Exhibit 10.201


Exhibit 10.201


****CONFIDENTIAL PORTION has been omitted pursuant to a request for confidential treatment by the Company to, and the material has been separately filed with, the SEC.  Each omitted Confidential Portion is marked by four asterisks.




SEVENTEENTH AMENDMENT TO THE FULL-TIME-TRANSPONDER CAPACITY AGREEMENT (PRE-LAUNCH)




This Seventeenth Amendment to the Full-Time Transponder Capacity Agreement (Pre-Launch) (the “Seventeenth Amendment”) is made and entered into as of this 4th day of June, 2013 by and between INTELSAT CORPORATION, formerly known as PanAmSat Corporation, a Delaware corporation (“Intelsat”), and GCI COMMUNICATION CORP., an Alaskan corporation (“Customer”).


RECITALS


WHEREAS, pursuant to that certain Full-Time Transponder Capacity Agreement (Pre-Launch) dated as of March 31, 2006, as amended (collectively, the “Agreement”) between Intelsat and Customer, Intelsat is providing Customer with **** transponders **** Galaxy 18; **** transponders **** Horizons 1; and **** Transponder **** Horizon-1;


WHEREAS, Customer and Intelsat wish to amend the terms of the Agreement to **** Transponder Capacity by **** Transponder **** satellite. 


AGREEMENT


NOW, THEREFORE, in consideration of the foregoing and of mutual covenants and agreements hereinafter set forth, the sufficiency and receipt of which is hereby acknowledged, the parties agree as follows:


		
	1.
	Except as specifically provided herein, all terms and provisions of the Agreement shall remain in full force and effect.  




		
	2.
	Section 1.1, Description of Capacity.  This Section shall be deleted and replaced with the following:




Intelsat agrees to provide to Customer and Customer agrees to accept from Intelsat, ****), in ****, for the Capacity Term (as defined here), the **** Transponder Capacity (defined below) meeting the “Performance Specifications” set forth in the “Technical Appendix” attached hereto as Appendix B.  For purposes of this Agreement, the “**** Transponder Capacity” or “**** Transponders” shall consist of (a) **** (as defined in Section 1.2, below) **** transponders (collectively, the “**** Transponders’ and individually, the “**** Transponder”) from that certain U.S. domestic satellite referred to by Intelsat as “****,” located in geostationary orbit at **** Longitude, (b) **** transponders from the **** of that certain satellite referred to by Intelsat as “****” at **** Longitude (“**** Transponder”); (c) **** Transponder **** on ****; and (e) **** Transponder from that certain U.S. domestic satellite referred to by Intelsat as “****” located in geostationary orbit at **** Longitude (the “**** Transponder”).








****CONFIDENTIAL PORTION has been omitted pursuant to a request for confidential treatment by the Company to, and the material has been separately filed with, the SEC.  Each omitted Confidential Portion is marked by four asterisks.




A **** Transponder is a transponder **** to the **** Parties of **** Transponders **** of their **** Transponders.  **** Transponders shall be **** the **** Parties of the **** Transponders (or such **** Party’s ****) **** transponder **** agreement for such **** Transponders.  


The transponders on the Satellite and the beams in which these transponders are grouped are referred to as “Transponder(s)” and the “Beam(s),” respectively.  Galaxy 18, Galaxy 13 or Horizons 1 **** Customer **** hereunder, as applied in context herein, is referred to as the “Satellite.”  Intelsat shall **** the **** Transponder Capacity to ****, except as specifically permitted under this Agreement.  


		
	3.
	Capacity Term.  The Capacity Term for the **** Transponder shall **** and shall ****.  




		
	4.
	**** Fee.  The **** Fee for the **** Transponder shall **** US$**** Fee of US$****; however, such rate **** US$**** (**** Fee of US$****) effective **** in the event Customer **** with Intelsat **** transponders on the **** satellite to **** by ****.  




		
	5.
	 Except as specifically set forth in this Amendment, all terms and conditions of the Agreement remain in full force and effect.  




IN WITNESS WHEREOF, each of the parties hereto has duly executed and delivered this Seventeenth Amendment as of the day and year above written.




INTELSAT CORPORATION            GCI COMMUNICATION CORP.




