referring first to fig1 , a block diagram of an exemplary satellite communications system 100 configured according to various embodiments of the invention is shown . the satellite communications system 100 includes a network 120 , such as the internet , interfaced with one or more earth terminals 115 that is configured to communicate with one or more subscriber terminals 130 , via a satellite 105 . system 100 also includes one or more telemetry , tracking , and control ( ttc ) terminals 170 . the earth terminal 115 is sometimes referred to as a hub , gateway terminal , or ground station and services the uplink 135 , downlink 140 to and from the satellite 105 . although only one earth terminal 115 is shown , this embodiment has a number of earth terminals all coupled to the network 120 , for example , twenty or forty earth terminals . the earth terminal 115 schedules traffic to the subscriber terminals 130 , although other embodiments could perform scheduling in other parts of the satellite communication system 100 . a satellite communications system 100 applicable to various embodiments of the invention is broadly set forth herein . in this embodiment , there is a predetermined amount of frequency spectrum available for transmission . the communication links between the earth terminals 115 and the satellite 105 may use the same or overlapping frequency spectrums with the communication links between the satellite 105 and the subscriber terminals 130 or could use different frequency spectrums . the network 120 may be any type of network and can include , for example , the internet , an ip network , an intranet , a wide - area network ( wan ), a local - area network ( lan ), a virtual private network ( vpn ), a virtual lan ( vlan ), a fiber optical network , a hybrid fiber - coax network , a cable network , the public switched telephone network ( pstn ), the public switched data network ( psdn ), a public land mobile network , and / or any other type of network supporting data communication between devices described herein , in different embodiments . the network 120 may include both wired and wireless connections , including optical links . as illustrated in a number of embodiments , the network may connect the earth terminal 115 with other earth terminals ( not pictured ), which are also in communication with the satellite 105 . all earth terminals in communication with the satellite 105 may also connect with a command center 180 . the earth terminal 115 provides an interface between the network 120 and the satellite 105 . the earth terminal 115 may be configured to receive data and information directed to one or more subscriber terminals 130 , and can format the data and information for delivery to the respective destination device via the satellite 105 . similarly , the earth terminal 115 may be configured to receive signals from the satellite 105 ( e . g ., from one or more subscriber terminals 130 ) directed to a destination connected with the network 120 , and can format the received signals for transmission with the network 120 . the earth terminal 115 may use a broadcast signal , with a modulation and coding (“ modcode ”) format adapted for each packet to the link conditions of the terminal 130 or set of terminals 130 to which the packet is directed . the command center 180 connected to the network 120 may communicate with each earth terminal 115 in the network and the satellite 105 . earth terminals 115 may be generally located remote from the actual subscriber terminals 130 to enable frequency re - use . the earth terminal 115 may use an antenna 110 to transmit the uplink signal to the satellite 105 . in one embodiment , the antenna 110 comprises a parabolic reflector with high directivity in the direction of the satellite 105 and low directivity in other directions . the antenna 110 may comprise a variety of alternative configurations and include operating features such as high isolation between orthogonal polarizations , high efficiency in the operational frequency bands , and low noise . in one embodiment of the present invention , a geostationary satellite 105 is configured to receive the signals from the location of antenna 110 and within the frequency spectrum transmitted . the satellite 105 may , for example , use a reflector antenna , lens antenna , phased array antenna , active antenna , or other mechanism known in the art for reception of such signals . the signals received from the gateway 115 are amplified with a low - noise amplifier ( lna ) and then frequency converted for changing the power levels and frequencies . the satellite 105 may process the signals received from the gateway 115 and forward the signal from the gateway 115 to one or more subscriber terminals 130 . in one embodiment of the present invention , the frequency - converted signals are passed through a bank of filters that separate the various frequency - converted signals having different bandwidth . a switch may select one of the various frequency - converted signals , which is then further amplified by traveling wave tube amplifiers ( twta ) to produce the desired equivalent isotropically