§  25.226   Blanket licensing provisions for domestic, U.S. Vehicle-Mounted
Earth Stations (VMESs) receiving in the 10.95-11.2 GHz (space-to-Earth),
11.45-11.7 GHz (space-to-Earth), and 11.7-12.2 GHz (space-to-Earth) frequency
bands and transmitting in the 14.0-14.5 GHz (Earth-to-space) frequency band,
operating with Geostationary Satellites in the Fixed-Satellite Service.

   (a) The following ongoing requirements govern all VMES licensees and
   operations in the 10.95-11.2 GHz (space-to-Earth), 11.45-11.7 GHz
   (space-to-Earth), 11.7-12.2 GHz (space-to-Earth) and 14.0-14.5 GHz
   (Earth-to-space) frequency bands receiving from and transmitting to
   geostationary orbit satellites in the fixed-satellite service. VMES
   licensees shall comply with the requirements in either paragraph
   (a)(1), (a)(2) or (a)(3) of this section and all of the requirements
   set forth in paragraphs (a)(4) through (a)(9) and paragraphs (c), (d),
   and (e) of this section. Paragraph (b) of this section identifies items
   that shall be included in the application for VMES operations to
   demonstrate that these ongoing requirements will be met.

   (1) The following requirements shall apply to a VMES that uses
   transmitters with off-axis EIRP spectral-densities lower than or equal
   to the levels in paragraph (a)(1)(i) of this section. A VMES, or VMES
   system, operating under this section shall provide a detailed
   demonstration as described in paragraph (b)(1) of this section. The
   VMES transmitter also shall comply with the antenna pointing and
   cessation of emission requirements in paragraphs (a)(1)(ii) and
   (a)(1)(iii) of this section.

   (i) A VMES system shall not exceed the off-axis EIRP spectral-density
   limits and conditions defined in paragraphs (a)(1)(i)(A) through (D) of
   this section.

   (A) The off-axis EIRP spectral-density emitted from the VMES, in the
   plane of the geostationary satellite orbit (GSO) as it appears at the
   particular earth station location, shall not exceed the following
   values:

   15-10log(N)-25logTH dBW/4kHz for 1.5DEG <= TH <= 7DEG

   -6 -10log(N) dBW/4kHz for 7DEG < TH <= 9.2DEG

   18 -10log(N)-25logTH dBW/4kHz for 9.2DEG < TH <= 48DEG

   -24 -10log(N) dBW/4kHz for 48DEG < TH <= 85DEG

   -14 -10log(N) dBW/4kHz for 85DEG < TH <= 180DEG

   where theta (TH) is the angle in degrees from the line connecting the
   focal point of the antenna to the orbital location of the target
   satellite, the plane of the GSO is determined by the focal point of the
   antenna and the line tangent to the arc of the GSO at the orbital
   location of the target satellite. For VMES networks using frequency
   division multiple access (FDMA) or time division multiple access (TDMA)
   techniques, N is equal to one. For VMES networks using multiple
   co-frequency transmitters that have the same EIRP, N is the maximum
   expected number of co-frequency simultaneously transmitting VMES earth
   stations in the same satellite receiving beam. For the purpose of this
   section, the peak EIRP of an individual sidelobe shall not exceed the
   envelope defined above for TH between 1.5DEG and 7.0DEG. For TH greater
   than 7.0DEG, the envelope shall be exceeded by no more than 10% of the
   sidelobes, provided no individual sidelobe exceeds the envelope given
   above by more than 3 dB.

