Ex Parte Notice_25Au

Ex PARTE PRESENTATION NOTIFICATION LETTER submitted by ORBCOMM License Corp.

Ex Parte Letter

2016-08-29

This document pretains to SAT-STA-20150821-00060 for Special Temporal Authority on a Satellite Space Stations filing.

IBFS_SATSTA2015082100060_1147792

                                                                                          Exhibit A
                                                                                   Spire Global, Inc.
                                                                             Response to Question 43
                                                                                     FCC Form 312

                                    Description of Application

       Spire Global, Inc. (“Spire”) requests authority to launch and operate a constellation of

low-earth orbit, non-geostationary orbit (“NGSO”) cubesats to provide maritime monitoring,

meteorological monitoring, and earth imaging services.1 As detailed in this narrative description

(“Narrative”), the Spire satellite system, i.e. the LEMUR constellation, will be constructed in two

phases. Phase I will employ 29 technically identical2 cubesats operating at a number of different

orbital altitudes and inclinations (the LEMUR-2 constellation). These satellites will use the

2020-2025 MHz band for downlink3 and the 402-403 MHz band for uplink and telemetry,

tracking, and command (“TT&C”).4 Phase II will employ up to 175 technically identical

satellites, operating at orbital altitudes from 400 to 650 km and inclinations ranging from

equatorial to polar sun-synchronous (98 degrees) (the LEMUR-3 constellation).5 These cubesats

will use the 8025-8400 MHz band for downlink, including TT&C, and the 2025-2110 MHz band




1
 Cubesats are also referred to as nanosatellites, small satellites, small sats, or picosats,
depending on context.
2
 The satellites have the same relevant radiofrequency characteristics (e.g., transmit power, out-
of-band emissions, antenna patterns and gain, and transmit and receive frequencies).
3
 The Phase I satellites will also use the 402-403 MHz band for backup downlink. See
Frequency Bands, Exhibit B (identifying the proposed frequency bands to be used on the
LEMUR constellations); see also infra Part II.A.4 (discussing the frequency bands used by the
LEMUR constellations).
4
 As discussed below, Spire already has received experimental authority for the launch and
operation for several of the 29 Phase I satellites and is not seeking further authorization with
respect to those previously authorized satellites or any subsequent Phase I satellite for which
Spire receives experimental authorization.
5
 Spire expects the constellation, at any point in time, to be comprised of approximately 125
satellites.


                                                                                        Exhibit A
                                                                                 Spire Global, Inc.
                                                                           Response to Question 43
                                                                                   FCC Form 312

for uplink, including TT&C. 6 Both the Phase I and Phase II satellites also will have equipment

capable of receiving two Automatic Identification System (“AIS”) signals, AIS 1 (161.9625-

161.9875 MHz) and AIS 2 (162.0125-162.0375 MHz),7 and also the Global Positioning System

(“GPS”) L1 signal (centered at 1575.42 MHz) and the L2 signal (centered at 1227.60 MHz).

        Spire also requests launch authority for a total of up to 900 satellites to be deployed over

the 15-year term of the requested satellite license. This authority will cover both the Phase I

satellites (that have not been granted experimental authorizations as of the date of the grant of

this application) and the Phase II satellites. Spire would have no more than 175 satellites

operational at any given time and would only launch additional satellites, as necessary, to

replenish its on-orbit fleet.

        In support of its request for authorization, Spire provides the following information

concerning its proposed satellite system.

I.      Description of the Applicant

        Spire, which was formerly known as NanoSatisfi, Inc. and formed in Delaware in August

2012, is a private U.S. company headquartered in San Francisco, California, with offices in

Glasgow and Singapore. The enterprise grew out of a volunteer effort by four graduate students


6
  The Phase II satellites will also use the 2020-2025 MHz band for backup downlink band and
the 402-403 MHz band for backup uplink and downlink, including for backup TT&C. See
Frequency Bands, Exhibit B (identifying the proposed frequency bands to be used on the
LEMUR constellations); see also infra Part II.A.4 (discussing the frequency bands used by the
LEMUR constellations).
7
 See, e.g., Amendment of Parts 1, 2, 15, 25, 27, 74, 78, 80, 87, 90, 97, and 101 of the
Commission’s Rules Regarding Implementation of the Final Acts of the World
Radiocommunication Conference (Geneva, 2007) (WRC-07), Other Allocation Issues, and
Related Rule Updates, et al., Report and Order, Order, and Notice of Proposed Rulemaking, 30
FCC Rcd 4183 ¶ 106 (2015) (“WRC-07 Implementation Order”).


                                                  2


                                                                                      Exhibit A
                                                                               Spire Global, Inc.
                                                                         Response to Question 43
                                                                                 FCC Form 312

at the International Space University who began building a prototype nanosatellite as a platform

for making space accessible and affordable to students. Early funding for the concept came from

the crowdfunding website Kickstarter, where the original ArduSat (short for “Arduino-based

satellite”) concept raised more than $100,000 from nearly 700 private space enthusiasts.8 Two

ArduSats were released into orbit from the International Space Station on November 19, 2013

pursuant to an experimental authorization granted by the Office of Engineering and Technology

(“OET”).9 Kickstarter funders and others used these satellites to test experiments, play games,

take pictures, and run applications. For this pioneering work related to the ArduSats, the Obama

Administration recognized Spire Co-founder and CEO Peter Platzer as a “Champion of

Change.”10

       Building on the success and experience of the ArduSat satellites, Spire subsequently

sought and received Federal Communications Commission (“FCC” or “Commission”) authority

to conduct a market trial with two, more advanced satellites, ArduSat-2 and LEMUR-1.11 These

satellites, which have more equipment and greater functionality than the prior ArduSats, were

designed to explore the potential commercial viability of providing services for educational,

8
 ArduSat—Your Arduino Experiment in Space, KICKSTARTER,
https://www.kickstarter.com/projects/575960623/ardusat-your-arduino-experiment-in-space (last
accessed May 27, 2015).
9
 See Application of Ardusat Inc., ELS File No. 0917-EX-ST-2012, Call Sign WG9XFC (granted
Apr. 26, 2013); Application of Ardusat Inc., ELS File No. 0787-EX-PL-2013, Call Sign
WG2XZS (granted Mar. 14, 2014).
10
  Peter Platzer, Creating Next Generation Innovators Through Space Education,
WHITEHOUSE.GOV BLOG (Jun. 6, 2013), https://www.whitehouse.gov/blog/2013/06/06/creating-
next-generation-innovators-through-space-education.
11
  See Application of NanoSatisfi, Inc., ELS File No. 0532-EX-PL-2013, Call Sign WG2XXW
(granted Dec. 6, 2013); Application of Spire Global, Inc., ELS File No. 0213-EX-PL-2014, Call
Sign WH2XCV (granted Apr. 25, 2014).


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Document Created: 2016-08-29 17:44:19
Document Modified: 2016-08-29 17:44:19

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