radiated power ( eirp ) at the payload antenna output . the high - power transmission signal passed through a transmit reflector antenna ( e . g ., a phased array antenna ) that forms the transmission radiation pattern ( spot beam ). in one embodiment of the present invention , the satellite 105 may operate in a multiple spot - beam mode , transmitting a number of narrow beams each directed at a different region of the earth , allowing for segregating subscriber terminals 130 into the various narrow beams . in another embodiment of the present invention , the satellite 105 may be configured as a “ bent pipe ” satellite , wherein the satellite 105 may frequency and polarization convert the received carrier signals before retransmitting these signals to their destination , but otherwise perform little on the contents of the signals . a spot beam may use a single carrier , i . e ., one frequency or a contiguous frequency range per beam . a variety of physical layer transmission modulation and coding techniques may be used by the satellite 105 in accordance with certain embodiments of the invention . adaptive coding and modulation can be used in some embodiments of the present invention . for other embodiments of the present invention , a number of network architectures consisting of space and ground segments may be used , in which the space segment is one or more satellites while the ground segment comprises of subscriber terminals , earth terminals or gateways , network operations centers ( nocs ) and a satellite and earth terminals command center . the earth terminals and the satellites can be connected via a mesh network or a star network , as evident to those skilled in the art . in one embodiment of the present invention , the command center 180 is connected to the network 120 and is operative to transmit instructions to the satellite and each participating earth terminal in the gso communication system . in another embodiment , the command center may be located at one geographical region and / or co - located with one of the earth terminals 115 . and yet in another embodiment , the command center may be distributed amongst multiple geographical regions and / or amongst several earth terminals . in yet another embodiment , the command center may be mobile and coupled to the network through a cellular link or a wireless metropolitan ( man ) or a wide area network ( wan ) link . the command center may be equipped with rf measurement equipment for measuring and evaluating interference characteristics . the downlink signals may be transmitted from the satellite 105 to one or more subscriber terminals 130 and received with the respective subscriber antenna 125 . in one embodiment , the antenna 125 and terminal 130 together comprise a very small aperture terminal ( vsat ), with the antenna 125 measuring approximately 0 . 6 meter in diameter and having approximately 2 watts of power . in other embodiments , a variety of other types of antennas 125 may be used at the subscriber terminal 130 to receive the signal from the satellite 105 . the link 150 from the satellite 105 to the subscriber terminals 130 may be referred to hereinafter as the forward downlink 150 . each of the subscriber terminals 130 may comprise a single user terminal or , alternatively , comprise a hub or router ( not pictured ) that is coupled to multiple user terminals . in one embodiment , subscriber terminal 130 may comprise a receiver including a bandpass filter bank adapted to let through a gso frequency spectrum and an extended frequency spectrum . each subscriber terminal 130 may be connected to various consumer premises equipment ( cpe ) 160 comprising , for example computers , local area networks , internet appliances , wireless networks , etc . ttc terminal 170 provides an interface for monitoring and controlling satellite 105 . for example , ttc terminal 170 may receive status information from satellite 105 , send commands to spacecraft 105 , and track the position of satellite 105 . in the present embodiment , ttc terminal 170 is connected to command center 180 via network 120 , and ttc terminal 170 is configured to receive commands from command center 180 and to send information , such as the status of satellite 105 , to command center 180 . ttc terminal 170 may be an independent terminal , as shown in the figure , or may alternatively be implemented in a terminal 115 that also carries traffic data . according to some alternative embodiments , ttc terminal 170 may be in direct communication with command center 180 or may be integrated into command center 180 . ttc terminal 170 communicates with satellite 105 using an antenna 175 . antenna 175 may be substantially similar to antenna 110 or may comprise a different configuration . uplink 195 represents a command uplink from ttc 115 for sending commands to satellite 105 . downlink 190 represents a telemetry downlink from satellite 105 for receiving data from satellite 105 , such as data representing the position of satellite 105 . ttc terminal 170 may be located remote from earth terminals 115 and subscriber terminals 130 . these links may be in - band with the