   (B) In all directions other than along the GSO, the off-axis EIRP
   spectral-density for co-polarized signals emitted from the VMES shall
   not exceed the following values:

   18 -10log(N) -25logTH dBW/4kHz for 3.0DEG <= TH <= 48DEG

   -24 -10log(N) dBW/4kHz for 48DEG < TH <= 85DEG

   -14 -10log(N) dBW/4kHz for 85DEG < TH <= 180DEG

   where TH and N are defined in paragraph (a)(1)(i)(A) of this section.
   This off-axis EIRP spectral-density applies in any plane that includes
   the line connecting the focal point of the antenna to the orbital
   location of the target satellite with the exception of the plane of the
   GSO as defined in paragraph (a)(1)(i)(A) of this section. For the
   purpose of this subsection, the envelope shall be exceeded by no more
   than 10% of the sidelobes provided no individual sidelobe exceeds the
   gain envelope given above by more than 6 dB. The region of the main
   reflector spillover energy is to be interpreted as a single lobe and
   shall not exceed the envelope by more than 6 dB.

   (C) In all directions, the off-axis EIRP spectral-density for
   cross-polarized signals emitted from the VMES shall not exceed the
   following values:

   5 -10log(N) -25logTH dBW/4kHz for 1.8DEG <= TH <= 7.0DEG

   -16 -10log(N) dBW/4kHz for 7.0DEG < TH <= 9.2DEG

   where TH and N are defined as set forth in paragraph (a)(1)(i)(A) of
   this section. This EIRP spectral-density applies in any plane that
   includes the line connecting the focal point of the antenna to the
   target satellite.

   (D) For non-circular VMES antennas, the major axis of the antenna shall
   be aligned with the tangent to the arc of the GSO at the orbital
   location of the target satellite, to the extent required to meet the
   specified off-axis EIRP spectral-density criteria.

   (ii) Each VMES transmitter shall meet one of the following antenna
   pointing requirements:

   (A) Each VMES transmitter shall maintain a pointing error of less than
   or equal to 0.2DEG between the orbital location of the target satellite
   and the axis of the main lobe of the VMES antenna, or

   (B) Each VMES transmitter shall declare a maximum antenna pointing
   error that may be greater than 0.2DEG provided that the VMES does not
   exceed the off-axis EIRP spectral-density limits in paragraph (a)(1)(i)
   of this section, taking into account the antenna pointing error.

   (iii) Each VMES transmitter shall meet one of the following cessation
   of emission requirements:

   (A) For VMESs operating under paragraph (a)(1)(ii)(A) of this section,
   all emissions from the VMES shall automatically cease within 100
   milliseconds if the angle between the orbital location of the target
   satellite and the axis of the main lobe of the VMES antenna exceeds
   0.5DEG, and transmission shall not resume until such angle is less than
   or equal to 0.2DEG, or

   (B) For VMES transmitters operating under paragraph (a)(1)(ii)(B) of
   this section, all emissions from the VMES shall automatically cease
   within 100 milliseconds if the angle between the orbital location of
   the target satellite and the axis of the main lobe of the VMES antenna
   exceeds the declared maximum antenna pointing error and shall not
   resume transmissions until such angle is less than or equal to the
   declared maximum antenna pointing error.

   (2) The following requirements shall apply to a VMES that uses off-axis
   EIRP spectral-densities in excess of the levels in paragraph (a)(1)(i)
   of this section. A VMES, or VMES system, operating under this
   subsection shall file certifications and provide a detailed
   demonstration as described in paragraph (b)(2) of this section.

   (i) The VMES shall transmit only to the target satellite system(s)
   referred to in the certifications required by paragraph (b)(2) of this
   section.

   (ii) If a good faith agreement cannot be reached between the target
   satellite operator and the operator of a future satellite that is
   located within 6 degrees longitude of the target satellite, the VMES
   operator shall accept the power-density levels that would accommodate
   that adjacent satellite.

   (iii) The VMES shall operate in accordance with the off-axis EIRP
   spectral-densities that the VMES supplied to the target satellite
   operator in order to obtain the certifications listed in paragraph
   (b)(2) of this section. The VMES shall automatically cease emissions
   within 100 milliseconds if the VMES transmitter exceeds the off-axis
   EIRP spectral-densities supplied to the target satellite operator.

   (3) The following requirements shall apply to a VMES system that uses
   variable power-density control of individual simultaneously
   transmitting co-frequency VMES earth stations in the same satellite
   receiving beam. A VMES system operating under this subsection shall
   file certifications and provide a detailed demonstration as described
   in paragraph (b)(3) of this section.

