Official name BADR B
Alternative name Badr B
Cospar ID 2001-056C
Norad ID 27003
Launch date 2001-12-10
Launch site TTMTR
Launch vehicle Zenit-2
Country/Organization Pakistan
Type application Technology
Operator SUPARCO
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 105.08
Inclination (deg) 99.72
Perigee (km) 984
Apogee (km) 1013
Eccentricity 0.014521782674011
Mean motion (revs. per day) 13.7038446897602
Semi-Major axis (km) 7376.635
Raan (deg) 280.0105
Arg of perigee (deg) 318.9499
Shape Box + 1 Arm
Mass (kg) 69
Height (m) 0.5
Width (m) 0.5
Depth (m) 0.5
Span (m^2) 6.5
Lifetime 2 years
Contractors SUPARCO
Power Solar cells, batteries

Badr-B is a follow up microsatellite project of the Pakistani space agency (SUPARCO), to its original Badr-A microsatellite project.

Badr-2 was developed in collaboration with UK industry and science institutes. Instruments monitor clouds to high resolution, and atmospheric atomic oxygen. Badr B is box shaped with side dimensions of 51 cm × 51 cm × 46.5 cm and features a gravity gradient stabilization system. The satellite weighs 68.5 kg and is built and designed in Pakistan with some foreign sub-systems. The camera was developed by RAL in the UK.

Besides the earth observation mission, Badr-B also used a radiation dosimeter to measure the exposure of Sun's ionizing radiation and, ans also studied the electromagnetic field of Earth. The Badr-B also conducted studies on battery charge when it is exposed to Solar flare and Solar winds.

Badr-B was launched with the Meteor-3M 1 meteorological satellite on a Zenit-2 launcher from Baikonur Cosmodrome on the 10 December 2001, into a 996 × 1050 km sun-synchronous orbit inclined at 99.7°. Other piggyback payloads on the same launch were Kompass, Maroc-Tubsat and Reflector.

Satellite COSPAR Date LS Launch Vehicle Remarks
BADR B 2001-056C 2001-12-10 TTMTR Zenit-2 with Meteor-3M 1, Kompass, Maroc-Tubsat, Reflector