By:     __/s/_____________________        By:  ___/s/_____________________
Name:    Patricia A. Casey___________        Name:  Jimmy Sipes_____________
		
	Title:
	SVP & Deputy General Counsel        Title:    VP Network Services & Chief Engineer












****CONFIDENTIAL PORTION has been omitted pursuant to a request for confidential treatment by the Company to, and the material has been separately filed with, the SEC.  Each omitted Confidential Portion is marked by four asterisks.






APPENDIX B-1 ****


TECHNICAL APPENDIX


	
		
	Satellite Information
	 

	Satellite:
	****

	Planned Orbital Location:
	**** Longitude

	Uplink  Beam/Band:
	**** / ****

	Downlink Beam/Band:
	**** / ****

	Nominal Transponder Bandwidth **** :
	****

	Customer's Transponder Capacity Allocation:
	****








1.0     INTRODUCTION.    This Technical  Appendix  contains the Performance  Specifications for the **** transponders assigned to the **** Uplink beam - **** Downlink beam.  As described further herein the specifications are **** transponder and **** as noted ****.




		
	2.0
	SATELLITE PERFORMANCE  CHARACTERISTICS


	
			
	Orbital Tolerances:
	Longitude Tolerance
	**** degrees

	Inclination Tolerance
	**** degrees








2.1    Communication  Antenna Pointing:    The  Satellite  will  maintain  the  orientation  of  its communications  antenna  relative  to the  earth  such that the EIRP,  G/T and  SFD described  in
. Section 3.1 are maintained.


	
	
	[The following “watermark” appears on each page of Appendix B-1: “March 30, 2006 Execution Copy” and has been removed to allow better clarity of the text of the appendix.]








Appendix B-1
**** Beam 
Technical Appendix







****CONFIDENTIAL TREATMENT






3.0    COMMUNICATION SYSTEM PERFORMANCE CHARACTERISTICS


3.1    EIRP, G/T and SFD Performance Specifications. PanAmSat specifies nominal **** transponder performance values for EIRP, G/T and SFD for selected cities within **** Uplink beam – **** Downlink beam of the Satellite as given below.


	
				
	Location
	EIRP dBW
[Notes 1, 2, 3, 5]
	G/T dB/K
[Notes 1, 3, 4, 5] 
	SFD dBW/m2
[Notes 1, 2, 3, 4, 5l

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****






Note (1):     Values apply **** transponder.
Note (2):          Values reflect **** transponder ****.
Note (3):      With **** section **** and ****  amplifier.
Note (4):      Values apply **** in the **** .
                    
Note (5):       All values are ****.


3.1.1   Estimated EIRP G/F and SFD in Locations Other Than Specified Cities.   In addition to 
 
the  values  indicated  above,  Figure  B-1  provides   EIRP  contours  for  the  Satellite  Downlink  Beams.  Figure B-2 provides G/T contours for the Satellite Uplink Beams. These contours permit the user to estimate EIRP and G/T for other locations within the overall footprint.  Estimated minimum beam center EIRP for the Transponders is ****.  Estimated minimum beam center G/T for the Transponders is ****. The SFD (****, and at the **** contour) is ****.




		
	Note:
	Beam center values are based on the specific beam patterns attached.  The contours are provided for estimation purposes only; the Performance Specification is based solely on the values for specific locations provided in Section 3.1.   It is recommended that a **** margin be included when utilizing the contours.




	
	
	[The following “watermark” appears on each page of Appendix B-1: “March 30, 2006 Execution Copy” and has been removed to allow better clarity of the text of the appendix.]














Appendix B-1
**** Beam 
Technical Appendix







****CONFIDENTIAL TREATMENT






Figure B-1.  ****








****


[Map of a region of the Earth with an overlay of numbred contour 


lines of spectific magnitudes in units of dBW.]






















**** Downlink Beam
(Contours  **** dBW)






































	
	
	[The following “watermark” appears on each page of Appendix B-1: “March 30, 2006 Execution Copy” and has been removed to allow better clarity of the text of the appendix.]




















Appendix B-1
**** Beam 
Technical Appendix







****CONFIDENTIAL TREATMENT






Figure B-2.  **** Uplink Beam












****


[Map of a region of the Earth with an overlay of numbred contour 


lines of spectific magnitudes in units of dB/K.]


