   (i) Except as defined under paragraph (a)(3)(ii) of this section, the
   effective aggregate EIRP-density from all terminals shall be at least 1
   dB below the off-axis EIRP-density limits defined in paragraphs
   (a)(1)(i)(A) through (C) of this section. In this context the term
   "effective" means that the resultant co-polarized and cross-polarized
   EIRP-density experienced by any GSO or non-GSO satellite shall not
   exceed that produced by a single VMES transmitter operating 1 dB below
   the limits defined in paragraphs (a)(1)(i)(A) through (C) of this
   section. A VMES system operating under this section shall file
   certifications and provide a detailed demonstration as described in
   paragraphs (b)(3)(i) and (b)(3)(iii) of this section.

   (ii) The following requirements shall apply to a VMES that uses
   off-axis EIRP spectral-densities in excess of the levels in paragraph
   (a)(3)(i) of this section. A VMES system operating under this section
   shall file certifications and provide a detailed demonstration as
   described in paragraphs (b)(3)(ii) and (b)(3)(iii) of this section.

   (A) If a good faith agreement cannot be reached between the target
   satellite operator and the operator of a future satellite that is
   located within 6 degrees longitude of the target satellite, the VMES
   shall operate at an EIRP-density defined in paragraph (a)(3)(i) of this
   section.

   (B) The VMES shall operate in accordance with the off-axis EIRP
   spectral-densities that the VMES supplied to the target satellite
   operator in order to obtain the certifications listed in paragraph
   (b)(3)(ii) of this section. The individual VMES terminals shall
   automatically cease emissions within 100 milliseconds if the VMES
   transmitter exceeds the off-axis EIRP spectral-densities supplied to
   the target satellite operator. The overall system shall be capable of
   shutting off an individual transmitter or the entire system if the
   aggregate off-axis EIRP spectral-densities exceed those supplied to the
   target satellite operator.

   (C) The VMES shall transmit only to the target satellite system(s)
   referred to in the certifications required by paragraph (b)(3) of this
   section.

   (iii) The VMES shall file a report one year following license issuance
   detailing the effective aggregate EIRP-density levels resulting from
   its operation, in compliance with paragraph (b)(3)(iii) of this
   section.

   (4) An applicant filing to operate a VMES terminal or system and
   planning to use a contention protocol shall certify that its contention
   protocol use will be reasonable.

   (5) There shall be a point of contact in the United States, with phone
   number and address, available 24 hours a day, seven days a week, with
   authority and ability to cease all emissions from the VMESs.

   (6) For each VMES transmitter, a record of the vehicle location (i.e.,
   latitude/longitude), transmit frequency, channel bandwidth and
   satellite used shall be time annotated and maintained for a period of
   not less than one (1) year. Records shall be recorded at time intervals
   no greater than every five (5) minutes while the VMES is transmitting.
   The VMES operator shall make this data available upon request to a
   coordinator, fixed system operator, fixed-satellite system operator,
   NTIA, or the Commission within 24 hours of the request.

   (7) In the 10.95-11.2 GHz (space-to-Earth) and 11.45-11.7 GHz
   (space-to-Earth) frequency bands VMESs shall not claim protection from
   interference from any authorized terrestrial stations to which
   frequencies are either already assigned, or may be assigned in the
   future.

   (8) A VMES terminal receiving in the 10.95-11.2 GHz (space-to-Earth),
   11.45-11.7 GHz (space-to-Earth) and 11.7-12.2 GHz (space-to-Earth)
   bands shall receive protection from interference caused by space
   stations other than the target space station only to the degree to
   which harmful interference would not be expected to be caused to an
   earth station employing an antenna conforming to the referenced
   patterns defined in § 25.209(a) and (b) and stationary at the location
   at which any interference occurred.

   (9) Each VMES terminal shall automatically cease transmitting within
   100 milliseconds upon loss of reception of the satellite downlink
   signal.