user data links 135 and 140 , or alternatively use another set of frequencies . in parallel to the development of gso satellite communication systems , ngso satellite based systems have been developed and deployed . as ngso satellites travel in orbits below a gso satellite , there may be periods where one or more ngso satellites are “ in - line ” with the gso satellite and one or more of the gso earth terminals . fig2 is a block diagram illustrating ngso satellite 215 moving along a non - geostationary orbit 250 that crosses the channel between the antenna 110 of the earth terminal 115 and the satellite 105 . the uplink beam of the antenna 110 is a narrow beam as it is targeting the gso satellite 105 . ngso satellite 215 is in - line with respect to the earth terminal &# 39 ; s antenna 110 and the satellite 105 only a very short period of time when it travels the orbit 250 , which crosses the channel between the antenna 110 and the satellite 105 . interference may not occur in both uplink and downlink channels of the gso satellite 105 and ngso satellite 215 when the two satellites operate in different frequency spectrums . interference may not occur when ngso coverage area 235 is geographically apart from gso satellite coverage area 210 . interference may not occur when ngso ground stations use antennas 225 that are differently polarized than the earth terminal antenna 110 . in order to extend the period that ngso satellite 215 can illuminate ngso coverage area 235 , a spot beam of ngso satellite 215 may continuously be steered over the ngso coverage area 235 , and each ngso ground station within the ngso coverage area also tracks the serving ngso satellite as it moves across the ngso coverage area . to ensure continuous coverage of ngso area 235 , an ngso satellite constellation may have multiple ngso satellites so that at least one of the multiple ngso satellites will be visible at any time from the steerable antennas 225 of respective ngso ground stations . antennas 225 may be mechanically steerable or active phased - array ground terminal antennas . ngso satellites are generally designed to have variable transmitter power level so that a constant power flux density over each service area is achieved . for example , the transmitter power of a spot beam illuminating a certain ngso coverage area is reduced when the ngso satellite is traveling directly at or near the top ( e . g ., position a ) of the illuminated ngso coverage area , and the transmitter power will be increased when the ngso satellite moves away from the coverage area 225 . the transmitter power of ngso ground station antennas may also be increased to compensate for path loss when the ngso satellite moves away ( e . g ., position b ) from the ngso coverage area or when fading events occur ( e . g ., under rain or snow conditions ). the ngso satellite may interfere with the gso earth terminal 115 although its main antenna beam is pointed at the ngso coverage area 235 that is geographically apart from the gso earth terminal because its side antenna beams may be pointing at the antenna 110 . interference between the gso satellite and the ngso satellite can be mitigated when the gso and ngso satellites use different frequency spectrums . however , frequency spectrums available for satellite communications is very limited and there is a need for frequency spectrum sharing in order to use the available frequency spectrum more efficiently . the itu radio regulations have been updated to allow ngso systems to share parts of the ku - and ka - band spectrums with gso satellite systems . in one embodiment of the present invention , a gso satellite system exploits the fact that ngso satellites may be in - line or approximately in - line with respect to the gso satellite and one or more of the earth terminals only for a relative short time period due to the narrow antenna beam of the earth terminal pointing to the gso satellite so that the ngso frequency spectrum can be used in the gso satellite communication system for the time period where ngso satellites are not in in - line with respect to the earth terminal and the gso satellite . fig3 is a block diagram illustrating different interference scenarios between a gso satellite system and an ngso satellite that is in - line or approximately in - line with respect to the earth terminal and the gso satellite . in the following description , “ in - line ” means that the ngso satellite is positioned between the main beam of the earth terminal &# 39 ; s antenna 110 and the respective gso satellite ( as shown in fig3 ) or alternatively that the gso satellite is positioned between the ngso satellite and the ngso ground stations &# 39 ; antennas 225 . “ interference ” relates to frequency , phase , amplitude disturbance and / or any combination thereof caused by interaction between signals transmitted by the gso and ngso satellite systems . an example of the interference level or severity may be expressed by the carrier to interference power ratio ( c / i ). there are four interference scenarios : ( 1 ) the ngso satellite is interfering with a gso earth terminal ; ( 2 ) ngso ground stations