**** Uplink Beam
(Contours **** dB/K)














	
	
	[The following “watermark” appears on each page of Appendix B-1: “March 30, 2006 Execution Copy” and has been removed to allow better clarity of the text of the appendix.]


















Appendix B-1
**** Beam 
Technical Appendix







****CONFIDENTIAL TREATMENT






3.1.2    Saturation.  For the purposes of this Specification, saturation is defined as the point on the single carrier power-out versus power-in transfer curve corresponding to the operating point that provides the specified EIRP output power and simultaneously meets the required linearity. All values listed in Section 3.1 are at full transponder saturation.


3.1.3    Two Carrier and Multi-carrier Operation.  The values provided in Sections 3.1 and 3.1.1 are based on the occupancy of the Transponder by a single carrier.  For operation in dual carrier mode, the following input and output back-off requirements must be met:


	
			
	Mode
	Output
	Input(see Note 1)

	Two Carrier
	****
	****

	 
	****
	 






Note (1): **** is **** may be ****.




Accordingly, an 18 MHz dual carrier digital video operation must be conducted at a level determined by the following formula:


EIRPCARRIER = EIRPSAT - Output Back-off


While subject to final approval by PanAmSat based on the specific transponder configuration, in general multi-carrier operations (3 or more QPSK carriers) must be conducted with a composite output and input back-off meeting the following specifications:


	
			
	Mode
	Output
	Input(see Note 1
above)

	Multi Carrier
	****
	****






For shared use Transponders, additional power constraints may be imposed in order to reduce the generation of intermodulation of other spurious signals.






	
	
	[The following “watermark” appears on each page of Appendix B-1: “March 30, 2006 Execution Copy” and has been removed to allow better clarity of the text of the appendix.]










Appendix B-1
**** Beam
Technical Appendix







****CONFIDENTIAL TREATMENT




3.1.4    Input Attenuators.   The gain of each Transponder is adjustable by ground command over a range of **** in **** increments.  The gain setting for each Transponder can be chosen by the Customer and must take into consideration the need to limit co-channel and adjacent satellite interference.


		
	3.1.5
	SFD Gain Stability.  The SFD shall not vary by more than **** over any **** and **** the Satellite for the specified cities listed in Section 3.1, assuming the following:


		
	a)
	Including the **** the transponder.


		
	b)
	Exluding the ****.


		
	c)
	Excluding **** spacecraft **** errors.


		
	d)
	Including ****.




		
	3.1.6
	EIRP Change Due to Redundant Power Amplifier.  When any transponder is switched from its primary HPA to an adjacent HPA, the transponder output power shall not decrease by more than **** relative to the EIRP using the primary power amplifier.




		
	3.1.7
	Gain Change Due to First Redundant Receiver.  When the first redundant receiver is substituted for a primary receiver, the gain of the affected transponders shall not decrease by more than ****.




		
	3.2
	Satellite Communication System Expected Performance




3.2.1    Cross  Polarization.   Cross polarization  isolation between co-frequency Transponders  is expected to be a minimum of **** contour **** 


3.2.2    Nominal  Channel  Frequencies,  Polarization   and  Passband.      Each Transponder in the Beam shall have the Nominal Tansponder Bandwidth specified above using the frequencies and polarizations shown below. PanAmSat reserves the right to assign and/or reassign Customer's space segment allocation (and its other customer's space segment allocations) within the Transponder or to other Transponders within the applicable Uplink and/or Downlink Beam of the Satellite in order to minimize mutual interference between adjacent satellites, to  ensure compliance with applicable coordination agreements with other networks, and/or to permit efficient loading of the Satellite. Except in emergency circumstances, PanAmSat shall notify Customer of any changes to its initial allocation as soon as reasonably practicable prior to such change and shall use reasonable efforts to minimize disruption to Customer's Transponder Capacity during any such change.


	
	
	[The following “watermark” appears on each page of Appendix B-1: “March 30, 2006 Execution Copy” and has been removed to allow better clarity of the text of the appendix.]






