About: USA-166     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : dbo:ArtificialSatellite, within Data Space : dbpedia.org associated with source document(s)
QRcode icon
http://dbpedia.org/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FUSA-166

USA-166, also known as GPS IIR-8 and GPS SVN-56, is an American navigation satellite which forms part of the Global Positioning System. It was the eighth Block IIR GPS satellite to be launched, out of thirteen in the original configuration, and twenty one overall. It was built by Lockheed Martin, using the satellite bus.

AttributesValues
rdf:type
rdfs:label
  • USA-166 (en)
rdfs:comment
  • USA-166, also known as GPS IIR-8 and GPS SVN-56, is an American navigation satellite which forms part of the Global Positioning System. It was the eighth Block IIR GPS satellite to be launched, out of thirteen in the original configuration, and twenty one overall. It was built by Lockheed Martin, using the satellite bus. (en)
foaf:name
  • USA-166 (en)
name
  • USA-166 (en)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/GPS-IIR.jpg
dcterms:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
sameAs
dbp:wikiPageUsesTemplate
thumbnail
apsis
  • gee (en)
COSPAR ID
image caption
  • A Block IIR GPS satellite (en)
launch date
launch rocket
  • D295 (en)
  • Delta II 7925-9.5, (en)
launch site
manufacturer
mission duration
mission type
operator
orbit inclination
orbit period
orbit reference
orbit regime
SATCAT
spacecraft bus
spacecraft type
has abstract
  • USA-166, also known as GPS IIR-8 and GPS SVN-56, is an American navigation satellite which forms part of the Global Positioning System. It was the eighth Block IIR GPS satellite to be launched, out of thirteen in the original configuration, and twenty one overall. It was built by Lockheed Martin, using the satellite bus. USA-166 was launched at 18:06:00 UTC on 29 January 2003, atop a Delta II carrier rocket, flight number D295, flying in the 7925-9.5 configuration. The XSS-10 satellite was carried as a secondary payload on the same rocket, but was deployed from the second stage of the three-stage rocket. The launch took place from Space Launch Complex 17B at the Cape Canaveral Air Force Station, and placed USA-166 into a transfer orbit. The satellite raised itself into medium Earth orbit using a Star-37FM apogee motor. By 1 February 2003, USA-166 was in an orbit with a perigee of 20,155 kilometres (12,524 mi), an apogee of 20,344 kilometres (12,641 mi), a period of 720.7 minutes, and 55 degrees of inclination to the equator. It is used to broadcast the PRN 16 signal, and operates in slot 1 of plane B of the GPS constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of 2012 it remains in service. (en)
gold:hypernym
prov:wasDerivedFrom
mission duration (μ)
page length (characters) of wiki page
COSPAR id
  • 2003-005A
launch date
mission duration (s)
SATCAT
  • 27663
launch vehicle
manufacturer
operator
type
foaf:isPrimaryTopicOf
is Link from a Wikipage to another Wikipage of
Faceted Search & Find service v1.17_git139 as of Feb 29 2024


Alternative Linked Data Documents: ODE     Content Formats:   [cxml] [csv]     RDF   [text] [turtle] [ld+json] [rdf+json] [rdf+xml]     ODATA   [atom+xml] [odata+json]     Microdata   [microdata+json] [html]    About   
This material is Open Knowledge   W3C Semantic Web Technology [RDF Data] Valid XHTML + RDFa
OpenLink Virtuoso version 08.03.3330 as of Mar 19 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 67 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software