Narrative

1228-EX-ST-2019 Text Documents

Spire Global, Inc.

2019-07-03ELS_233318

    Spire LEMUR-2 Satellite Bus Experimental Special Temporary Authority Request

Spire Global, Inc. (“Spire”) requests experimental special temporary authority (“STA”) for one
(1) to-be-deployed Spire LEMUR-2 satellite bus (“LEMUR-2 Satellite”), which will host a
payload to be operated by KeyW Corporation (the “KeyW Payload”) onboard. Grant of the
LEMUR-2 Satellite STA request will allow KeyW to provide valuable demonstration and test
data to the United States Air Force in a timely manner.1

The Spire LEMUR-2 Satellite subject to the STA request will be launched in Q4 2019 from the
International Space Station (“ISS”). Given the necessary review and integration time frames,
Spire respectfully requests expedited consideration and grant of this STA request by August 31,
2019, or at the earliest practicable time thereafter.

Spire understands that it is possible that the operational lifetime of the experimental KeyW
Payload mission could extend up to one year. To the extent that valuable additional test data
may be available beyond the initial six-month experimental STA period requested herein, Spire
may seek a single, one-time renewal of the experimental STA consistent with the Commission’s
rules.

Description

Spire has received multiple Federal Communications Commission (“Commission”) Part 25
licenses to operate its own constellation of LEMUR-2 satellites on orbit.2 In its most recent Part
25 license application, Spire noted that:

         its new hosted payload service will provide added benefits to the quickly
         growing low-Earth orbit (“LEO”) market. Educational, government, and other
         commercial entities will have easier and quicker access to space as Spire will
         be deploying new satellites frequently. By utilizing Spire’s Phase II small
         satellite (“smallsat”) platform, these entities will also minimize the amount of




1
  A companion experimentation STA request to operate the KeyW Payload, including relevant supporting
materials regarding the nature and important public interest benefits of the proposed operations, will be
filed separately by KeyW.
2
  See Stamp Grant, Spire Global, Inc., File No. SAT-LOA-20151123-00078 (granted in part and deferred
in part Mar. 18, 2016, as corrected Mar. 24, 2016); Stamp Grant, Spire Global, Inc., File No. SAT-LOA-
20151123-00078 (granted in part and deferred in part June 16, 2016); Stamp Grant, Spire Global, Inc.,
File No. SAT-LOA-20151123-00078 (granted in part and deferred in part Oct. 14, 2016); Stamp Grant,
Spire Global, Inc., File No. SAT-AMD-20161114-00107 (granted in part and deferred in part Apr. 7,
2017); Stamp Grant, Spire Global, Inc., File No. SAT-AMD-20161114-00107 (granted in part and
deferred in part May 18, 2017); Stamp Grant, Spire Global, Inc., File No. SAT-AMD-20161114-00107
(granted in part and deferred in part July 13, 2017); Stamp Grant, Spire Global, Inc., File No. SAT-AMD-
20180102-00001 (granted in part and deferred in part Nov. 29, 2018).


            spacecraft deployed into LEO and the burden on NTIA and others in
            coordinating active radiofrequency links.3

Spire now requests experimental STA for one (1) to-be-deployed Spire LEMUR-2 Satellite,
which will host the KeyW Payload onboard.

The LEMUR-2 Satellite subject to this STA request will (i) receive commands and software
updates and (ii) downlink telemetry and data gathered by the KeyW Payload. Spire notes that
the LEMUR-2 Satellite will not contain its typical Automatic Identification System, Automatic
Dependent Surveillance-Broadcast, and Global Navigation Satellite System Radio Occultation
payloads. Instead, this LEMUR-2 Satellite will only contain the KeyW Payload and standard
LEMUR-2 Satellite radios and associated hardware. These radios and hardware have already
been approved for use by the Commission under the Spire Phase II License Grant.4

As noted, the LEMUR-2 Satellite (including the KeyW Payload) will be deployed from the ISS.
It will be deployed at the ISS altitude with an inclination of 51.6˚. Accordingly, the LEMUR-2
Satellite will operate within the parameters (385-650 km at any inclination) permissible under
the Spire Phase II License Grant,5 which similarly should be permissible in the context of this
experimental STA request.

As the Schedule S (list of frequencies and associated technical parameters), ODAR, and Orbital
Debris Mitigation Plan have been previously submitted, reviewed, and approved by the
Commission’s International Bureau, Spire hereby (i) incorporates these materials by reference in
the attached exhibits and (ii) requests an experimental STA grant for one (1) to-be-deployed
LEMUR-2 Satellite. To the extent the Commission requests other information in connection
with this experimental STA request, Spire will expeditiously supplement the record of this
proceeding.

Spire confirms that it will adhere to all Phase II License Grant conditions and applicable
coordination agreements with Federal/non-Federal operators in the bands, as well as additional
conditions that may be imposed in the context of this experimental STA request. At all times,
Spire will operate the LEMUR-2 Satellite on a non-interference basis vis-à-vis other authorized
radio systems and services. Accordingly, an expeditious grant of this STA request for the
LEMUR-2 Satellite is in the public interest and will quickly allow KeyW to provide valuable
data to the United States Air Force in a timely manner.


3
  Amendment Application of Spire Global, Inc., File No. SAT-AMD-20180102-00001, Exhibit A at 4-5
(filed Jan. 2, 2018) (“Phase II Amendment Application”).
4
    See Phase II License Grant.
5
  See id.; see also attached exhibits (Phase II Amendment Application exhibits). The KeyW Payload and
LEMUR-2 Satellite together will weigh approximately 5.6 kg, and the surface area will be no more than
the surface area dimensions for the Phase II LEMUR-2 satellite listed in the Orbital Debris Assessment
Report (“ODAR”). As a result, the LEMUR-2 Satellite and KeyW Payload meet all applicable orbital
dwell and collision risk thresholds.



Document Created: 0450-07-19 00:00:00
Document Modified: 0450-07-19 00:00:00

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