USA-64
{{Short description|American navigation satellite used for GPS}}
{{Use American English|date=December 2020}}
{{Use dmy dates|date=December 2020}}
{{Infobox spaceflight
| name = USA-64
| names_list = Navstar 2-09
GPS II-9
GPS SVN-15
| image =
| image_caption =
| image_size = 290px
| mission_type = Navigation
| operator = U.S. Air Force
| COSPAR_ID = 1990-088A
| SATCAT = 20830
| mission_duration = 7.5 years (planned)
16.5 years (achieved)
| spacecraft = GPS II
| spacecraft_type = GPS Block II
| manufacturer = Rockwell International
| launch_mass = {{cvt|840|kg}}
| dimensions = {{cvt|5.3|m}} of long
| power = 710 watts
| launch_date = 1 October 1990, 21:56:00 UTC
| launch_rocket = Delta II 6925-9.5
(Delta D199)
| launch_site = Cape Canaveral, LC-17A
| launch_contractor = McDonnell Douglas
| entered_service = 31 October 1990
| declared = 17 November 2006
| deactivated = 14 March 2007
| orbit_reference = Geocentric orbit
| orbit_regime = Medium Earth orbit
(Semi-synchronous)
| orbit_slot = D5 (slot 5 plane D)
| orbit_periapsis = {{cvt|19972|km}}
| orbit_apoapsis = {{cvt|20390|km}}
| orbit_inclination = 54.9°
| orbit_period = 717.94 minutes
| apsis = gee
| programme = Global Positioning System
| previous_mission = USA-63 (GPS II-8)
| next_mission = USA-66 (GPS II-10)
}}
USA-64, also known as GPS II-9 and GPS SVN-15, was an American navigation satellite which formed part of the Global Positioning System. It was the last of nine Block II GPS satellites to be launched, which were the first operational GPS satellites to fly. It was also the last Block II satellite to be retired from service.
Background
Global Positioning System (GPS) was developed by the U.S. Department of Defense to provide all-weather round-the-clock navigation capabilities for military ground, sea, and air forces. Since its implementation, GPS has also become an integral asset in numerous civilian applications and industries around the globe, including recreational used (e.g., boating, aircraft, hiking), corporate vehicle fleet tracking, and surveying. GPS employs 24 spacecraft in 20,200 km circular orbits inclined at 55.0°. These vehicles are placed in 6 orbit planes with four operational satellites in each plane.{{cite web|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1990-088A|title=Display: Navstar 2-09 1990-088A|publisher=NASA|date=14 May 2020|access-date=18 December 2020}} {{PD-notice}}
GPS Block 2 was the operational system, following the demonstration system composed of Block 1 (Navstar 1 - 11) spacecraft. These spacecraft were 3-axis stabilized, nadir pointing using reaction wheels. Dual solar arrays supplied 710 watts of power. They used S-band (SGLS) communications for control and telemetry and Ultra high frequency (UHF) cross-link between spacecraft. The payload consisted of two L-band navigation signals at 1575.42 MHz (L1) and 1227.60 MHz (L2). Each spacecraft carried 2 rubidium and 2 Cesium clocks and nuclear detonation detection sensors. Built by Rockwell Space Systems for the U.S. Air force, the spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years.
Launch
USA-64 was launched at 21:56:00 UTC on 1 October 1990, atop a Delta II launch vehicle, flight number D199, flying in the 6925 configuration.{{cite web |url=http://planet4589.org/space/log/launchlog.txt|title=Launch Log|publisher=Jonathan's Space Page|first=Jonathan|last=McDowell|access-date=10 July 2012}} The launch took place from Launch Complex 17A (LC-17A) at the Cape Canaveral Air Force Station (CCAFS),{{cite web|url=http://planet4589.org/space/lvdb/list2.html|title=Launch List|publisher=Jonathan's Space Page|work=Launch Vehicle Database|first=Jonathan|last=McDowell|access-date=10 July 2012|archive-date=15 August 2020|archive-url=https://web.archive.org/web/20200815040340/http://planet4589.org/space/lvdb/list2.html|url-status=dead}} and placed USA-64 into a transfer orbit. The satellite raised itself into medium Earth orbit using a Star-37XFP apogee motor.{{cite web|url=http://space.skyrocket.de/doc_sdat/navstar-2.htm|title=GPS-2 (Navstar-2)|first=Gunter |last=Krebs|work=Gunter's Space Page|access-date=10 July 2012}}
Mission
On 31 October 1990, USA-64 was in an orbit with a perigee of {{cvt|19972|km}}, an apogee of {{cvt|20390|km}}, a period of 717.94 minutes, and 54.9° of inclination to the equator.{{cite web |last1=McDowell |first1=Jonathan C. |title=satcat |url=https://planet4589.org/space/gcat/data/cat/satcat.html |website=General Catalog of Artificial Space Objects |access-date=4 April 2023 |archive-url=https://web.archive.org/web/20230316221545/http://www.planet4589.org/space/gcat/data/cat/satcat.html |archive-date=16 March 2023 |url-status=live}} It operated in slot 5 of plane D of the GPS constellation.{{cite web|url=http://www.astronautix.com/project/navstar.htm|archive-url=https://web.archive.org/web/20021111162023/http://www.astronautix.com/project/navstar.htm|url-status=dead|archive-date=11 November 2002|title=Navstar|publisher=Encyclopedia Astronautica |first=Mark|last=Wade|access-date=10 July 2012}} The satellite had a mass of {{cvt|840|kg}}, and generated 710 watts of power. It had a design life of 7.5 years, having been added from active service on 17 November 2006 for testing, and ceased operations on 14 March 2007.
References
{{Portal|Spaceflight}}
{{Reflist|2}}
{{GPS satellites}}
{{Orbital launches in 1990}}