Appendix B-1
**** Beam
Technical Appendix









6






****CONFIDENTIAL TREATMENT


                       SATELLITE/BEAM FREQUENCY PLAN


	
						
	****
	Bandwidth (MHz}
	Uplink Center Frequency (MHz)
	Uplink Polarization
	Downlink Center Frequency (MHz)
	Downlink Polarization

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****






		
	3.2.3
	Frequency Translation.  The communication system translates uplink transmissions by a net frequency subtraction of ****.  The net translation error is not expected to exceed ****.


		
	3.2.4
	In-Band Frequency Response. For carrier levels between single carrier saturation and **** below single carrier saturation, the output power of each transponder under single carrier operation conditions and excluding adjacent channel multipath effects, shall not vary by more than the following:




	
		
	Frequency  from 
Channel Center ( MHz)
	Maximum Transponder Output
Power Variation  Peak-to-Peak (dB)

	****
	****

	****
	****






Note: All values are nominal ****.
	
	
	[The following “watermark” appears on each page of Appendix B-1: “March 30, 2006 Execution Copy” and has been removed to allow better clarity of the text of the appendix.]














Appendix B-1
**** Beam
Technical Appendix

    




****CONFIDENTIAL TREATMENT


		
	3.2.5
	Total  Group  Delay.  The maximum total group delay in any Transponder relative to the value at channel center, excluding adjacent Transponder multipath delay, and  measured between the input to the receive antenna and the output of the transmit  antenna, shall be less than the values listed below. These requirements apply at flux densities between the SFD and **** below the SFD.




	
		
	Frequency from Channel Center< MHz)
	



Total Group Delay (ns)

	****
	****

	****
	****

	****
	****

	****
	****

	****
	****






Note : All values are nominal ****.




		
	3.2.6
	Transponder   Amplitude   Linearity.    In any Transponder the carrier to third order intermodulation ratio shall be equal to or greater than those values shown below for the primary channel amplifier. The input back-off shown is for each of two equal power carriers relative to single carrier saturation. A degradation **** shall be allowed at each output level for any channel other than the primary.




	
		
	Total Output Backoff                                Level Relative to Single       Carrier Saturation, dB
	Carrier/3rd Order Intermod

	****
	****

	****
	****

	****
	****

	****
	****

	****
	****






Note: All values are nominal ****.




End of Appendix B-1 ****




	
	
	[The following “watermark” appears on each page of Appendix B-1: “March 30, 2006 Execution Copy” and has been removed to allow better clarity of the text of the appendix.]






Appendix B-1
**** Beam
Technical Appendix



    




****CONFIDENTIAL TREATMENT




APPENDIX B-2 **** 


TECHNICAL APPENDIX


	
		
	Satellite Information
	 

	Satellite:
	****

	Planned Orbital Location:
	**** Longitude

	Uplink Beam/Band:
	**** / ****

	Downlink Beam/Band:
	**** / ****

	Nominal Transponder Bandwidth ****:
	****

	Customer's Transponder Capacity Allocation:
	****












1.0      INTRODUCTION.   This Technical Appendix  contains the Performance  Specifications for **** transponders assigned to **** Uplink beam - **** Downlink beam in a ****. As described further herein the specifications are **** transponder and **** as noted, ****.






		
	2.1
	SATELLITE PERFORMANCE CHARACTERISTICS




	
			
	



Orbital Tolerances:
	Longitude Tolerance:
	**** degrees

	Inclination Tolerance:
	**** degrees

	





****:
	Frequency:
	****

	EIRP:
	****

	Coverage:
	****






		
	2.2
	Communication  Antenna Pointing:    The Satellite will maintain the orientation of its communications antenna relative to the earth such that the EIRP, G/T and SFD described in Section 3.1 are maintained.















Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT




3.1    COMMUNICATION SYSTEM PERFORMANCE CHARACTERISTICS


		
	3.2
	EIRP,  G/T  and  SFD  Performance  Specifications.  PanAmSat specifies nominal **** transponder performance values for EIRP, G/T and SFD for selected cities within **** Uplink beam – **** Downlink beam of the satellite as given below. 




