Space Security Index
Space Security Index
Space Security Index
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<strong>Space</strong> <strong>Security</strong> 2011<br />
46<br />
Contributing: ese sensors belong to private contractors or other government agencies and<br />
provide some data under contract to the SSN.<br />
Data from all SSN sensors is used to maintain positions on more than 21,000 manmade<br />
objects in Earth orbit. ose objects that can be tracked repeatedly and whose source has been<br />
identied are placed in the satellite catalog, currently numbering more than 15,000 objects.<br />
A low accuracy version of this catalog is publicly available at the <strong>Space</strong> Track website, 14 but<br />
the data is not suciently precise to adequately support collision avoidance. e U.S. Air<br />
Force uses a private high-accuracy catalog for a number of data products.<br />
Operators outside the U.S. government can also request surveillance information through<br />
the Commercial and Foreign Entities (CFE) program, a pilot initiative started in 2004 that<br />
allows satellite operators to access space surveillance data through a website. Initially, the Air<br />
Force <strong>Space</strong> Command oversaw the CFE pilot program and its website, <strong>Space</strong>-Track.org.<br />
In 2009, however, responsibility for CFE, renamed SSA Sharing Program, was transferred<br />
to the U.S. Strategic Command (USSTRATCOM) — specically, to the Joint Functional<br />
Component Command for <strong>Space</strong>. But while some operators would like direct access to<br />
orbital data, there is some reluctance to release it widely. 15 For instance, regulations for the<br />
CFE program restrict the sharing of surveillance information with a non-U.S. government<br />
entity to agreements in which “providing such data analysis to that entity is in the national<br />
security interest of the United States.” 16<br />
In recent years there has been increased impetus in the U.S. to boost conjunction analysis<br />
— the ability to accurately predict high-speed collisions between two orbiting objects.<br />
However, this will necessitate certain changes in the way space objects are monitored by<br />
the Department of Defense (DOD). At the time of the Iridium collision, approximately<br />
140 spacecraft were being monitored for potential collisions and the Joint <strong>Space</strong> Operations<br />
Center (JSpOC) had ve operators supporting a single position for conjunction prediction. 17<br />
To conduct more eective collision avoidance, more personnel and computing equipment<br />
are needed. According to Lt. Gen. Larry James, former commander of the Joint Functional<br />
Component Command for <strong>Space</strong> at Vandenberg Air Force Base, collision analysis of roughly<br />
1,300 satellites — including approximately 500 that are not maneuverable — would require<br />
as many as 20 more people than were available at the time of the Cosmos-Iridium collision. 18<br />
2010 Development<br />
U.S. launches orbital space surveillance sensor as part of 20-year plan to improve SSA<br />
In November, the U.S. Air Force’s <strong>Space</strong> Command announced that it has a 20-year plan<br />
to improve U.S. SSA capability. 19 Lieutenant Colonel Richard Benz of <strong>Space</strong> Command’s<br />
Directorate of Plans and Requirements said that they were also working with U.S. Strategic<br />
Command and the National <strong>Security</strong> <strong>Space</strong> Oce to better dene requirements for SSA<br />
capabilities and systems. 20<br />
e rst step in the plan was the launch of the <strong>Space</strong> Based <strong>Space</strong> Surveillance (SBSS)<br />
Block 10 satellite on 25 September from Vandenberg Air Force Base in California. 21 e<br />
launch had been delayed almost two years from its original date of December 2008, with an<br />
entire program cost of $823-million. e Block 10 satellite is considered a “pathnder” for<br />
follow-on satellites and the eventual creation of an SBSS constellation. e launch vehicle<br />
placed the satellite into a 630-km, Sun-synchronous orbit and was designed to have a sevenyear<br />
lifespan. 22