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NORAD Two Line Element Sets for GOES Satellites Details
- Component XLINK
- NORAD Two Line Element Sets for GOES Satellites Relationships
- Component Type
- {http://www.isotc211.org/2005/gmd}CI_Citation
- Component Set
- GLOBAL-CS
- Component Update Information
- Last Updater
- export_comp_migrate.sql
- Last Updated
- 2012-02-23 11:59:44 EST
- Date Created
- 2012-02-23 11:59:44 EST
- More Details
- NORAD Two Line Element Sets for GOES Satellites Extras
- Uuid
- 86D032BB-C51B-8BFC-E040-0AC8C5AB42D9
- Owner
- richard.fozzard
- Index Data
- NORAD Two Line Element Sets for GOES Satellites
- XML Show XML
- <?xml version="1.0" encoding="ISO-8859-1"?><gmd:CI_Citation xmlns:gmd="http://www.isotc211.org/2005/gmd" xmlns:gml="http://www.opengis.net/gml/3.2" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:gco="http://www.isotc211.org/2005/gco" xmlns:gmi="http://www.isotc211.org/2005/gmi" xmlns:gmx="http://www.isotc211.org/2005/gmx" xmlns:gsr="http://www.isotc211.org/2005/gsr" xmlns="http://www.isotc211.org/2005/gmi" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.isotc211.org/2005/gmi http://www.ngdc.noaa.gov/metadata/published/xsd/schema.xsd" uuid="86D032BB-C51B-8BFC-E040-0AC8C5AB42D9"><gmd:title><gco:CharacterString>NORAD Two Line Element Sets for GOES Satellites</gco:CharacterString></gmd:title><gmd:date gco:nilReason="inapplicable"/><gmd:citedResponsibleParty><gmd:CI_ResponsibleParty><gmd:organisationName><gco:CharacterString>CelesTrak</gco:CharacterString></gmd:organisationName><gmd:contactInfo><gmd:CI_Contact><gmd:onlineResource><gmd:CI_OnlineResource><gmd:linkage><gmd:URL>http://celestrak.com/NORAD/elements/goes.txt</gmd:URL></gmd:linkage><gmd:protocol><gco:CharacterString>http</gco:CharacterString></gmd:protocol><gmd:applicationProfile><gco:CharacterString>txt</gco:CharacterString></gmd:applicationProfile><gmd:name><gco:CharacterString>NORAD Two Line Elements</gco:CharacterString></gmd:name><gmd:description><gco:CharacterString>The NORAD TLE provided by Celestrak display up-to-date orbital elements such as Inclination, Right Ascension of the Ascending Node, Eccentricity, Argument of Perigee, and Mean Anomaly. For information on the format of TLE, go to: http://celestrak.com/NORAD/documentation/tle-fmt.asp</gco:CharacterString></gmd:description><gmd:function><gmd:CI_OnLineFunctionCode codeList="http://www.ngdc.noaa.gov/metadata/published/xsd/schema/resources/Codelist/gmxCodelists.xml#CI_OnLineFunctionCode" codeListValue="information">information</gmd:CI_OnLineFunctionCode></gmd:function></gmd:CI_OnlineResource></gmd:onlineResource></gmd:CI_Contact></gmd:contactInfo><gmd:role><gmd:CI_RoleCode codeList="http://www.ngdc.noaa.gov/metadata/published/xsd/schema/resources/Codelist/gmxCodelists.xml#CI_RoleCode" codeListValue="distributor">distributor</gmd:CI_RoleCode></gmd:role></gmd:CI_ResponsibleParty></gmd:citedResponsibleParty></gmd:CI_Citation>