Attachment STA Narrative

This document pretains to SES-STA-20171026-01216 for Special Temporal Authority on a Satellite Earth Station filing.

IBFS_SESSTA2017102601216_1296509

                                       Before the
                         FEDERAL COMMUNICATIONS COMMISSION
                                  Washington, D.C. 20554



    In the Matter of                                       )
                                                           )
    SES Americom, Inc.                                     )     SES-STA-________-____
                                                           )     Call sign E170139
    Request for Special Temporary Authority to             )
    Conduct In-Orbit Testing with and Provide TT&C         )
    for SES-15 at 137° W.L.


                       REQUEST FOR SPECIAL TEMPORARY AUTHORITY

                  SES Americom, Inc. (“SES”) respectfully requests Special Temporary Authority

(“STA”) to use its E170139 earth station located in its South Mountain, California teleport 1 to

communicate with SES-15 at 137° W.L. in order to (1) perform in-orbit testing (“IOT”) of the

satellite’s Ku-band payload, (2) provide telemetry, tracking and command (TT&C) services for

the satellite while it is located at 137° W.L. and (3) provide TT&C during the satellite’s drift to

its final orbital location, 129.15° W.L. Authority is sought for a period of up to 30 days,

commencing on or around November 19, 2017. SES requests authority for the earth station to

communicate with the Gibraltar-licensed SES-15 satellite to test the Ku-band payload and

provide TT&C services.

                  SES Satellites (Gibraltar) Limited received market access to provide service into

the United States from 129.15° W.L. using the Ku- and Ka-bands as well as to operate the




1
 SES Americom, Inc., Call Sign E170139, File No. SES-LIC-20170726-00806, granted October
4, 2017.


WAAS payload in the L- and conventional and extended C-bands. 2 SES-15 was launched on

May 18, 2017 and is currently en route to its test orbital location at 137° W.L. SES-15 will be

located at 137° W.L. +/-0.1 degrees during IOT. The proposed stationkeeping volume will not

overlap with any other satellite. SES seeks earth station STA to perform testing of the SES-15

Ku-band payload using the following frequency bands:

    14.0-14.5 GHz                                 Uplink

    11.7-12.2 GHz                                 Downlink

    11.45-11.7 GHz                                Downlink

    11.2-11.45 GHz                                Downlink

    10.95-11.2 GHz                                Downlink

    10.7-10.95 GHz                                Downlink



SES also seeks earth station STA to provide TT&C while SES-15 is located at 137° W.L. and as

it drifts to 129.15° W.L. using the following frequencies:

    10700.5 MHz and 12199.5 MHz                   Telemetry

    13999 MHz, 3 14001 MHz and 14499 MHz          Command




2
  SES Satellites (Gibraltar) Limited, (Call Sign S2951), File No. SAT-MPL-20160718-00063,
granted Dec. 14, 2016; modifying File No. SAT-PPL-20160126-00007, granted July 12, 2016
(“SES-15 Grant”).
3
 SES Satellites (Gibraltar) Limited was granted a waiver of Section 25.202(g) to conduct
command operations using the 13999 MHz frequency. See id., Attachment to Grant at 3,
Condition 6.
                                                                                                  2


As discussed below, performing IOT while SES-15 is at 137° W.L. rather than at 129.15° W.L.

will permit testing to occur without disruption to existing customers at 129.15° W.L. and will not

adversely affect the operation of any adjacent satellites.

                  Grant of STA Will Serve the Public Interest. Grant of SES’s request to test the

Ku-band payload on SES-15 at 137° W.L. and provide TT&C for the satellite during testing and

drift is in the public interest. By testing SES-15 at this location, SES will minimize the risk of

interference to other satellites operating at the nominal 129° W.L. orbital location. Testing will

allow SES to ensure that the satellite’s communications payload is fully operational at the time it

arrives at its final orbital location, thereby avoiding any interruption in service that otherwise

might be associated with spacecraft testing. Additionally, STA to provide TT&C will ensure

safe satellite operations during the testing and drift operations.

