embodied in off—axis EIRP spectral density mask applicable to Ku—band mobile VSAT operations." Specifically, Panasonic seeks to operate at off—axis EIRP spectral density levels up to 5 dB higher than the FCC mask, which is consistent with the coordinated levels of the SES—6 satellite and permitted by the FCC rules.3 In addition, SES understands that the FCC has granted Panasonic with authority for such higher power operations with other satellites (up to the coordinated levels of the serving satellite).* 1 See 47 C.FR. §25.218(D). 2 See 47 C.F.R. §§25.222(a)(1)(i)(a), 25.226(a)(1)(i)(a) and 25.227(a)(1)(i)(a). 3 See 47 C.F.R. §§25.222(a)(2), 25.226(a)(2) and 25.227(a)(2). * Panasonic Avionics Corporation, Radio Station Authorization, Call Sign E100089, File No. SES— MFS—20120913—00818 (granted July 24, 2013) ("Blanket AES License") and Application SES | 1129 20" Street W, Suite 1000 | Washinglon, DC 20036 |USA | Tel: +1 202478 7100 Faxc +1 202 478 7101 | wnses.com

The FCC has authorized Panasonic to operate two Ku—band AMSS aircraft earth station SES* ("AES") terminal types: the Panasonic phased—array ("PPA") terminal (referred to previously as the "Aura LE") and the MELCO terminals The basic characteristics of these terminals set forth in the FCC authorization and associated materials submitted to the FCC include: Antenna PPA AES MELCO Dimensions 0.89 m 0.68 m (0.17 m in height) (0.18 m in height) Type of Antenna Dual panel waveguide fed Elliptical, mechanically phased array steered cassegrain Max. Input Power at 16 watts 9.9 watts Antenna Flange Bandwidth 10.95—11.2 GHz; 11.45—12.2 10.95—11.2 GHz; 11.45—12.2 GHz (receive); 14.0—14.5 GHz GHz (receive); 14.0—14.4 GHz (transmit) (transmit) Transmit Gain 37 dBi at 14.25 GHz 32.2 dBi at 14.25 GHz Max. EIRP 48 dBwW 42.1 dBW Transmit Horizontal or Vertical Horizontal or Vertical Polarization Receive G/T 10 to 14 dB/K 8.0 to 9.3 dB/K Transmit Azimuth 1.5 degrees 1.5 degrees Beamwidth Transmit Elevation 4 degrees 5.6 degrees Beamwidth Pointing Accuracy 0.2 degrees (3—sigma, 0.25 degrees (3—sigma, automatic cut—off at 0.35 automatic cut—off at 0.5 degrees offset) degrees offset) We understand that the PPA AES and MELCO terminals are designed to comply with the FCC‘s rules and policies governing Ku—band earth stations aboard aircraft ("ESAAs") adopted in new Section 25.227 of the rules.© In addition, the terminals have operated without interference under various FCC experimental and commercial authorizations." Narrative at 8—10, 14 (confirming higher power operations with certain satellite points of communication, including Eutelsat 10A}. 5 See Blanket AES License at 3 (Section E — Antenna Facilities}. 647 C.E.R. §25.227. 7 See File Nos. SES—LIC—20100805—00992, SES—AMD—20100914—01163, SES—STA—20110104— 00005 (Call Sign: E100089); ELS File Nos. 0210—EX—RR—2013 (granted July 12, 2011), 0143—EX— SE | 1129 20° Street NW, Sute 1000 | Washington, DC 20086 |USA | Tel: +1 202478 7100 | Fax: +1 202 478 7101 | unnwses.com