	
							
	



Location


	H
EIRP
dBW
[ Notes 1, 2, 3, 
5]
	V
EIRP
dBW
[ Notes 1, 2,
 3, 5]
	H
G/T
dB/K
[ Notes 1, 3, 
4, 5]
	V
G/T
dB/K
[ Notes 1, 3, 
4, 5]
	H
SFD
dBW/m2
[ Notes 1, 2,
 3, 4, 5]
	V
SFD
dBW/m2
[ Notes 1, 2,
 3, 4, 5]

	****
	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****
	****






Note (1):    Values apply **** transponder.
Note (2):    Values reflect **** transponder ****. 
Note (3):    With the **** section **** and **** amplifier.
Note (4):    Values apply **** in the ****.
Note (5):    All values are ****.




3.1.l    Estimated  EIRP.  G/T and  SFD in  Locations  Other  Than  Specified  Cities.  In addition to the  values indicated above, Figures  B-1 and  B-2 provide  EIRP contours for the Satellite Downlink Beams.  Figures B-3 and B-4 provide G/T contours for the Satellite Uplink Beams.  These contours permit the user to estimate EIRP and G/T for other locations within the overall footprint.   Estimated minimum beam center  EIRP for the Transponders is **** for **** and **** for  ****.  Estimated minimum  beam center G/T for the Transponders is **** for **** and **** for ****. The SFD (**** attenuation, and at the **** contour) is ****.




		
	Note :
	Beam center values are based on the specific beam patterns attached . The contours are provided for estimation purposes only; the Performance Specification is based solely on the values for specific locations provided in Section 3. 1.  It is recommended that **** margin be included when utilizing the contours.















Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT






Figure B-1.  **** Downlink ****L.








****




[Map of a region of the Earth with an overlay of numbred contour 


lines of spectific magnitudes in units of dBW.]




























**** Downlink Beam
(Contours **** dBW)



Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT






Figure B-2. **** Downlink ****L.








****


[Map of a region of the Earth with an overlay of numbred contour 


lines of spectific magnitudes in units of dBW.]










































**** Downlink
(Contours **** dBW)



Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT


Figure B-3. **** Uplink ****L.






****


[Map of a region of the Earth with an overlay of numbred contour 


lines of spectific magnitudes in units of dB/K.]




































**** Uplink Beam
(Contours **** dB/K.)



Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT




Figure B-4.  **** Uplink ****L.




****


[Map of a region of the Earth with an overlay of numbred contour 


lines of spectific magnitudes in units of dB/K.]
































**** Uplink Beam
(Contours **** dB/K)



Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT




3.1.2    Saturation.  For the purposes of this Specification, saturation is defined as the point on the single carrier power-out versus power-in transfer curve corresponding to the operating point that provides the specified EIRP output power and simultaneously meets the required linearity. All values listed in Section 3.1 are at full transponder saturation.


3.1.3    Two Carrier  and Multi-carrier Operation.  The values provided in Sections 3.1 and 3.1.1 are based on the occupancy of the Transponder by a single carrier. For operation in dual carrier mode, the following input and output back-off requirements must be met:


	
			
	Mode
	Output
	Input(see Note 1)

	Two Carrier
	****
	****

	 
	****
	 






Note (1):   **** is **** may be ****.


Accordingly, an 18 MHz dual carrier digital video operation must be conducted at a level determined by the following formula:


EIRPCARRIER = EIRPSAT - Output Back-off
While subject to final approval by PanAmSat based on the specific Transponder configuration, in general multi-carrier operations (3 or more QPSK carriers) must be conducted with a composite output and input back-off meeting the following specifications:


	
			
	Mode
	Output
	Input(see Note 1)

	Multi Carrier
	****
	****






For shared use Transponders, additional power constraints may be imposed in order to reduce the generation of intermodulation of other spurious signals.



Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT




3.1.4    Input Attenuators.   The gain of each Transponder is adjustable by ground command over a range of **** in **** increments.  The gain setting for each Transponder can be chosen by the Customer and must take into consideration the need to limit co-channel and adjacent satellite interference.


		
	3.1.5
	SFD Gain Stability.  The SFD shall not vary by more than **** over any **** and **** over the life of the Satellite for the specified cities listed in Section 3.1, assuming the following:


		
	a)
	Including the **** the transponder.


		
	b)
	Exluding the ****.


		
	c)
	Including **** spacecraft **** errors.


		
	d)
	Including ****.




		
	3.1.6
	EIRP Change Due to Redundant  Power Amplifier.  When any transponder is switched from its primary HPA to an adjacent HPA, the transponder output power, at the beginning of life and ambient temperature, shall not decrease by more than **** relative to the EIRP using the primary power amplifier.




