Official name BRITE TORONTO
Alternative name BRITE-Toronto
Cospar ID 2014-033L
Norad ID 40020
Launch date 2014-06-19
Launch site OREN
Launch vehicle Dnepr
Country/Organization Canada
Type application Astronomy / Technology
Operator UTIAS (University of Toronto, Institute for Aerospace Studies)
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 98.01
Inclination (deg) 97.87
Perigee (km) 605
Apogee (km) 722
Eccentricity 0.0881688018085908
Mean motion (revs. per day) 14.692378328742
Semi-Major axis (km) 7041.635
Raan (deg) 268.3891
Arg of perigee (deg) 216.9561
Shape Box
Mass (kg) 7
Height (m) 0.2
Width (m) 0.2
Depth (m) 0.2
Span (m^2) 0.2
Contractors UTIAS
Propulsion None
Configuration Gryphon Bus (GNB)
Power Solar cells, batteries

CanX-3 (Canadian Advanced Nanospace eXperiments), also known as BRITE (BRIght-star Target Explorer), is a mission planned to make photometric observations of some of the brightest starts in the sky in order to examine these stars for variability. The observations have a precision at least 10 times better than achievable using ground-based observations, and it is packaged inside a CanX-class nanosatellite.

The Principal Investigator for the BRITE mission is Emeritus professor Anthony F. J. Moffat Département de physique, Université de Montréal. Prof. Jaymie Matthews (University of British Columbia), Prof. Stefan Mochnacki and Prof. Emeritus Slavek Rucinski (University of Toronto) are also part of the Canadian BRITE team. The Austrian Co-Principal Investigator is Professor Werner W. Weiss, University of Vienna.

The design is a 20 cm cube, chosen to accommodate the main telescope. It leverages a number of technologies qualified on CanX-2 and incorporates SFL's high-performance attitude control system, using reaction wheels developed in collaboration with Sinclair Interplanetary.

The two canadian satellites are copies of the Austrian BRITE satellites UniBRITE (CanX 3A) and TUGsat 1 (BRITE-Austria). One has an instrument sensitive to a blue (BRITE-Montreal) and the other with a camera optimized for a red wavelength range (BRITE-Toronto).

BRITE-CA 2 (BRITE-Montreal) failed to separate from the launch vehicle.

Satellite COSPAR Date LS Launch Vehicle Remarks
SL-24 R/B 2014-033AP 2014-06-19 OREN Dnepr with Deimos 2, KazEOSat 2, Saudisat 4, TabletSat-Aurora, BugSat 1, AprizeSat 9, AprizeSat 10, UniSat 6, BRITE-CA 1, Hodoyoshi 3, Hodoyoshi 4, Perseus-M 1, Perseus-M 2, Flock-1c 1, ..., 11, POPSAT-HIP 1, QB50P1, QB50P2, PACE, TigriSat, ANTELSAT, Lemur 1, NanoSatC-Br 1, Duchifat 1, PolyITAN 1, DTUSat 2, AeroCube 6A, AeroCube 6B / failed to separate from upper stage
BRITE TORONTO 2014-033L 2014-06-19 OREN Dnepr with Deimos 2, KazEOSat 2, Saudisat 4, TabletSat-Aurora, BugSat 1, AprizeSat 9, AprizeSat 10, UniSat 6, BRITE-CA 2, Hodoyoshi 3, Hodoyoshi 4, Perseus-M 1, Perseus-M 2, Flock-1c 1, ..., 11, POPSAT-HIP 1, QB50P1, QB50P2, PACE, TigriSat, ANTELSAT, Lemur 1, NanoSatC-Br 1, Duchifat 1, PolyITAN 1, DTUSat 2, AeroCube 6A, AeroCube 6B