   (b) Applications for VMES operation in the 14.0-14.5 GHz
   (Earth-to-space) band to GSO satellites in the fixed-satellite service
   shall include, in addition to the particulars of operation identified
   on Form 312, and associated Schedule B, the applicable technical
   demonstrations in paragraphs (b)(1), (b)(2) or (b)(3) of this section
   and the documentation identified in paragraphs (b)(4) through (b)(8) of
   this section.

   (1) A VMES applicant proposing to implement a transmitter under
   paragraph (a)(1) of this section shall demonstrate that the transmitter
   meets the off-axis EIRP spectral-density limits contained in paragraph
   (a)(1)(i) of this section. To provide this demonstration, the
   application shall include the tables described in paragraph (b)(1)(i)
   of this section or the certification described in paragraph (b)(1)(ii)
   of this section. The VMES applicant also shall provide the value N
   described in paragraph (a)(1)(i)(A) of this section. A VMES applicant
   proposing to implement a transmitter under paragraph (a)(1)(ii)(A) of
   this section shall provide the certifications identified in paragraph
   (b)(1)(iii) of this section. A VMES applicant proposing to implement a
   transmitter under paragraph (a)(1)(ii)(B) of this section shall provide
   the demonstrations identified in paragraph (b)(1)(iv) of this section.

   (i) Any VMES applicant filing an application pursuant to paragraph
   (a)(1) of this section shall file three tables showing the off-axis
   EIRP level of the proposed earth station antenna in the direction of
   the plane of the GSO; the co-polarized EIRP in the elevation plane,
   that is, the plane perpendicular to the plane of the GSO; and cross
   polarized EIRP. Each table shall provide the EIRP level at increments
   of 0.1DEG for angles between 0DEG and 10DEG off-axis, and at increments
   of 5DEG for angles between 10DEG and 180DEG off-axis.

   (A) For purposes of the off-axis EIRP table in the plane of the GSO,
   the off-axis angle is the angle in degrees from the line connecting the
   focal point of the antenna to the orbital location of the target
   satellite, and the plane of the GSO is determined by the focal point of
   the antenna and the line tangent to the arc of the GSO at the orbital
   position of the target satellite.

   (B) For purposes of the off-axis co-polarized EIRP table in the
   elevation plane, the off-axis angle is the angle in degrees from the
   line connecting the focal point of the antenna to the orbital location
   of the target satellite, and the elevation plane is defined as the
   plane perpendicular to the plane of the GSO defined in paragraph
   (b)(1)(i)(A) of this section.

   (C) For purposes of the cross-polarized EIRP table, the off-axis angle
   is the angle in degrees from the line connecting the focal point of the
   antenna to the orbital location of the target satellite and the plane
   of the GSO as defined in paragraph (b)(1)(i)(A) of this section will be
   used.

   (ii) A VMES applicant shall include a certification, in Schedule B,
   that the VMES antenna conforms to the gain pattern criteria of
   § 25.209(a) and (b), that, combined with the maximum input power
   density calculated from the EIRP density less the antenna gain, which
   is entered in Schedule B, demonstrates that the off-axis EIRP spectral
   density envelope set forth in paragraphs (a)(1)(i)(A) through
   (a)(1)(i)(C) of this section will be met under the assumption that the
   antenna is pointed at the target satellite.

   (iii) A VMES applicant proposing to implement a transmitter under
   paragraph (a)(1)(ii)(A) of this section shall provide a certification
   from the equipment manufacturer stating that the antenna tracking
   system will maintain a pointing error of less than or equal to 0.2DEG
   between the orbital location of the target satellite and the axis of
   the main lobe of the VMES antenna and that the antenna tracking system
   is capable of ceasing emissions within 100 milliseconds if the angle
   between the orbital location of the target satellite and the axis of
   the main lobe of the VMES antenna exceeds 0.5DEG.

