About: USA-1 (satellite)   Sponge Permalink

An Entity of Type : dbkwik:resource/G7YR4yAvfoe7I_ap4nmguQ==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

USA-1, also known as Navstar 9, GPS I-9 and GPS SVN-9, was an American navigation satellite launched in 1984 as part of the Global Positioning System development programme. It was the ninth of eleven Block I GPS satellites to be launched, and the first satellite to receive a USA designation.

AttributesValues
rdf:type
rdfs:label
  • USA-1 (satellite)
rdfs:comment
  • USA-1, also known as Navstar 9, GPS I-9 and GPS SVN-9, was an American navigation satellite launched in 1984 as part of the Global Positioning System development programme. It was the ninth of eleven Block I GPS satellites to be launched, and the first satellite to receive a USA designation.
sameAs
COSPAR ID
  • 1984(xsd:integer)
dcterms:subject
dbkwik:nasa/proper...iPageUsesTemplate
deactivated
  • 1994-06-20(xsd:date)
SATCAT
  • 15039(xsd:integer)
Mission Duration
  • 3.15576E8
  • 1.57788E8
spacecraft type
Name
  • USA-1
Manufacturer
orbit period
  • 43076.4
orbit inclination
  • 62(xsd:double)
Operator
launch site
Mission Type
apsis
  • gee
orbit regime
launch rocket
Launch date
  • --06-13
orbit reference
abstract
  • USA-1, also known as Navstar 9, GPS I-9 and GPS SVN-9, was an American navigation satellite launched in 1984 as part of the Global Positioning System development programme. It was the ninth of eleven Block I GPS satellites to be launched, and the first satellite to receive a USA designation. USA-1 was launched at 11:37 UTC on 13 June 1984, atop an Atlas E/F carrier rocket with an SGS-2 upper stage. The Atlas used had the serial number 42E, and was originally built as an Atlas E. The launch took place from Space Launch Complex 3W at Vandenberg Air Force Base, and placed USA-1 into a transfer orbit. The satellite raised itself into medium Earth orbit using a Star-27 apogee motor. By 14 July 1984, USA-1 had been raised to an orbit with a perigee of kilometre (mi), an apogee of kilometre (mi), a period of 717.94 minutes, and 62.5 degrees of inclination to the equator. The satellite had a design life of 5 years and a mass of kilogram (lb). It broadcast the PRN 13 signal in the GPS demonstration constellation, and was retired from service on 20 June 1994.
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