The PPA AES and MELCO terminals avoid interference to other satellite operations by SES* limiting off—axis EIRP spectral density to no more than coordinated levels through various means, including: (i) limiting transmit power spectral density by controlling the transmit power of the terminal and using spread spectrum technology (selecting appropriate carrier bandwidths and spread factors); (ii) controlling the off—axis gain of the antenna along the GSO by inhibiting transmissions when the skew angle exceeds a specified threshold; and (iii) controlling pointing error and inhibiting transmissions when the pointing offset exceeds the specified threshold (0.35 degrees for the PPA AES; 0.5 degrees for the MELCO}. When operating in the manner authorized by the FCC and with the associated off—axis EIRP density envelope for the SES—6 satellite (which is 5 dB higher than the Commission‘s two—degree spacing levels), Panasonic‘s proposed operations comply with the off—axis EIRP density levels necessary to protect potentially affected satellites up to and including 6° off—axis from the SES—6 satellite and will not cause unacceptable interference into these adjacentsatellites. SES confirms that the maximum downlink satellite EIRP density of 13.0 dBW/KHz, the operational level of the Ku—band AMSS network operated by Panasonic, is routinely used without causing unacceptable interference to adjacentsatellite operations. In view of the foregoing and consultations between SES engineering staff and Panasonic, SES hereby confirms the following: 1. SES is familiar with the technical characteristics of the PPA AES and MELCO terminals. 2. The proposed operations of the PPA AES and MELCO terminals with the SES—6 satellite have the potential to receive harmful interference from adjacent satellite networks that may be unacceptable. 3. The power density levels and associated off—axis gain performance ofits PPA AES and MELCO terminals that Panasonic provided to SES are consistent with the existing coordination agreements between SES and the adjacent satellite systems within 6° of orbital separation from the SES—6 satellite. 4. SES will include the power—density levels and associated off—axis gain performance ofits PPA AES and MELCO terminals of the proposed operations in all future coordination agreements for the SES—6 satellite. ML—2012 (granted August 21, 2012), 0210—EX—RR—2013 (granted June 7, 2013) (Call Sign WE2XMD). SES | 1120 20" Street NW, Sute 1000 | Washington, DC 20036 |USA | Tel:+1 202478 7100| Faxc +1 202 478 7101 | uninses.com

5. Operation of the PPA AES and MELCO terminals will not cause unacceptable interference into other operations on SES—6, or adjacent satellites, and are SES* otherwise in accordance with SES‘ technical requirements and applicable operationallimitations, including coordinated off—axis EIRP density levels. Please let me know if you require any additional information regarding Panasonic‘s operation of the PPA AES or MELCO terminals on the SES—6 satellite. Sincerely, l_ /Klmtly M. Baum Vice President, Spectrum Managementand Development SES | 1129 20" Street NW, Suie 1000 | Washington, DC 20036 |USA | Tel:+1 202478 7100 Fax: +1 202 478 7101 | winses.com

SES-6 Emissions Designators for PPA (Aura LE) Max EIRP Density Per Carrier (dBW/4kHz) Max EIRP per Carrier (dBW) Satellite and Beam Name Emission Designator Bandwdith (Hz) Tx/Rx SES-6 AW Tx 500KG7D 500,000 40.00 19.82 SES-6 AW Tx 9M00G7D 9,000,000 48.00 15.27 SES-6 AW Rx 1M20G7D 1,200,000 SES-6 AW Rx 54M0G7D 54,000,000 SES-6 AE Tx 500KG7D 500,000 41.60 21.42 SES-6 AE Tx 9M00G7D 9,000,000 48.00 15.27 SES-6 AE Rx 1M20G7D 1,200,000 SES-6 AE Rx 54M0G7D 54,000,000 2-4