   (iv) A VMES applicant proposing to implement a transmitter under
   paragraph (a)(1)(ii)(B) of this section shall:

   (A) Declare, in its application, a maximum antenna pointing error and
   demonstrate that the maximum antenna pointing error can be achieved
   without exceeding the off-axis EIRP spectral-density limits in
   paragraph (a)(1)(i) of this section; and

   (B) Demonstrate that the VMES transmitter can detect if the transmitter
   exceeds the declared maximum antenna pointing error and can cease
   transmission within 100 milliseconds if the angle between the orbital
   location of the target satellite and the axis of the main lobe of the
   VMES antenna exceeds the declared maximum antenna pointing error, and
   will not resume transmissions until the angle between the orbital
   location of the target satellite and the axis of the main lobe of the
   VMES antenna is less than or equal to the declared maximum antenna
   pointing error.

   (2) A VMES applicant proposing to implement a transmitter under
   paragraph (a)(2) of this section and using off-axis EIRP
   spectral-densities in excess of the levels in paragraph (a)(1)(i) of
   this section shall provide the following certifications and
   demonstration as exhibits to its earth station application:

   (i) A statement from the target satellite operator certifying that the
   proposed operation of the VMES has the potential to create harmful
   interference to satellite networks adjacent to the target satellite(s)
   that may be unacceptable.

   (ii) A statement from the target satellite operator certifying that the
   power density levels that the VMES applicant provided to the target
   satellite operator are consistent with the existing coordination
   agreements between its satellite(s) and the adjacent satellite systems
   within 6DEG of orbital separation from its satellite(s).

   (iii) A statement from the target satellite operator certifying that it
   will include the power-density levels of the VMES applicant in all
   future coordination agreements.

   (iv) A demonstration from the VMES operator that the VMES system is
   capable of detecting and automatically ceasing emissions within 100
   milliseconds when the transmitter exceeds the off-axis EIRP
   spectral-densities supplied to the target satellite operator.

   (3) A VMES applicant proposing to implement VMES system under paragraph
   (a)(3) of this section and using variable power-density control of
   individual simultaneously transmitting co-frequency VMES earth stations
   in the same satellite receiving beam shall provide the following
   certifications and demonstration as exhibits to its earth station
   application:

   (i) The applicant shall make a detailed showing of the measures it
   intends to employ to maintain the effective aggregate EIRP-density from
   all simultaneously transmitting co-frequency terminals operating with
   the same satellite transponder at least 1 dB below the EIRP-density
   limits defined in paragraphs (a)(1)(i)(A) through (C) of this section.
   In this context the term "effective" means that the resultant
   co-polarized and cross-polarized EIRP-density experienced by any GSO or
   non-GSO satellite shall not exceed that produced by a single VMES
   transmitter operating at 1 dB below the limits defined in paragraphs
   (a)(1)(i)(A) through (C) of this section. The International Bureau will
   place this showing on public notice along with the application.

   (ii) An applicant proposing to implement a VMES under paragraph
   (a)(3)(ii) of this section that uses off-axis EIRP spectral-densities
   in excess of the levels in paragraph (a)(3)(i) of this section shall
   provide the following certifications, demonstration and list of
   satellites as exhibits to its earth station application:

   (A) A detailed showing of the measures the applicant intends to employ
   to maintain the effective aggregate EIRP-density from all
   simultaneously transmitting co-frequency terminals operating with the
   same satellite transponder at the EIRP-density limits supplied to the
   target satellite operator. The International Bureau will place this
   showing on public notice along with the application.

   (B) A statement from the target satellite operator certifying that the
   proposed operation of the VMES has the potential to create harmful
   interference to satellite networks adjacent to the target satellite(s)
   that may be unacceptable.

   (C) A statement from the target satellite operator certifying that the
   aggregate power density levels that the VMES applicant provided to the
   target satellite operator are consistent with the existing coordination
   agreements between its satellite(s) and the adjacent satellite systems
   within 6DEG of orbital separation from its satellite(s).

   (D) A statement from the target satellite operator certifying that it
   will include the aggregate power-density levels of the VMES applicant
   in all future coordination agreements.