		
	3.1.7
	SFD Change Due to First Redundant  Receiver.  When the first redundant receiver is substituted for a primary receiver, the SFD, at the beginning of life at ambient temperature, shall not decrease by more than ****.




		
	3.2
	Satellite Communication  System Expected  Performance




3.2.1    Cross Polarization. Cross polarization isolation between co-frequency Transponders is expected to be a minimum of **** contour ****.


3.2.2    Nominal  Channel  Frequencies,  Polarization  and  Passband.       Each    Transponder in the Beam shall have the Nominal Tansponder Bandwidth specified above using the frequencies and polarizations shown below. PanAmSat reserves the right to assign and/or reassign Customer's space segment allocation (and its other customer's space segment allocations) within the Transponder or to other Transponders within the applicable Uplink and/or Downlink Beam of the Satellite in order to minimize mutual interference between adjacent satellites, to ensure compliance with applicable coordination agreements with other networks, and/or to permit efficient loading of the Satellite. Except in emergency circumstances, PanAmSat shall notify Customer of any changes to its initial allocation as soon as reasonably practicable prior to such change and shall use reasonable efforts to minimize disruption to Customer's Transponder Capacity during any such change.  



Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT




SATELLITE/BEAM FREQUENCY PLAN




	
						
	****
	Bandwidth (MHz}
	Uplink Center Frequency (MHz)
	Uplink Polarization
	Downlink Center Frequency (MHz)
	Downlink Polarization

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****






		
	3.2.3
	Frequency Translation.  The communication system translates uplink transmissions by a net frequency subtraction of ****. The net translation error is not expected to ****.






		
	3.2.4
	In-Band Frequency Response. For carrier levels between single carrier saturation and **** below single carrier saturation, the output power of each transponder under single carrier operation conditions and excluding adjacent channel multipath effects, shall not vary by more than the following:




	
		
	Frequency from Channel Center ( MHz)
	Maximum Transponder Output Power Variation. Peak-to-Peak (dB)

	****
	****

	****
	****






Note: All values are nominal ****.

Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT




		
	3.2.5
	Total Group  Delay.   The maximum total group delay in any Transponder relative to the value at channel center, excluding adjacent Transponder multipath delay, and measured between the input to the receive antenna and the output of the transmit  antenna, shall be less than the values listed below. These requirements apply at flux densities between the SFD and **** below the SFD.




	
		
	Frequency from
Channel Center ( MHz)
	

Total Group Delay (ns)

	****
	****

	****
	****

	****
	****

	****
	****

	****
	****






Note : All values are nominal ****.






		
	3.2.6
	Transponder   Amplitude   Linearity.    In any Transponder the carrier to third order intermodulation ratio shall be equal to or greater than those values shown below for the primary channel amplifier. The input back-off shown is for each of two equal power carriers relative to single carrier saturation. A degradation of **** shall be allowed at each output level for any channel other than the primary.




	
		
	Total Output Backoff
Level for the sum relative relative 
to the output power at the single unmodulated carrier SFD, dB
	

Minimum Carrier/3rd Order 
Intermod, dB

	****
	****

	****
	****

	****
	****

	****
	****

	****
	****






Note : All values are nominal ****.


End of Appendix B-2



Appendix B-2
**** Beam
Technical Appendix 




****CONFIDENTIAL TREATMENT


APPENDIX B-3


TECHNICAL APPENDIX FOR ****


	
		
	Satellite Information
	 

	Satellite:
	****

	Orbital Location:
	****

	Uplink Beam/Band:
	**** / ****

	Downlink Beam/Band:
	**** / ****

	Nominal Transponder Bandwidth ****:
	****










1.0  INTRODUCTION.  This Technical Appendix contains the Performance Specifications for the **** transponders assigned to **** Satellites and **** Uplink beams – **** Downlink beams.  As described further herein the specifications are **** transponder and **** as noted, ****. 
The EIRP, G/T and SFD  performance specifications are shown in section 3.1 for the **** satellites designated for the ****.