SES-6-AE MELCO Link Budget Forward Link Budget Return Link Budget eXConnect Terminal eXConnect Terminal Antenna Type MELCO Antenna Type MELCO Lat 69.7 deg Lat 69.7 deg Lon -39.4 deg Lon -39.4 deg EIRP max 47.2 dBW EIRP max 47.2 dBW G/T 9.3 dB/K G/T 9.3 dB/K Satellite Satellite Name SES-6-AE Name SES-6-AE Longitude -40.5 deg Longitude -40.5 deg Hub Earth Station Hub Earth Station Site Cologne Site Cologne Lat 50.863 deg Lat 50.863 deg Lon 6.848 deg Lon 6.848 deg EIRP max 75.5 dBW EIRP max 75.5 dBW G/T 35.0 dB/K G/T 35.0 dB/K Signal Signal Waveform DVB-S2 Waveform iDirect Modulation QPSK Modulation BPSK Bits per symbol 2 Bits per symbol 1 Spread Factor 1 Spread Factor 4 Coding Rate 0.50 Coding Rate 0.43 Overhead Rate 0.83 Overhead Rate 0.68 Channel Spacing 1.20 Channel Spacing 1.20 Spectral Efficiency (Rate/Noise BW) 0.83 bps/Hz Spectral Efficiency (Rate/Noise BW) 0.07 bps/Hz Data Rate 1.86E+07 bps Data Rate 4.86E+05 bps Information Rate (Data + Overhead) 2.25E+07 bps Information Rate (Data + Overhead) 7.19E+05 bps Symbol Rate 2.25E+07 Hz Symbol Rate 1.67E+06 Hz Chip Rate (Noise Bandwidth) 2.25E+07 Hz Chip Rate (Noise Bandwidth) 6.67E+06 Hz Occupied Bandwidth 2.70E+07 Hz Occupied Bandwidth 8.00E+06 Hz Power Equivelent Bandwidth 7.20E+07 Hz Power Equivelent Bandwidth 6.65E+05 Hz C/N Threshold 0.9 dB C/N Threshold -5.0 dB Uplink Uplink Frequency 14.250 GHz Frequency 14.250 GHz Back off 0.2 dB Back off 2.0 dB EIRP Spectral Density 37.8 dBW/4kHz EIRP Spectral Density 13.0 dBW/4kHz Slant Range 39858 km Slant Range 40395 km Space Loss, Ls 207.4 dB Space Loss, Ls 207.5 dB Pointing Loss, Lpnt 0.0 dB Pointing Loss, Lpnt 0.4 dB Atmosphere / Weather Loss, La 2.5 dB Atmosphere / Weather Loss, La 0.0 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB Transponder G/T @ Hub 1.0 dB/K Transponder G/T @ Terminal 1.0 dB/K Thermal Noise, C/No 95.1 dBHz Thermal Noise, C/No 67.0 dBHz C/(No+Io) 94.6 dBHz C/(No+Io) 66.5 dBHz Satellite Satellite Flux Density -90.2 dBW/m2 Flux Density -118.3 dBW/m2 SFD @ Hub -87.2 dBW/m2 SFD @ Terminal -87.2 dBW/m2 Small Signal Gain (IBO/OBO) 2.0 dB Small Signal Gain (IBO/OBO) 3.0 dB OBO 1.0 dB OBO 28.1 dB Downlink Downlink Frequency 12.000 GHz Frequency 12.000 GHz Transponder Sat. EIRP @ Beam Peak 49.2 dBW Transponder Sat. EIRP @ Beam Peak 49.2 dBW Transponder Sat. EIRP @ Terminal 48.0 dBW Transponder Sat. EIRP @ Hub 47.0 dBW DL PSD Limit 13.0 dBW/4kHz DL PSD Limit 13.0 dBW/4kHz DL PSD @ Beam Peak 10.7 dBW/4kHz DL PSD @ Beam Peak -11.2 dBW/4kHz Carrier EIRP @ Beam Peak 48.2 dBW Carrier EIRP @ Beam Peak 21.1 dBW Carrier EIRP @ Terminal 47.0 dBW Carrier EIRP @ Hub 18.9 dBW Slant Range 40395 km Slant Range 39858 km Space Loss, Ls 205.5 dB Space Loss, Ls 205.4 dB Pointing Loss, Lpnt 0.3 dB Pointing Loss, Lpnt 0.0 dB Atmosphere / Weather Loss, La 0.0 dB Atmosphere / Weather Loss, La 2.6 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB PCMA Loss 0.0 dB PCMA Loss 0.0 dB Thermal Noise, C/No 79.1 dBHz Thermal Noise, C/No 74.4 dBHz C/(No+Io) 77.1 dBHz C/(No+Io) 73.5499 dBHz End to End End to End End to End C/(No+Io) 77.1 dBHz End to End C/(No+Io) 65.7 dBHz Implementation Loss 1.5 dB Implementation Loss 0.0 dB End to End C/N w/ Imp Loss 2.0 dB End to End C/N w/ Imp Loss -2.6 dB Link Margin 1.1 dB Link Margin 2.4 dB