   (E) A demonstration from the VMES operator that the VMES system is
   capable of detecting and automatically ceasing emissions within 100
   milliseconds when an individual transmitter exceeds the off-axis EIRP
   spectral-densities supplied to the target satellite operator and that
   the overall system is capable of shutting off an individual transmitter
   or the entire system if the aggregate off-axis EIRP spectral-densities
   exceed those supplied to the target satellite operator.

   (F) An identification of the specific satellite or satellites with
   which the VMES system will operate.

   (iii) The applicant shall acknowledge that it will maintain sufficient
   statistical and technical information on the individual terminals and
   overall system operation to file a detailed report, one year after
   license issuance, describing the effective aggregate EIRP-density
   levels resulting from the operation of the VMES system.

   (4) There shall be an exhibit included with the application describing
   the geographic area(s) in which the VMESs will operate.

   (5) Any VMES applicant filing for a VMES terminal or system and
   planning to use a contention protocol shall include in its application
   a certification that will comply with the requirements of paragraph
   (a)(4) of this section.

   (6) The point of contact referred to in paragraph (a)(5) of this
   section shall be included in the application.

   (7) Any VMES applicant filing for a VMES terminal or system shall
   include in its application a certification that will comply with the
   requirements of paragraph (a)(6) of this section.

   (8) All VMES applicants shall submit a radio frequency hazard analysis
   determining via calculation, simulation, or field measurement whether
   VMES terminals, or classes of terminals, will produce power densities
   that will exceed the Commission's radio frequency exposure criteria.
   VMES applicants with VMES terminals that will exceed the guidelines in
   § 1.1310 of this chapter for radio frequency radiation exposure shall
   provide, with their environmental assessment, a plan for mitigation of
   radiation exposure to the extent required to meet those guidelines. All
   VMES licensees shall ensure installation of VMES terminals on vehicles
   by qualified installers who have an understanding of the antenna's
   radiation environment and the measures best suited to maximize
   protection of the general public and persons operating the vehicle and
   equipment. A VMES terminal exhibiting radiation exposure levels
   exceeding 1.0 mW/cm^2 in accessible areas, such as at the exterior
   surface of the radome, shall have a label attached to the surface of
   the terminal warning about the radiation hazard and shall include
   thereon a diagram showing the regions around the terminal where the
   radiation levels could exceed 1.0 mW/cm^2 . All VMES licensees shall
   ensure that a VMES terminal ceases transmission upon encountering an
   obstruction that degrades the VMES downlink signal.

   (c)(1) Operations of VMESs in the 14.0-14.2 GHz (Earth-to-space)
   frequency band within 125 km of the NASA TDRSS facilities on Guam
   (latitude 13DEG36'55" N, longitude 144DEG51'22" E) or White Sands, New
   Mexico (latitude 32DEG20'59" N, longitude 106DEG36'31" W and latitude
   32DEG32'40" N, longitude 106DEG36'48" W) are subject to coordination
   with the National Aeronautics and Space Administration (NASA) through
   the National Telecommunications and Information Administration (NTIA)
   Interdepartment Radio Advisory Committee (IRAC). Licensees shall notify
   the International Bureau once they have completed coordination. Upon
   receipt of such notification from a licensee, the International Bureau
   will issue a public notice stating that the licensee may commence
   operations within the coordination zone in 30 days if no party has
   opposed the operations.

   (2) When NTIA seeks to provide similar protection to future TDRSS sites
   that have been coordinated through the IRAC Frequency Assignment
   Subcommittee process, NTIA will notify the Commission's International
   Bureau that the site is nearing operational status. Upon public notice
   from the International Bureau, all Ku-band VMES licensees shall cease
   operations in the 14.0-14.2 GHz band within 125 km of the new TDRSS
   site until the licensees complete coordination with NTIA/IRAC for the
   new TDRSS facility. Licensees shall notify the International Bureau
   once they have completed coordination for the new TDRSS site. Upon
   receipt of such notification from a licensee, the International Bureau
   will issue a public notice stating that the licensee may commence
   operations within the coordination zone in 30 days if no party has
   opposed the operations. The VMES licensee then will be permitted to
   commence operations in the 14.0-14.2 GHz band within 125 km of the new
   TDRSS site, subject to any operational constraints developed in the
   coordination process.

