Official name AAU CUBESAT
Alternative name AAU-Cubesat
Cospar ID 2003-031G
Norad ID 27846
Launch date 2003-06-30
Launch site PKMTR
Launch vehicle Rokot-KM
Country/Organization Denmark
Type application Technology
Operator Aalborg University Cubesat
RCS size SMALL
Decay date ON ORBIT
Period (min) 101.19
Inclination (deg) 98.69
Perigee (km) 809
Apogee (km) 821
Eccentricity 0.00736196319018405
Mean motion (revs. per day) 14.2306552030833
Semi-Major axis (km) 7193.135
Raan (deg) 126.7804
Arg of perigee (deg) 262.4163
Shape Box
Mass (kg) 1
Height (m) 0.1
Width (m) 0.1
Depth (m) 0.1
Span (m^2) 0.1
Contractors Aalborg University Cubesat
Propulsion None
Configuration CubeSat (1U)
Power Solar cells, batteries

The main purpose for the AAU-Cubesat (Aalborg University Cubesat) project is for the involved students to achieve a great deal of knowledge about designing and constructing Space worthy technology, but the "scientific" mission of the AAU-CubeSat is to take pictures of the surface of the Earth and particularly of Denmark by using the on-board camera. The images recorded by the satellite were later transmitted to the ground station, located at Aalborg University, from where they were distributed over the Internet and made accessible for the general public.

Several success criterias have been defined. A basic success criteria in this case is, to develop and build a satellite which is able to survive the launch and the hazardous environment in its orbit. Another success criteria is establishment of a communication link with the ground station informing about the status of the satellite. Finally to point the on board camera towards a specific target on the ground, to take an image and to send this data down to the ground station, represents the final success criteria.

To summarize the above the missions success criterias are the following:

  • That the involved students have achieved some useful knowledge of space technology.
  • That communication is established with the satellite and housekeeping information is retrieved.
  • Take and download any picture.
  • Test ACS performance.
  • Take pictures of certain locations on earth.
  • Take pictures of celestial objects and experiment with the various subsystems.

The satellite was successfully deployed in orbit, but no signals were received.

Satellite COSPAR Date LS Launch Vehicle Remarks
AAU CUBESAT 2003-031G 2003-06-30 PKMTR Rokot-KM with MOST, MIMOSA, CanX 1, DTUSat, XI-IV, CUTE 1, QuakeSat, Monitor-E GVM