SES-6-AW MELCO Link Budget Forward Link Budget Return Link Budget eXConnect Terminal eXConnect Terminal Antenna Type MELCO Antenna Type MELCO Lat 74.4 deg Lat 74.4 deg Lon -71.9 deg Lon -71.9 deg EIRP max 47.2 dBW EIRP max 47.2 dBW G/T 9.3 dB/K G/T 9.3 dB/K Satellite Satellite Name SES-6-AW Name SES-6-AW Longitude -40.5 deg Longitude -40.5 deg Hub Earth Station Hub Earth Station Site Cologne Site Cologne Lat 50.86 deg Lat 50.86 deg Lon 6.848 deg Lon 6.848 deg EIRP max 75.5 dBW EIRP max 75.5 dBW G/T 35.0 dB/K G/T 35.0 dB/K Signal Signal Waveform DVB-S2 Waveform iDirect Modulation QPSK Modulation BPSK Bits per symbol 2 Bits per symbol 1 Spread Factor 1 Spread Factor 4 Coding Rate 0.40 Coding Rate 0.43 Overhead Rate 0.93 Overhead Rate 0.68 Channel Spacing 1.20 Channel Spacing 1.20 Spectral Efficiency (Rate/Noise BW) 0.74 bps/Hz Spectral Efficiency (Rate/Noise BW) 0.07 bps/Hz Data Rate 1.67E+07 bps Data Rate 4.86E+05 bps Information Rate (Data + Overhead) 1.80E+07 bps Information Rate (Data + Overhead) 7.18E+05 bps Symbol Rate 2.25E+07 Hz Symbol Rate 1.67E+06 Hz Chip Rate (Noise Bandwidth) 2.25E+07 Hz Chip Rate (Noise Bandwidth) 6.67E+06 Hz Occupied Bandwidth 2.70E+07 Hz Occupied Bandwidth 8.00E+06 Hz Power Equivelent Bandwidth 7.20E+07 Hz Power Equivelent Bandwidth 3.96E+05 Hz C/N Threshold 0.2 dB C/N Threshold -5.0 dB Uplink Uplink Frequency 14.250 GHz Frequency 14.250 GHz Back off 0.1 dB Back off 3.1 dB EIRP Spectral Density 37.9 dBW/4kHz EIRP Spectral Density 11.9 dBW/4kHz Slant Range 39858 km Slant Range 41170 km Space Loss, Ls 207.4 dB Space Loss, Ls 207.6 dB Pointing Loss, Lpnt 0.0 dB Pointing Loss, Lpnt 0.4 dB Atmosphere / Weather Loss, La 2.5 dB Atmosphere / Weather Loss, La 0.0 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB Transponder G/T @ Hub 0.0 dB/K Transponder G/T @ Terminal 0.0 dB/K Thermal Noise, C/No 94.2 dBHz Thermal Noise, C/No 64.7 dBHz C/(No+Io) 93.7 dBHz C/(No+Io) 64.2 dBHz Satellite Satellite Flux Density -90.1 dBW/m2 Flux Density -119.6 dBW/m2 SFD @ Hub -86.1 dBW/m2 SFD @ Terminal -86.2 dBW/m2 Small Signal Gain (IBO/OBO) 3.0 dB Small Signal Gain (IBO/OBO) 3.0 dB OBO 1.0 dB OBO 30.4 dB Downlink Downlink Frequency 12.000 GHz Frequency 12.000 GHz Transponder Sat. EIRP @ Beam Peak 48.1 dBW Transponder Sat. EIRP @ Beam Peak 47.0 dBW Transponder Sat. EIRP @ Terminal 47.0 dBW Transponder Sat. EIRP @ Hub 47.0 dBW DL PSD Limit 13.0 dBW/4kHz DL PSD Limit 13.0 dBW/4kHz DL PSD @ Beam Peak 9.6 dBW/4kHz DL PSD @ Beam Peak -15.6 dBW/4kHz Carrier EIRP @ Beam Peak 47.1 dBW Carrier EIRP @ Beam Peak 16.6 dBW Carrier EIRP @ Terminal 46.0 dBW Carrier EIRP @ Hub 16.6 dBW Slant Range 41170 km Slant Range 39858 km Space Loss, Ls 205.7 dB Space Loss, Ls 205.4 dB Pointing Loss, Lpnt 0.3 dB Pointing Loss, Lpnt 0.0 dB Atmosphere / Weather Loss, La 0.0 dB Atmosphere / Weather Loss, La 2.6 dB Radome, Lr 0.0 dB Radome, Lr 0.0 dB PCMA Loss 0.0 dB PCMA Loss 0.0 dB Thermal Noise, C/No 77.9 dBHz Thermal Noise, C/No 72.2 dBHz C/(No+Io) 76.0 dBHz C/(No+Io) 71.2930 dBHz End to End End to End End to End C/(No+Io) 75.9 dBHz End to End C/(No+Io) 63.4 dBHz Implementation Loss 1.5 dB Implementation Loss 0.0 dB End to End C/N w/ Imp Loss 0.9 dB End to End C/N w/ Imp Loss -4.8 dB Link Margin 0.7 dB Link Margin 0.2 dB

SES-6 Emissions Designators for MELCO Max EIRP Density Per Carrier (dBW/4kHz) Max EIRP per Carrier (dBW) Satellite and Beam Name Emission Designator Bandwdith (Hz) Tx/Rx SES-6 AW - MELCO Tx 500KG7D 500,000 32.10 11.92 SES-6 AW - MELCO Tx 9M00G7D 9,000,000 44.65 11.92 SES-6 AW - MELCO Rx 1M20G7D 1,200,000 SES-6 AW - MELCO Rx 54M0G7D 54,000,000 SES-6 AE - MELCO Tx 500KG7D 500,000 33.20 13.02 SES-6 AE - MELCO Tx 9M00G7D 9,000,000 45.75 13.02 SES-6 AE - MELCO Rx 1M20G7D 1,200,000 SES-6 AE - MELCO Rx 54M0G7D 54,000,000 2-7


Document Created: 2013-09-30 23:04:23
Document Modified: 2013-09-30 23:04:23
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