   (d)(1) Operations of VMESs in the 14.47-14.5 GHz (Earth-to-space)
   frequency band in the vicinity of radio astronomy service (RAS)
   observatories observing in the 14.47-14.5 GHz band are subject to
   coordination with the National Science Foundation (NSF). The
   appropriate NSF contact point to initiate coordination is
   Electromagnetic Spectrum Manager, NSF, 4201 Wilson Blvd., Suite 1045,
   Arlington VA 22203, fax 703-292-9034, e-mail esm@nsf.gov . Licensees
   shall notify the International Bureau once they have completed
   coordination. Upon receipt of the coordination agreement from a
   licensee, the International Bureau will issue a public notice stating
   that the licensee may commence operations within the coordination zone
   in 30 days if no party has opposed the operations.

   (2) Table 1 provides a list of each applicable RAS site, its location,
   and the applicable coordination zone.

   Table 1--Applicable Radio Astronomy Service (RAS) Facilities and
   Associated Coordination Distances
   Observatory Latitude (north) Longitude (west) Radius (km) of
   coordination zone
   Arecibo, Observatory, Arecibo, PR 18DEG20'37" 66DEG45'11" Island of
   Puerto Rico.
   Green Bank, WV 38DEG25'59" 79DEG50'23" 160.
   Very Large Array, near Socorro, NM 34DEG04'44" 107DEG37'06" 160.
   Pisgah Astronomical Research Institute, Rosman, NC 35DEG11'59"
   82DEG52'19" 160.
   U of Michigan Radio Astronomy Observatory, Stinchfield Woods, MI
   42DEG23'56" 83DEG56'11" 160.
   Very Long Baseline Array (VLBA) stations:
   Owens Valley, CA 37DEG13'54" 118DEG16'37" 160*.
   Mauna Kea, HI 19DEG48'05" 155DEG27'20" 50.
   Brewster, WA 48DEG07'52" 119DEG41'00"
   Kitt Peak, AZ 31DEG57'23" 111DEG36'45"
   Pie Town, NM 34DEG18'04" 108DEG07'09"
   Los Alamos, NM 35DEG46'30" 106DEG14'44"
   Fort Davis, TX 30DEG38'06" 103DEG56'41"
   North Liberty, IA 41DEG46'17" 91DEG34'27"
   Hancock, NH 42DEG56'01" 71DEG59'12"
   St. Croix, VI 17DEG45'24" 64DEG35'01"

   *Owens Valley, CA operates both a VLBA station and single-dish
   telescopes.

   (3) When NTIA seeks to provide similar protection to future RAS sites
   that have been coordinated through the IRAC Frequency Assignment
   Subcommittee process, NTIA will notify the Commission's International
   Bureau that the site is nearing operational status. Upon public notice
   from the International Bureau, all Ku-band VMES licensees shall cease
   operations in the 14.47-14.5 GHz band within the relevant geographic
   zone (160 kms for single-dish radio observatories and Very Large Array
   antenna systems and 50 kms for Very Long Baseline Array antenna
   systems) of the new RAS site until the licensees complete coordination
   for the new RAS facility. Licensees shall notify the International
   Bureau once they have completed coordination for the new RAS site and
   shall submit the coordination agreement to the Commission. Upon receipt
   of such notification from a licensee, the International Bureau will
   issue a public notice stating that the licensee may commence operations
   within the coordination zone in 30 days if no party opposed the
   operations. The VMES licensee then will be permitted to commence
   operations in the 14.47-14.5 GHz band within the relevant coordination
   distance around the new RAS site, subject to any operational
   constraints developed in the coordination process.

   (e) VMES licensees shall use Global Positioning Satellite-related or
   other similar position location technology to ensure compliance with
   paragraphs (c) and (d) of this section.

   [ 74 FR 57099 , Nov. 4, 2009]