                  No Harmful Interference to Other Spacecraft. Testing the SES-15 Ku-band

payload at 137° W.L. will not cause harmful interference to the operations of any other

spacecraft due to orbital angular separation, frequency diversity and/or geographically diverse

beam coverage. Except for SES’s AMC-4 spacecraft, there are no satellites within +/- 6 degrees

of 137° W.L. operating in the Ku-band. SES will manage the operations of its satellites to

prevent interference.

                  No Harmful Interference to Terrestrial Services. Transmissions associated with

IOT of SES-15 will not cause harmful interference to any terrestrial services in the extended Ku-

band. The satellite will operate within the power flux density limits set out in Section 25.208(b)

of the Commission’s rules, and the Commission has already granted a waiver authorizing the

satellite to provide domestic service in the extended Ku-bands based on its operational limits. 4



4
    Id. at 2, Condition 3.
                                                                                                     3


                Additionally, the earth station will not exceed the maximum output EIRP density

specified in its license, except in the case of certain tests involving high-powered continuous

wave (“CW”) for a short duration of time lasting from 30 minutes to several hours. A detailed

description of the proposed IOT activities and TT&C operations is provided in Attachment 1.

SES will conduct all IOT and TT&C operations on a non-harmful interference basis and will

cease transmissions promptly in the event SES receives a complaint of harmful interference

regarding its operations.

                Waiver Requests. SES seeks a waiver of footnote NG52 in order to conduct

domestic operations in the extended Ku-band downlink bands and SES seeks any necessary

waiver of Section 25.210(j) of the Commission’s rules in order to permit communications with

SES-15 at 137° W.L. with an east-west stationkeeping tolerance of +/- 0.1 degree during the IOT

operations. Grant of these waivers is consistent with Commission policy:

                        The Commission may waive a rule for good cause shown.
                        Waiver is appropriate if special circumstances warrant a
                        deviation from the general rule and such deviation would
                        better serve the public interest than would strict adherence
                        to the general rule. Generally, the Commission may grant a
                        waiver of its rules in a particular case if the relief requested
                        would not undermine the policy objective of the rule in
                        question and would otherwise serve the public interest. 5

                Section 2.106 Footnote NG52. SES seeks any necessary waiver of footnote

NG52 to permit the reception of U.S. domestic services in the 10.7-11.7 GHz band on an

unprotected, non-interference basis. The Commission has granted a waiver for SES-15 to

provide domestic service in these bands. 6 Footnote NG52 was intended to preserve access to the

10.7-11.7 GHz spectrum for terrestrial fixed service (“FS”) stations by limiting FSS use of the


5
    PanAmSat Licensee Corp., 17 FCC Rcd 10483, 10492 (Sat. Div. 2002) (footnotes omitted).
6
    SES-15 Grant, Attachment at 2, Condition 3.

                                                                                                  4


band to international operations only. 7 SES-15 will meet the power flux density limits on the

ground to protect FS operations, and the number of antennas that will be used to communicate in

these bands will be limited, thereby ensuring protection of FS services. Moreover, because SES

seeks authority to receive in this spectrum on an unprotected basis, FS use of the band will not be

constrained. Therefore, grant of the requested waiver will not undermine the purpose of the rule.

                Section 25.210(j): Section 25.210(j) specifies that geostationary space stations

“must be maintained within 0.05° of their assigned orbital location in the east/west direction,

unless specifically authorized by the Commission to operate with a different longitudinal

tolerance.” 8 Here, SES is seeking authority to communicate with SES-15 while the satellite is

maintained with a +/- 0.1 degree stationkeeping tolerance during the limited period of IOT

operations. The relaxed stationkeeping tolerance will minimize interruptions to the payload

testing operations due to stationkeeping maneuvers, which would delay the satellite’s on-station

start of operations. It will also conserve fuel for future satellite operations. Furthermore, the

SES-15 stationkeeping volume will not overlap with that of other satellites near 137° W.L. and

therefore there will be no adverse effect on the operations of other spacecraft.

