Official name FEDSAT
Alternative name Fedsat
Cospar ID 2002-056B
Norad ID 27598
Launch date 2002-12-14
Launch site TNSTA
Launch vehicle H-2A-202
Country/Organization Australia
Type application Science, magnetosphere
Operator Technology
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 100.76
Inclination (deg) 98.75
Perigee (km) 787
Apogee (km) 802
Eccentricity 0.00943989930774072
Mean motion (revs. per day) 14.2913854704248
Semi-Major axis (km) 7172.635
Raan (deg) 85.3399
Arg of perigee (deg) 61.8614
Shape Box + 1 Ant
Mass (kg) 58
Height (m) 0.5
Width (m) 0.5
Depth (m) 0.5
Span (m^2) 3
Contractors Space Innovations Limited (bus)
Propulsion None
Configuration MicroSIL bus
Power Solar cells, batteries

FedSat (Federation Satellite) is an Australian scientific microsatellite mission, a 58 cm cube weighing approximately 50 kg. It was launched in late 2002 from Japan by Japan's National Space Development Agency. Its purposes are:

  • to establish Australian capability in microsatellite technologies;
  • to develop expertise necessary for sustaining those industries and profiting from them;
  • to test and develop Australian-developed intellectual property;
  • and to provide a research platform for Australian space-science, communication and GPS studies.

FedSat is being developed by the Cooperative Research Centre for Satellite Systems, which combines the resources and skills of 12 Australian organisations. Contributions from each of the partner organisations are doubled by the Commonwealth Government, under its Commonwealth Government's Cooperative Research Centre's Program. The total budget of the Centre is approximately $60 million over 7 years, with $20 million of that allocated for the FedSat mission.

Much of FedSat is being developed in Australia by the CRCSS. Three of the 6 main payloads have been fully developed by the CRCSS, and the other three have been supplied by overseas organisations in consultation with the CRCSS. The satellite platform, the structure that houses and maintains the payloads, is being provided by overseas organisations. CRCSS engineers could have developed an Australian platform, but given the time available from project-start to launch, that was not practical. So the CRCSS opted to contract an overseas platform supplier, avoiding the need to reinvent established technologies.

Payloads:

  • GPS Receiver
  • NewMag: The NewMag magnetometer is a very sensitive and rapid-sampling device for measuring the strength of the Earth's magnetic field.
  • High performance computing:
    The FedSat high performance computing payload is the world's first use of reconfigurable computing technology in space.
  • Ka-band transponder
  • Baseband processor
  • CD ROM: FedSat also carries a compact disc mounted on the side, containing the audio messages members of the Australian public recorded to go into space from March to August 2000.
Satellite COSPAR Date LS Launch Vehicle Remarks
FEDSAT 2002-056B 2002-12-14 TNSTA H-2A-202 with ADEOS 2, WEOS, Micro-Lab-Sat 1