Official name BADR 1
Alternative name Badr-A
Cospar ID 1990-059A
Norad ID 20685
Launch date 1990-07-16
Launch site XSC
Launch vehicle CZ-2E
Country/Organization Pakistan
Type application Technology
Operator SUPARCO
RCS size MEDIUM
Decay date 1990-12-08
Shape Poly
Mass (kg) 51.54
Height (m) 0.5
Width (m) 0.5
Depth (m) 0.5
Span (m^2) 0.5
Lifetime 35 days achieved
Contractors SUPARCO
Propulsion None
Power Solar cells, batteries

Badr-A was the first pakistani satellite.

Badr-A was launched on the 16th of July 1990 from a Chinese CZ-2E launcher alongside a Aussat-B-MFS dummy payload into a 201 × 984 km orbit inclined at 28.4°, and was built by SUPARCO in Pakistan.

The spacecraft weighed 52 kg. It had 26 facets, and was electrically based on UoSAT-2. It carried Store and Forward transponder in the 144-146 MHz and 435-436 MHz bands.

The project objectives were:

  • To acquire know-how for indigenous development of satellites to create infrastructure for future satellite development activities
  • To test the performance of indigenously developed satellite subsystems in space environment
  • To perform experiments in real-time voice and data communications between two user ground stations
  • To demonstrate store-and-forward type message communication
  • To educate the country's academic, scientific and amateur community in the tracking and use of low-earth-orbiting satellites

It was originally planned for launch on a Shuttle mission in 1986, but was delayed due to the Challenger dissaster. Instead it was moved to the maiden flight of the Chinese CZ-2E rocket.

Contact was lost on the 20 August 1990 due to what is believed to be an electrical failure.

Satellite COSPAR Date LS Launch Vehicle Remarks
BADR 1 1990-059A 1990-07-16 XSC CZ-2E with Aussat-B-MFS [PKM]