are interfering with the gso satellite ; ( 3 ) gso earth terminals are interfering with the ngso satellite , and ( 4 ) the gso satellite is interfering with an ngso ground station . the worst case interference scenario ( 1 ) may occur when the ngso satellite is pointing its main antenna beam at an ngso terminal that is located closely to the gso earth terminal . interference scenario ( 1 ) may also occur when the main beam of the ngso satellite is pointing to an ngso ground station that is geographically apart from the gso earth terminals but the ngso satellite antenna side beams are pointing at the gso earth terminal . the worst case interference scenarios ( 2 ) and ( 4 ) may occur when the main beam of an ngso ground station is pointing at the gso satellite . and the worst case in interference scenario ( 3 ) may be when the main beam of the gso antenna is pointing at the ngso satellite . these four interference scenarios will be avoided or at least mitigated if the gso satellite system does not use the ngso frequency spectrum when an ngso satellite is in - line . the interference severity can be measured using rf equipment , estimated using known data , or simulated using known simulation models . the carrier - to - interference power ratio is for example a parameter for determining the interference level . the gso system must operate on a totally non - interference basis with the ngso system . this requires that when the ngso satellite is in - line or approximately in - line with respect to the earth terminal and the gso satellite , the gso earth terminal cannot transmit any signals towards the ngso satellite utilizing the ngso frequency spectrum since the transmitted signals would interfere with the desired ngso ground station uplink signals . ngso satellite systems can be low earth orbit ( leo ) satellite systems , medium earth orbit ( meo ) satellite systems , or high earth orbit ( heo ) satellite systems . the interference level and / or the in - line duration may depend on the antenna characteristics , receiver sensitivity of the ngso satellite in question , and its orbital altitude . according to some embodiments , if satellite 215 is a heo satellite , satellite 215 may be in an orbit that is sometimes higher than the orbit of satellite 215 . as a result , satellite 105 may pass between satellite 215 and antennas 225 of the ngso ground stations , which may result in satellite 105 interfering with communications between satellite 215 and the ngso ground stations if satellite 225 is using an extended frequency spectrum that includes the ngso frequency spectrum . when the gso and ngso satellites are not in - line , the ngso spectrum is said to be “ available ” for utilization by the gso satellite communication system . when the gso and ngso satellites are “ in - line ” or approximately “ in - line ”, the ngso spectrum is said to be “ unavailable ” for utilization by the gso system . in one embodiment of the present invention , the gso satellite design will incorporate at least two bandpass filters , which may be selected according to instructions received from a command center on earth . the selection of a bandpass filter having the appropriate bandwidth may be based on orbital ephemeris data that are maintained and updated by a gso network management system ( nms ). earth terminals that are participating in the gso satellite communication system may be capable of transmitting signals to the gso satellite using a gso frequency spectrum and an extended frequency spectrum . the extended spectrum includes the gso frequency spectrum and an ngso frequency spectrum . in another embodiment , the gso satellite design may incorporate a control device on board that contains orbital ephemeris data . the on - board control device may select the appropriate bandpass filter based on the stored orbital ephemeris data . this design alternative is feasible if all frequency spectrums and orbital information of the ngso system have been determined and remain unchanged during the life of the gso satellite . when the ngso spectrum is available , a bandpass filter with a bandwidth that passes the gso and ngso spectrums will be used . when the ngso spectrum is not available , a bandpass filter with a narrower bandwidth that only lets the gso spectrum through but attenuates the ngso spectrum sufficiently will be used . this will reduce all emissions by the satellite in the ngso band to a level that does not cause any downlink interference to the ngso system . in addition , when the ngso spectrum is unavailable , the earth terminals of the gso system will not use the ngso frequency spectrum to prevent any significant radiation and interference to the ngso satellites . during the short interval of ngso spectrum unavailability , the gso satellite communication system will operate in a reduced transmission capacity mode . in one embodiment , the gso satellite communication system uses its allocated gso frequency spectrum in a primary basis . the gso satellite communication system extends the allocated primary gso frequency spectrum with an ngso frequency spectrum in a secondary basis when the ngso satellite is not in - line , and the spectrum extension can be operated in a non - interfering manner . in one embodiment , both the gso and the ngso satellite communication systems operate in a ka - band . for example , the gso primary uplink frequency spectrum may be 28 . 