Official name NAVSTAR 50 (USA 156)
Alternative name Navstar 50 (USA 156) (GPS IIR-7)
Cospar ID 2001-004A
Norad ID 26690
Launch date 2001-01-30
Launch site AFETR
Launch vehicle Delta-7925
Country/Organization USA
Type application Navigation
Operator US Air Force (USAF) → US Space Force (USSF)
RCS size LARGE
Decay date ON ORBIT
Period (min) 751.61
Inclination (deg) 54.58
Perigee (km) 20998
Apogee (km) 21012
Eccentricity 0.000333253987145918
Mean motion (revs. per day) 1.91588722874895
Semi-Major axis (km) 27383.135
Raan (deg) 60.9131
Arg of perigee (deg) 350.7418
Shape Box + 2 Pan
Mass (kg) 1077
Height (m) 1.5
Width (m) 1.9
Depth (m) 1.9
Span (m^2) 19.3
Lifetime 10 years
Contractors Lockheed Martin
Equipment ?
Propulsion Star-37FM
Configuration AS-4000
Power 2 deployable solar arrays, batteries

GPS-2R (Global Positioning System) or Navstar-2R (Navigation System using Timing And Ranging) are the third evolution stage of the second generation of the GPS satellites.

The GPS-IIR replenishment satellites are produced by General Electric Astrospace (later Martin Marietta and Lockheed Missiles & Space) under a contract issued in 1989, which included 21 satellites based on the commercial AS-4000 bus. These provided improved navigation accuracy and longer autonomous satellite operation than earlier model GPS satellites. The satellites were three-axis stabilized and operated at downlink frequencies of 1572.42 MHz and 1227.6 MHz (L-Band) and 2227.5 MHz (S-Band). Lockheed was responsible for launch and flight operations support of the GPS-IIR through 2006.

Block IIR satellites provided dramatic improvements over previous blocks. They could determine their own position by performing inter-satellite ranging with other IIR vehicles. They also had reprogramable satellite processors enabling problem fixes and upgrades in flight, increased satellite autonomy, and radiation hardness.

Additionally, the Block IIR could be launched into any of the required GPS orbits at any time, assuming a 60-day advanced notice, and required many fewer ground contacts to maintain the constellation. All of these improvements result in increased accuracy for GPS users and a cost 33 percent less per satellite than the previous generation of Block IIA satellites. Up to 12 Block IIR satellites were to be modified to use the new military M-code on both the L1 and L2 channel as well as the more robust civil signal L2C on the L2 channel. The M-code signal was to enable GPS operations in a higher jamming environment and reduce vulnerability of military GPS-based systems. The first modified Block IIR (or IIR-M) is planned for launch 2004.

Satellite COSPAR Date LS Launch Vehicle Remarks
NAVSTAR 43 (USA 132) 1997-035A 1997-07-23 AFETR Delta-7925
NAVSTAR 46 (USA 145) 1999-055A 1999-10-07 AFETR Delta-7925
NAVSTAR 47 (USA 150) 2000-025A 2000-05-11 AFETR Delta-7925
NAVSTAR 48 (USA 151) 2000-040A 2000-07-16 AFETR Delta-7925
NAVSTAR 49 (USA 154) 2000-071A 2000-11-10 AFETR Delta-7925
NAVSTAR 50 (USA 156) 2001-004A 2001-01-30 AFETR Delta-7925
NAVSTAR 51 (USA 166) 2003-005A 2003-01-29 AFETR Delta-7925 with XSS 10
NAVSTAR 52 (USA 168) 2003-010A 2003-03-31 AFETR Delta-7925
NAVSTAR 53 (USA 175) 2003-058A 2003-12-21 AFETR Delta-7925
NAVSTAR 54 (USA 177) 2004-009A 2004-03-20 AFETR Delta-7925
NAVSTAR 55 (USA 178) 2004-023A 2004-06-23 AFETR Delta-7925
NAVSTAR 56 (USA 180) 2004-045A 2004-11-06 AFETR Delta-7925