2.0    SATELLITE PERFORMANCE CHARACTERISTICS


	
			
	

Orbital Tolerances:
	Longitude Tolerance:
	****

	Inclination Tolerance:
	  ****






2.1    Communication Antenna Pointing:  The Satellite will maintain the orientation of its communications antenna relative to the earth such that the EIRP, G/T and SFD described in Section 3.1 are maintained.







Appendix B-3
**** Beams 
Technical Appendix








****CONFIDENTIAL TREATMENT




		
	3.0
	COMMUNICATION SYSTEM PERFORMANCE CHARACTERISTICS




		
	3.1
	EIRP.  G/T  and  SFD  Performance  Specifications .  PanAmSat specifies nominal **** transponder performance values for EIRP, G/T and SFD for selected cities within **** Uplink beam – **** Downlink beam of the Satellite as given below.




**** SATELLITE ****


	
						
	Location
	EIRP
dBW
[ Notes 1, 2, 3, 5]
	(H)
G/T
dB/K
[Notes 1, 3, 4, 5]
	(V)
G/T
dB/K
[Notes 1, 3, 4, 5]
	(H)
SFD
dBW/
m2
[Notes 1, 2, 3, 4, 5]
	(V)
SFD
dBW/
m2
[Notes 1, 2, 3, 4, 5]

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****






**** SATELLITE ****


	
				
	Location
	EIRP
dBW
[ Notes 1, 2, 3, 5]
	G/T
dB/K
[Notes 1, 3, 4, 5]
	SFD
dBW/
m2
[Notes 1, 2, 3, 4, 5]

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****

	****
	****
	****
	****






Note (1):    Values apply **** transponder.
Note (2):    Values reflect **** transponder ****.
Note (3):    With the **** section **** and **** amplifier.
Note (4):    Values apply **** in the nominal **** (**** nominal).
Note (5):    All values are ****.
Note (6):    Values apply ****.

Appendix B-3
**** Beams 
Technical Appendix








****CONFIDENTIAL TREATMENT




3.1.1    Estimated  ****  Beam  ****   for   EIRP,   G/T   and   SFD   for   ****  Satellite ****.
Estimated **** beam **** EIRP for the Transponders is **** beam. Estimated **** beam **** G/T **** the transponders is **** SFD (**** G/T contour) is****..
3.1.2     Estimated  ****  Beam  ****   for   EIRP.   G/T   and   SFD   for   **** Satellite ****.
Estimated **** beam **** EIRP for the Transponders  is **** for  the  downlink beam.  Estimated **** beam **** G/T **** the transponders is **** (**** G/T contour) is ****.


Note:    It is recommended that a **** beam ****.






3.1.3    Saturation.  For the purposes of this Specification, saturation is defined as  the point on 
the single  carrier  power-out versus power-in transfer curve corresponding to the  operating point 
that provides the specified EIRP output power and simultaneously meets the required linearity.  
All values listed in Section 3.1 are at full transponder saturation.






		
	3.1.4
	Two Carrier and Multi-carrier Operation. The values provided in Sections 3.1 and 3.1.1


are based on the occupancy of the Transponder by a single carrier. For operation in dual carrier mode, the following input and output back-off requirements must be met:


	
			
	Mode
	Output Backoff (OBO)
	Input(see Note 1)

	Two Carrier
	****
	****

	Two Carrier
	****
	 






Note (1):  **** is ****. **** may be **** .


Accordingly, an 18 MHz dual carrier digital video operation must be conducted at a level determined by the following formula:


EIRPCARRIER = EIRPSAT - Output Back-off




While subject to final approval by PanAmSat based on the specific Transponder configuration, in general multi-carrier operations (3 or more QPSK carriers) must be conducted with a composite output and input back-off meeting the following specifications:

Appendix B-3
**** Beams 
Technical Appendix








****CONFIDENTIAL TREATMENT




	
			
	Mode
	Output Backoff (OBO)
	Input(see Note 1)

	Multi Carrier
	****
	****






For shared use Transponders, additional power constraints may be imposed in order to reduce the generation of intermodulation of other spurious signals.


3.1.5    Input Attenuators.   The  gain of each Transponder is adjustable by  ground  command over 
a minimum range of **** in **** increments.   The gain setting for each  Transponder can be chosen by the Customer and must take into consideration the need to limit co-channel and  
adjacent satellite interference.