1 to 28 . 6 ghz , and the gso primary downlink frequency spectrum may be 18 . 3 to 18 . 8 ghz . the ngso uplink frequency spectrum may be 28 . 6 to 29 . 1 ghz and the ngso downlink frequency spectrum may be 18 . 8 to 19 . 3 ghz . in order to manage the interference events , orbital ephemeris data must be carefully managed and updated by the gso network management system ( nms ). when an interference event is anticipated , the nms must have the capability to move all traffic to the gso spectrum and select the appropriate bandpass filter . from a frequency reuse standpoint , the ngso frequency spectrum would be an extension of the gso operating frequency spectrum . generally a satellite receives an uplink signal transmitted from an earth terminal at some frequency and converts it to a downlink signal at an offset transmit frequency . the downlink signal at the transmit frequency is then amplified for obtaining the downlink eirps . twta or solid state power amplifiers can be used . different uplink and downlink frequencies are used so that they do not interfere with each other . the satellite rf subsystem includes a receiver bandpass filter 410 adapted to pass the desired uplink signal , a low noise amplifier 420 adapted to amplify the filtered uplink signal 415 , a mixer 430 that down converts the uplink signal at frequency frx by mixing it with a local oscillator 440 , and a bandpass filter 450 that passes the desired frequency product 460 as shown in fig4 a . according to some embodiments , the satellite rf subsystem may include another filter ( not shown ) between the low noise amplifier 420 and mixer 430 . mixer 430 is a 3 - port device that takes the input signal 425 ( e . g ., the amplified uplink signal ) and the local oscillator signal 440 and frequency translates the uplink signal to a downlink signal . in most satellite communication , the downlink frequency signal is lower than the uplink frequency signal . if the signal level applied to the mixer is low , the mixed products may have two frequency products representing the sum ( f lo + f rx ) and the difference ( f lo − f rx ). if the signal level applied to the mixer is high , the resulting mixed products may have multiple harmonics consisting of every m * f rx ± n * f lo frequency product where m and n are integers . fig4 b is a block diagram illustrating the sum and difference products of an lo frequency of 9 . 0 ghz with a 2 . 0 ghz signal . the difference product is 7 . 0 ghz and the sum product is 11 . 0 ghz . fig4 c is a block diagram illustrating all of the possible sum and difference spectral products for m , n = 1 , 2 , and 3 . the difference product is 7 . 0 mhz and the sum product is 11 . 0 ghz for m = n = 1 . filter 450 is a bandpass filter that attenuates all of the undesired harmonics to a power level below the spectral emission requirements and let the desired frequency product pass through to the amplifiers ( not shown ). in one embodiment of the present invention , an exemplary design of the gso satellite system utilizing the additional ngso spectrum is shown in fig5 . the satellite rf receiver subsystem 500 comprises a receiver bandpass filter 510 that passes the composite gso / ngso uplink signal spectrum 515 and attenuates all other frequency components including the image of the uplink signal . the composite gso / ngso signal is then amplified by a low noise amplifier 520 and the amplified composite signal 525 is then applied to mixer 530 , where the signal 525 is mixed with local oscillator 540 to produce multiple frequency products including a desired gso downlink signal . according to some embodiments , the satellite rf subsystem may include another filter ( not shown ) between the low noise amplifier 520 and mixer 530 . mixer 530 may be a balanced mixer to cancel many mixer products due to the balance characteristics . the mixer may also be an image rejection mixer . lo 540 may be generated from an oven - controlled crystal oscillator ( ocxo ), which provides a very stable reference frequency . the multiple frequency products 545 are then divided into two paths 554 and 556 by power divider 550 . in one embodiment , both paths 554 and 556 have the same power level . in one embodiment , the filter response of bandpass filter 560 has a bandwidth that lets the desired gso downlink signal 570 through and the filter response of bandpass filter 562 has an extended bandwidth that lets the composite gso / ngso downlink signal 572 through . in one embodiment , bandpass filters 560 and 562 can be implemented with lumped l and c components , which provide wide bandwidth but moderate q . in another embodiment , bandpass filters can be implemented using microstrips for achieving high q . in yet another embodiment , bandpass filters can be implemented using high k ceramic materials for achieving even higher q . the frequency responses of bandpass