Official name USA 159
Alternative name DSP 21
Cospar ID 2001-033A
Norad ID 26880
Launch date 2001-08-06
Launch site AFETR
Launch vehicle Titan-4(02)B IUS
Country/Organization USA
Type application Early Warning
Operator US Air Force (USAF) → US Space Force (USSF)
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.12
Inclination (deg) 12.06
Perigee (km) 35782
Apogee (km) 35792
Eccentricity 0.000139715539162266
Mean motion (revs. per day) 1.00270172408991
Semi-Major axis (km) 42165.135
Raan (deg) 21.5624
Arg of perigee (deg) 229.602
Shape Cyl + 1 Pan
Mass (kg) 2386
Diameter (m) 3.3
Height (m) 10
Span (m^2) 11.5
Contractors TRW → Northrop Grumman
Equipment ?
Propulsion ?
Power 4 deployable fixed solar arrays, solar cells, batteries

The DSP (Defense Support Program) Block-3 (a.k.a DSP-I) satellites are the third generation of DSP early warning satellites, which cost about $ 180M per spacecraft.

The Spacecraft spins slowly (6 rpm) about the nadir axis to permit scanning of the Earth by the detector system. Zero momentum (three axis) stabilized using a reaction wheel to counter the spacecraft spin. Four solar panels deploy to generate roughly 1300 W. The DSP are radiation hardened. The payload is classified, but is probably a telescope with 6000 element IR array, nuclear explosion detectors, particle detection monitors.

DSP 23 failed less then a year after launch and was inspected by the MITEx A and MITEx B satellites in orbit.

DSP 16 was retired in 2016 and was moved into a graveyard orbit above the geostationary belt.

Satellite COSPAR Date LS Launch Vehicle Remarks
USA 39 1989-046A 1989-06-14 AFETR Titan-4(02)A IUS
USA 65 1990-095A 1990-11-13 AFETR Titan-4(02)A IUS
USA 75 1991-080B 1991-11-24 AFETR Shuttle [IUS] with Atlantis-F10 (STS 44)
USA 107 1994-084A 1994-12-22 AFETR Titan-4(02)A IUS
USA 130 1997-008A 1997-02-23 AFETR Titan-4(02)B IUS
USA 142 1999-017A 1999-04-09 AFETR Titan-4(02)B IUS
USA 149 2000-024A 2000-05-08 AFETR Titan-4(02)B IUS
USA 159 2001-033A 2001-08-06 AFETR Titan-4(02)B IUS
USA 176 2004-004A 2004-02-14 AFETR Titan-4(02)B IUS
USA 197 2007-054A 2007-11-11 AFETR Delta-4H