USA-49
American navigation satellite used for GPS
title: "USA-49" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["gps-satellites", "usa-satellites", "spacecraft-launched-in-1989"] description: "American navigation satellite used for GPS" topic_path: "general/gps-satellites" source: "https://en.wikipedia.org/wiki/USA-49" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0
::summary American navigation satellite used for GPS ::
::data[format=table title="Infobox spaceflight"]
| Field | Value |
|---|---|
| name | USA-49 |
| names_list | Navstar 2-05 |
| GPS II-5 | |
| GPS SVN-17 | |
| image_size | 290px |
| mission_type | Navigation |
| operator | U.S. Air Force |
| COSPAR_ID | 1989-097A |
| SATCAT | 20361 |
| mission_duration | 7.5 years (planned) |
| 15 years (achieved) | |
| spacecraft | GPS II |
| spacecraft_type | GPS Block II |
| manufacturer | Rockwell International |
| launch_mass | 840 kg |
| dimensions | 5.3 m of long |
| power | 710 watts |
| launch_date | 11 December 1989, |
| 18:10:01 UTC | |
| launch_rocket | Delta II 6925-9.5 |
| (Delta D190) | |
| launch_site | Cape Canaveral, LC-17B |
| launch_contractor | McDonnell Douglas |
| entered_service | January 1990 |
| deactivated | 23 February 2005 |
| orbit_reference | Geocentric orbit |
| orbit_regime | Medium Earth orbit |
| (Semi-synchronous) | |
| orbit_slot | D3 (slot 3 plane D) |
| orbit_periapsis | 20009 km |
| orbit_apoapsis | 20357 km |
| orbit_inclination | 54.9° |
| orbit_period | 718.0 minutes |
| apsis | gee |
| programme | Global Positioning System |
| previous_mission | USA-47 (GPS II-4) |
| next_mission | USA-50 (GPS II-6) |
| :: |
| name = USA-49 | names_list = Navstar 2-05 GPS II-5 GPS SVN-17 | image = | image_caption = | image_size = 290px
| mission_type = Navigation | operator = U.S. Air Force | COSPAR_ID = 1989-097A | SATCAT = 20361 | mission_duration = 7.5 years (planned) 15 years (achieved)
| spacecraft = GPS II | spacecraft_type = GPS Block II | manufacturer = Rockwell International | launch_mass = 840 kg | dimensions = 5.3 m of long | power = 710 watts
| launch_date = 11 December 1989, 18:10:01 UTC | launch_rocket = Delta II 6925-9.5 (Delta D190) | launch_site = Cape Canaveral, LC-17B | launch_contractor = McDonnell Douglas
| entered_service = January 1990 | disposal_type = | deactivated = 23 February 2005
| orbit_reference = Geocentric orbit | orbit_regime = Medium Earth orbit (Semi-synchronous) | orbit_slot = D3 (slot 3 plane D) | orbit_periapsis = 20009 km | orbit_apoapsis = 20357 km | orbit_inclination = 54.9° | orbit_period = 718.0 minutes | apsis = gee
| programme = Global Positioning System | previous_mission = USA-47 (GPS II-4) | next_mission = USA-50 (GPS II-6)
USA-49, also known as GPS II-5 and GPS SVN-17, was an American navigation satellite which formed part of the Global Positioning System. It was the fifth of nine Block II GPS satellites to be launched, which were the first operational GPS satellites to fly.
Background
It was part of the 21-satellite Global Positioning System (GPS) Block II series that provides precise position data (accurate to within 16 m) to military and civilian users worldwide. Its signals could be received on devices as small as a telephone. The GPS II satellites, built by Rockwell International for the Air Force Space Systems Division, each have a 7.5-year design life. The Air Force intends to launch a GPS II every 2 to 3 months until the constellation of 21 operational satellite and 3 spares is aloft. The GPS Block II join 7 operational Block 1 satellites.
Launch
USA-49 was launched at 18:10:01 UTC on 11 December 1989, atop a Delta II launch vehicle, flight number D190, flying in the 6925-9.5 configuration. The launch took place from Launch Complex 17B (LC-17B) at the Cape Canaveral Air Force Station (CCAFS), and placed USA-49 into a transfer orbit. The satellite raised itself into medium Earth orbit using a Star-37XFP apogee motor.
Mission
On 11 January 1990, USA-49 was in an orbit with a perigee of 20009 km, an apogee of 20357 km, a period of 718.0 minutes, and 54.9° of inclination to the equator. It operated in slot 3 of plane D of the GPS constellation. The satellite had a mass of 840 kg, and generated 710 watts of power. It had a design life of 7.5 years, and ceased operations on 23 February 2005.
References
References
- McDowell, Jonathan. "Launch Log". Jonathan's Space Report.
- McDowell, Jonathan. "Launch List". Jonathan's Space Report.
- Krebs, Gunter. "GPS-2 (Navstar-2)". Gunter's Space Page.
- McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Report.
- Wade, Mark. "Navstar". Encyclopedia Astronautica.
- "Display: Navstar 2-05 1989-097A". NASA.
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