filters 560 and 562 are different . in one embodiment , bandpass filter 560 passes the gso frequency spectrum but attenuates the ngso frequency spectrum whereas bandpass filter 562 passes both gso and ngso frequency spectrums and attenuates all other frequencies . the desired bandwidth of the downlink signal can then be selected by switch 580 . in one embodiment , switch 580 can be a pin diode single - pole double - throw ( spdt ) mmic switch . in one embodiment of the present invention , a control device 590 on - board the satellite is operative to demodulate the down - converted signal , extract relevant information from the demodulated signal , and decode instructions that are relevant for the operation of the receiver subsystem . the down - converted signal can be taken from the output 545 of the mixer 530 , from the output 570 of the gso bandpass filter 560 , or from the output 572 of the gso / ngso bandpass filter 562 and demodulated by demodulator 591 . one skilled in the art will recognize that the down - converted signal is not limited to only being taken from the output 545 , from the output 570 , or from the output 572 as illustrated in fig5 , and that the down - converted signal may be taken from other points in the receiver subsystem according to alternative embodiments of the present invention . decoded instructions are then applied to corresponding components of the receiver subsystem . in one embodiment , instructions may include the selection of the desired bandpass filter . according to other embodiments of the present invention , instructions from the command center may not be transmitted in band as described in fig6 . for example , instructions from the command center may be transmitted to satellite 105 via a separate telemetry link , such as uplink 195 illustrated in fig1 . where the command signals are not transmitted in band , additional hardware for processing signals carrying the instructions from the command center may be included in receiver subsystem 500 . since the gso satellite payload can dynamically operate over the ngso frequency spectrum , it provides the gso satellite communication system the capability to operate over spectrum that is otherwise not being used . in the case where the frequency spectrum has been allocated to the ngso satellite system but is not used , it provides the gso satellite communication system the capability to totally utilize that frequency spectrum . if and when that frequency spectrum is allocated and it is fully utilized by the ngso satellite system , the gso satellite system can be configured such that it will never operate over that frequency spectrum . because ngso satellites are typically closer to the earth &# 39 ; s surface than gso satellites , the necessary antenna size and transmission power level are often much smaller than those of gso satellites , and the footprints of the ngso satellites ( coverage areas ) are also much smaller than the gso satellite coverage areas . in one embodiment of the present invention , the gso satellite design may use the ngso band flexibly and efficiently when the ngso satellite system is operational but does not operate over a given coverage area that overlaps the gso coverage area . in this case , the frequency spectrum of the gso satellite system may be extended to include the ngso frequency spectrum . one of the primary factors of the ngso spectrum availability to the gso system is the directivity of both the gso and ngso systems . high antenna directivity results in narrow beam widths and confines transmitted and received spectral energy , the frequency of occurrences where the narrow beams are in - line is reduced . this is the case where spot - beam satellite systems are deployed . the satellite filter selectivity would be individually controllable for each narrow beam . for example , if a gso satellite system were operating over the continental united states with a number of small directional antennas and an ngso satellite was passing over the west coast , the east coast beams could continue to operate with the extended bandwidth that includes the ngso frequency band since they are well out of the ngso coverage area . in case where ngso satellite systems utilize omni - directional antennas , they will likely interfere more frequently with a gso satellite that utilizes the ngso band , and hence , the gso satellite can utilize the extended frequency band a much smaller fraction of time . fig6 is a block diagram illustrating a gso satellite communication system that uses an extended frequency spectrum in a non - interference manner , in accordance with one embodiment of the present invention . the gso earth terminal and the gso satellite may select the appropriate bandpass filter according to instructions received from the command center ( not shown ). gso frequency band 610 is the primary frequency spectrum allocated to the gso satellite communication system and ngso frequency band 620 is the primary frequency spectrum allocated to the ngso satellite communication system . when the ngso satellite 215 is in - line with respect to the gso earth terminal ( shown as antenna 110 ) and the gso satellite , the command center will instruct the gso earth terminal and the gso satellite 105 to use the gso spectrum only , the use of the gso spectrum is indicated by filter response 630 . when the ngso satellite 215 is not in - line with respect to the gso earth terminal and the gso satellite , the command center will instruct the gso earth terminal and the satellite to use the extended frequency spectrum , which includes the gso frequency spectrum 610 and ngso frequency spectrum 620 . the use of the extended frequency spectrum is indicated by filter response 640 . therefore , when the ngso satellite is not in - line , subscriber terminals ( shown as antennas 125 ) of the gso satellite communication system can benefit the higher channel capacity if they are capable of receiving the extended frequency spectrum . it will be understood that the position of the ngso band related to the gso band is for illustration only and is not meant to be limiting . in one embodiment ( shown in fig6 ), the ngso band is above the gso band . in other embodiment , the ngso band may be below the gso band as illustrated in fig8 b . in one embodiment , the satellite may include an on - board control device that may demodulate and decode instructions transmitted from the terrestrial command center . the control device then selects the bandpass filter having the appropriate bandwidth according to the decoded instructions . in another embodiment , the control device may operate autonomously with a control program stored in a memory to select the appropriate bandpass filter directly without the intervention of the command center . this scenario may be realizable when the orbital ephemeris data has been predetermined and no changes in the trajectory of the ngso satellite constellation and utilized frequency bands will be expected . since the orbital position locations of the ngso satellites relative to the earth and coverage areas are very predictable , the occurrence of the unavailability events are well known and relatively easy to determine by orbit monitoring equipment . orbit monitoring may be performed at the gso command center or at a site remote from the command center . in one embodiment , the gso command center may have the ability to directly provide control to the satellite as well as the ability to provide commands to every gso earth terminal connecting to the gso satellite communication system . in another embodiment , the command center may transmit instructions to the gso satellite through the use of a gso earth terminal participating in the gso communication network . fig7 illustrates an exemplary block diagram of a gso command center comprising a central processing unit 730 and a network control unit 740 . the central processing unit 730 may be coupled to memory 760 . interference statistics between the gso satellite link and the ngso satellite link can be performed by cpu 730 and the results may also be stored in the memory 760 . the memory 760 can be in the form of semiconductor storage such as random access memory ( static or dynamic ram ), magnetic storage such as hard discs , or other mass storage such as optical discs . cpu 730 is further coupled to an orbital ephemeris data acquisition unit 750 that collects ephemeris data of one or more ngso satellite constellations . ngso satellite constellations may include multiple satellites traveling in low earth orbit , medium earth orbit , and / or high earth orbit . cpu 730 may be used to compute the time period where the orbital trajectory of the ngso satellite constellation may cross the in - line path of the gso satellite and one of the earth terminals . the time period when a ngso satellite of the ngso constellation may be in - line with the gso channel with be stored in the memory 760 . the cpu 730 may further be connected to a satellite control unit 720 that may communicate with ttc terminal 170 to send commands to satellite 105 . the cpu 730 may further be connected to network control unit 740 that is operative to communicate with each of the earth terminals participating in the gso satellite communication system . network communication unit 740 may include a physical layer that supports a set of communication protocols such as point - to - point protocol ( ppp ), internet protocol ( ip ), the transmission control protocol ( tcp ), a wireless wide area network protocol , a mobile cellular network , and / or a combination of any communication protocols . in one embodiment of the present invention , right before the onset of an unavailability event , the command center performs the following actions : i ) the command center sends a command to the satellite instructing the satellite to utilize the gso bandwidth filter , i . e ., all emissions of the ngso band will be attenuated below a specified level , and ii ) the command center instructs all participating gso earth terminals to only transmit signal energy in the uplink gso uplink spectrum . immediately after the unavailability event , the command center performs the following actions : i ) the command center instructs the satellite to utilize the wider bandwidth filter that