Official name CANX-1
Alternative name Can X-1
Cospar ID 2003-031H
Norad ID 27847
Launch date 2003-06-30
Launch site PKMTR
Launch vehicle Rokot-KM
Country/Organization Canada
Type application Technology
Operator UTIAS (University of Toronto, Institute for Aerospace Studies)
RCS size SMALL
Decay date ON ORBIT
Period (min) 101.15
Inclination (deg) 98.69
Perigee (km) 807
Apogee (km) 820
Eccentricity 0.00799016594960049
Mean motion (revs. per day) 14.2362827483935
Semi-Major axis (km) 7191.635
Raan (deg) 153.8611
Arg of perigee (deg) 201.0811
Shape Box
Mass (kg) 1
Height (m) 0.1
Width (m) 0.1
Depth (m) 0.1
Span (m^2) 0.1
Contractors UTIAS
Propulsion None
Configuration CubeSat (1U)
Power Solar cells, batteries

The CanX-1 (Canadian Advanced Nanospace eXperiments) PicoSatellite Mission is the first in a series of CubeSat Missions at the University of Toronto. The Canadian Advanced Nanospace eXperiments (CanX) promote the development and testing of low-cost space technologies and push the envelope of performance that can be achieved with small low-power devices. The first mission, CanX-1, will launch in mid 2003 and will demonstrate key enabling technologies for future missions including:

  • A Powerful CubeSat Computer based on an Atmel ARM microprocessor.
  • Triple-Junction GaAs Solar Cells with Peak Power Tracking
  • CMOS imagers for observation and Star Tracking
  • Active Magnetic Control including B-dot Detumbling and 3-axis stabilization

The satellite is a 10 cm cube, with a mass less than one kilogram. The satellite generates about two Watts of peak power using direct energy conversion. More power is available when peak power tracking is enabled.

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

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