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		<id>http://wiki.newmars.com/index.php?action=history&amp;feed=atom&amp;title=Low_Earth_Orbit</id>
		<title>Low Earth Orbit - Revision history</title>
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		<updated>2026-05-19T20:32:04Z</updated>
		<subtitle>Revision history for this page on the wiki</subtitle>
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	<entry>
		<id>http://wiki.newmars.com/index.php?title=Low_Earth_Orbit&amp;diff=279&amp;oldid=prev</id>
		<title>Josh Cryer: 1 revision</title>
		<link rel="alternate" type="text/html" href="http://wiki.newmars.com/index.php?title=Low_Earth_Orbit&amp;diff=279&amp;oldid=prev"/>
				<updated>2009-01-21T11:02:30Z</updated>
		
		<summary type="html">&lt;p&gt;1 revision&lt;/p&gt;
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				&lt;td colspan=&#039;1&#039; style=&quot;background-color: white; color:black; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&#039;1&#039; style=&quot;background-color: white; color:black; text-align: center;&quot;&gt;Revision as of 11:02, 21 January 2009&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&#039;2&#039; style=&#039;text-align: center;&#039; lang=&#039;en&#039;&gt;&lt;div class=&quot;mw-diff-empty&quot;&gt;(No difference)&lt;/div&gt;
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		<author><name>Josh Cryer</name></author>	</entry>

	<entry>
		<id>http://wiki.newmars.com/index.php?title=Low_Earth_Orbit&amp;diff=278&amp;oldid=prev</id>
		<title>Maxie: Category</title>
		<link rel="alternate" type="text/html" href="http://wiki.newmars.com/index.php?title=Low_Earth_Orbit&amp;diff=278&amp;oldid=prev"/>
				<updated>2006-01-27T23:40:40Z</updated>
		
		<summary type="html">&lt;p&gt;Category&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;Low earth orbit or LEO refers to the lowest orbits that are stable for a reasonable length of time (months?). Typically around 200 - 1200 km (124 - 726 miles) above the Earth&amp;#039;s surface.  These orbits tend to have orbital velocities around 27,400 km/h (8 km/s), making one revolution in about 90 minutes but are only a small distance above the Earth compared to other orbits such as geostationary orbits. (See: [[GEO]]) &lt;br /&gt;
&lt;br /&gt;
The International Space Station ([[ISS]]) for instance, is in a LEO orbit, making it accessible to [[Soyuz]] and [[Space Shuttle]] manned missions, and [[Progress]] and [[ATV]] unmanned resupply missions.&lt;br /&gt;
&lt;br /&gt;
LEO is used as a baseline to compare the payload capacity of rockets.&lt;br /&gt;
&lt;br /&gt;
[[Category:Interplanetary Transportation]]&lt;/div&gt;</summary>
		<author><name>Maxie</name></author>	</entry>

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