includes the gso channel and the ngso frequency band , and ii ) the command center instructs all participating gso earth terminals in the gso satellite system to transmit signal utilizing both the gso and ngso spectrum . in one embodiment of the invention , the selection between the allocated primary gso frequency spectrum and the extended frequency spectrum is performed by a switch . referring back to fig5 , switch 580 may be a pin diode single - pole double - throw ( spdt ) mmic switch . the desired spdt switching function can be achieved with a variety of different gaas pin diode configurations such as series diodes , shunt diodes , and / or a combination of series and shunt diodes . switch 580 may also be implemented with a series and a shunt capacitive micro - electro - mechanical systems ( mems ) switch . for example , commercially available high - power spdt switch vendors for ka - band are triquint semiconductor and endware , and an exemplary mems switch vendor is teravicta technologies . one skilled in the art will recognize that the implementation of switch 580 described herein merely illustrate one embodiment of switch 580 and that alternative constructions and equivalents may be used without departing from the spirit of the invention . in one embodiment of the present invention , both the gso and the ngso satellite systems utilize the ka - band . since the ka - band allocated frequency bands for gso and ngso satellite systems are adjacent to each other , extending the filter bandwidth to support the wider spectrum is very straightforward . in one embodiment , both the gso and the ngso satellite systems operate in a ka - band . in one embodiment , the gso primary channel frequency spectrum is 28 . 1 to 28 . 6 ghz , and the gso primary downlink channel frequency spectrum is 18 . 3 to 18 . 8 ghz . the ngso uplink channel frequency spectrum is 28 . 6 to 29 . 1 ghz and the ngso downlink channel frequency spectrum is 18 . 8 to 19 . 3 ghz . fig8 a illustrates the bandpass filter frequency response for the uplink and downlink channels of the gso satellite communication system using the extended frequency spectrum ( including the ngso frequency spectrum in addition to the gso frequency spectrum ). in this embodiment , the gso channel spectrum is below the ngso frequency spectrum , and the second bandpass filter 572 ( fig5 ) will have its bandwidth extended above the gso spectrum to include the ngso spectrum . in another embodiment , the gso primary uplink channel uses 29 . 5 to 30 . 0 ghz , and the gso primary downlink channel uses 19 . 7 to 20 . 2 ghz . the ngso uplink channel is 28 . 6 to 29 . 1 ghz and the ngso downlink channel is 18 . 8 to 19 . 3 ghz . fig8 b illustrates the bandpass filter frequency response for the uplink and downlink channels of the gso satellite communication system using the extended frequency spectrum . in this embodiment , the gso channel spectrum is above the ngso frequency spectrum , and the second band - pass filter 572 ( fig5 ) will have its bandwidth extended below the gso spectrum to include the ngso spectrum . the ngso frequency spectrum is in both cases in the proximate range of the gso frequency spectrum . it will be understood that the frequency spectrums for both gso and ngso satellite communication systems are for illustrative purpose only and are not meant to be limiting . in other embodiments , the gso and the ngso satellite communication systems may use the ku - band . specific details are given in the description to provide a thorough understanding of the embodiments . however , it will be understood by one of ordinary skill in the art that the embodiments may be practiced without these specific details . for example , well - known circuits , processes , algorithms , structures , and techniques have been shown without unnecessary detail in order to avoid obscuring the embodiments . also , it is noted that the embodiments may be described as a process that is depicted as a flow cart , a structure diagram , or a block diagram . although they may describe the operations as a sequential process , many of the operations can be performed in parallel or concurrently . in addition , the order of the operations may be re - arranged . furthermore , embodiments may be implemented by hardware , software , firmware , middleware , microcode , or any combination thereof . when implemented in software , firmware , middleware or microcode , the program code or code segments to perform the necessary tasks may be stored in a machine readable medium such as a storage medium . processors may perform the necessary tasks . having described several embodiments , it will be recognized by those skilled in the art that various modifications , alternative constructions , and equivalents may be used without departing from the spirit of the invention . for example , the above elements may merely be a component of a larger system , wherein other rules may take precedence over or otherwise modify the application of the invention . accordingly , the above description should not be taken as limiting the scope of the invention , which is defined in the following claims .