                Protective Conditions. SES will coordinate its test and TT&C operations with all

potentially affected operating satellite networks and will operate only the Ku-band TT&C

payload of the SES-15 spacecraft during satellite drift. All testing will be conducted on an

unprotected, non-harmful interference basis, and SES operations will cease immediately upon

notification of harmful interference. 9


7
    See 47 C.F.R § 2.106, Footnote NG52. This policy was previously codified in footnote NG104.
8
    47 C.F.R. § 25.210(j).
9
 The 24/7 point of contact for SES during IOT and drift is Payload Management Operations
Center Level 1, +1 410 970 7570; +1 800 772 2363; pmocl1@ses.com.

                                                                                                    5


               SES hereby certifies that no party to this application is subject to a denial of

benefits pursuant to Section 5301 of the Anti-Drug Abuse Act of 1988, 21 U.S.C. § 862.

               For the foregoing reasons, SES respectfully requests special temporary authority

to operate its E170139 earth station to test the Ku-band payload on SES-15 at 137° W.L. and to

provide TT&C during IOT and drift for a period of up to 30 days commencing on or around

November 19, 2017. Grant of the requested authority will permit testing of the spacecraft

without affecting services to customers and will permit a seamless transition of services.

                                                   Respectfully submitted,
                                                   SES Americom, Inc.

                                                   By: /s/ Petra A. Vorwig

 Of Counsel                                        Petra A. Vorwig
 Karis A. Hastings                                 Senior Legal & Regulatory Counsel
 SatCom Law LLC                                    SES Americom, Inc.
 1317 F Street, N.W., Suite 400                    1129 20th Street N.W., Suite 1000
 Washington, D.C. 20004                            Washington, D.C. 20036
 Tel: (202) 599-0975


Dated: October 26, 2017




                                                                                                  6


                                         Attachment 1

Call Sign: E170139

Site Details
 Contact Information:                            Address:
 David Coyle                                     5990 Solano Verde Dr.
 805-386-2712                                    Somis, California 93066

 Geographic Coordinates:
 Latitude: 34 °19 ’32.3 "N                       Longitude: 118 °59 ’43.2 "W

 Site Elevation:
 313.0 meters

Antenna Details

Antenna ID:                         SM-K06
Manufacture/Model:                  GD Satcom/9.0M
Antenna Size:                       9.0 meters
Antenna Gain Transmit:              60.1 dBi at 14.125 GHz
Antenna Gain Receive:               58.5 dBi at 11.7250 GHz
Height Above Ground Level:          9.7 meters
Height Above Sea Level:             322.7 meters
Total Input Power at the Flange:    2000.0 watts
Total EIRP for the test Carrier:    93.1 dBW

TT&C Operational Details
 Frequency    Transmit         Polarization          Emission    Max EIRP      Max EIRP
 (MHz)        /Receive                               Designato   per           Density per
                                                     r           Carrier       Carrier
                                                                 (dBW)         (dBw/4kHz)
 10700.5           R           Horizontal and        500KF9D     0.0           0.0
                               Vertical Linear
 12199.5           R           Horizontal and        500KF9D     0.0           0.0
                               Vertical Linear
 13999             T           Horizontal and        1M00F9D     76.1          52.1
                               Vertical Linear
 14001             T           Horizontal and        1M00F9D     76.1          52.1
                               Vertical Linear
 14499             T           Horizontal and        1M00F9D     76.1          52.1
                               Vertical Linear


IOT Operational Details
 Frequency      Transmit   Polarization      Emission     Max EIRP   Max EIRP
 (MHz)          /Receive                     Designator   per        Density per
                                                          Carrier    Carrier
                                                          (dBW)      (dBw/4kHz)
10700-10950    R           Horizontal and    N0N          0.0        0.0
                           Vertical Linear
10950-11200    R           Horizontal and    N0N          0.0        0.0
                           Vertical Linear
11200-11450    R           Horizontal and    N0N          0.0        0.0
                           Vertical Linear
11450-11700    R           Horizontal and    N0N          0.0        0.0
                           Vertical Linear
11700-12200    R           Horizontal and    N0N          0.0        0.0
                           Vertical Linear
14000-14500    T           Horizontal and    N0N          81.5       81.5
                           Vertical Linear



Document Created: 2017-10-26 15:08:27
Document Modified: 2017-10-26 15:08:27

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