		
	3.1.6
	SFD Gain Stability.  The SFD shall not vary by more than **** over any **** and **** Satellite for the specified cities listed in Section 3.1, assuming the following:


a)    Including the **** the transponder.
b)    Exluding the ****.
c)    Excluding **** spacecraft **** errors.


		
	3.1.7
	EIRP Change Due to Redundant Power Amplifier.  When any transponder is switched from its primary HPA to an adjacent HPA, the transponder output power shall not decrease by more than **** relative to the EIRP using the primary power amplifier.




		
	3.1.8
	Gain Change Due to First Redundant  Receiver.  When the first redundant receiver is substituted for a primary receiver, the gain of the affected transponders shall not decrease by more than ****.




3.2    Satellite Communication  System Expected  Performance


3.2.l    Cross Polarization. Cross polarization isolation between co-frequency Transponders is expected to be a minimum of **** contour ****.


3.2.2    Nominal   Channel  Frequencies.  Polarization   and  Passband.    Each Transponder in the Beam shall have the Nominal Tansponder Bandwidth specified above using the frequencies and polarizations shown below.  PanAmSat  reserves the right to assign and/or reassign Customer's space segment allocation (and its other customer's space segment allocations) within the Transponder or to other Transponders within the applicable Uplink and/or Downlink Beam of the Satellite in order to minimize mutual interference between adjacent satellites, to ensure compliance with applicable coordination agreements with other networks, and/or  to  permit efficient loading of the Satellite.  Except in emergency circumstances, PanAmSat shall notify Customer of any changes to its initial allocation as soon as reasonably practicable  prior to such

Appendix B-3
**** Beams 
Technical Appendix








****CONFIDENTIAL TREATMENT






change  and  shall  use  reasonable  efforts  to  minimize  disruption  to  Customer's  Transponder Capacity during any such change.






**** SATELLITE/BEAM FREQUENCY PLAN




	
						
	****
	Bandwidth (MHz)
	Uplink Center Frequency (MHz)
	Uplink Polarization
	Downlink Center Frequency (MHz)
	Downlink Polarization

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****













Appendix B-3
**** Beams 
Technical Appendix








                   ****CONFIDENTIAL TREATMENT




**** SATELLITE/BEAM FREQUENCY PLAN




	
						
	****
	Bandwidth (MHz)
	Uplink Center Frequency (MHz)
	Uplink Polarization
	Downlink Center Frequency (MHz)
	Downlink Polarization

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****

	****
	****
	****
	****
	****
	****








		
	3.2.3
	Frequency Translation . The communication system translates uplink transmissions by a net  frequency  subtraction  of ****.   The net translation  error is not expected to exceed ****.


		
	3.2.4
	In-Band  Frequency  Response .  For carrier levels between single carrier saturation and **** below single carrier saturation, the output power of each transponder  under  single carrier operation conditions and excluding adjacent channel multipath effects,  shall not vary by more than the following:




	
		
	Frequency from Channel Center ( MHz)
	Maximum Transponder  Output Power Variation   Peak-to-Peak (dB)

	****
	****






Note : All values are nominal ****.




		
	3.2.5
	Total  Group  Delay.  The maximum total group delay in any Transponder relative to the value at channel center, excluding adjacent Transponder multipath delay, and measured between the input to the receive antenna and the output of the transmit  antenna, shall be less than the values listed below.



Appendix B-3
**** Beams 
Technical Appendix








                        ****CONFIDENTIAL TREATMENT


	
		
	Frequency from
Channel Center (MHz)
	

Total Group Delay (ns)

	****
	****

	****
	****

	****
	****






Note:  All values are nominal ****.




		
	3.2.6
	Transponder   Amplitude   Linearity.    In any Transponder the carrier to third order intermodulation ratio shall be equal to or greater than those values shown below for the primary channel amplifier. The input back-off shown is for each of two equal power carriers relative to single carrier saturation. A degradation of **** shall be allowed at each output level for any channel other than the primary.




	
		
	Total Output Backoff Level Relative to Single Carrier Saturation  dB
	

Carrier/3rd Order Intermod

	****
	****

	****
	****

	****
	****






Note: All values are nominal ****.




End of Appendix B-3

Appendix B-3
**** Beams 
Technical Appendix