 | Badr B2
| Class: Technology. Type: Communications. Destination: Maximum Payload Orbit. Nation: Pakistan. Agency: Suparco. Manufacturer: SIL. Pakistani experimental series with a variety of payloads. Badr B was built in collaboration with the English company SIL and carried an Earth imager - the first step toward an indigenous military surveillance capability. Typical orbit: 208 km x 988 km at 29 degrees inclination. Mass: 52 kg (114 lb).
Badr Chronology - 1990 July 16 - Badr-A - Launch Site: Xichang. Launch Complex: LC2. Launch Vehicle: CZ. Mass: 52 kg (114 lb). Perigee: 208 km (129 mi). Apogee: 988 km (613 mi). Inclination: 28.50 deg. Period: 96.70 min.
First launch of new Chinese launch vehicle. Experimental Pakistani payload.
- 2001 December 10 - Badr B - Launch Site: Baikonur. Launch Complex: LC45/1. Launch Vehicle: Zenit. Mass: 70 kg (154 lb). Perigee: 996 km (618 mi). Apogee: 1,015 km (630 mi). Inclination: 99.70 deg.
Badr B was Pakistan's second satellite. Built in collaboration with the English company SIL, it had a mass of 70 kg and carried an Earth imager.
Bibliography:- McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: http://msl.jpl.nasa.gov/home.html.
- McDowell, Jonathan, Launch Log, October 1998. Web Address when accessed: http://hea-www.harvard.edu/~jcm/space/log/launch.html.
- National Space Science Center Planetary Page, As of 19 February 1999.. Web Address when accessed: http://nssdc.gsfc.nasa.gov/planetary/planetary_home.html.
- NASA/GSFC Orbital Information Group Website, Web Address when accessed: http://oig1.gsfc.nasa.gov/.
- Space-Launcher.com, Orbital Report News Agency. Web Address when accessed: http://www.orbireport.com/Log.html.
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