Official name DTUSAT 2
Alternative name DTUSat-2
Cospar ID 2014-033W
Norad ID 40030
Launch date 2014-06-19
Launch site OREN
Launch vehicle Dnepr
Country/Organization Denmark
Type application Technology, education
Operator Danmarks Tekniske Universitet
RCS size SMALL
Decay date ON ORBIT
Period (min) 96.16
Inclination (deg) 98
Perigee (km) 568
Apogee (km) 581
Eccentricity 0.0113141862489121
Mean motion (revs. per day) 14.9750415973378
Semi-Major axis (km) 6952.635
Raan (deg) 71.0356
Arg of perigee (deg) 326.0813
Shape Box
Mass (kg) 1.333
Height (m) 0.1
Width (m) 0.1
Depth (m) 0.1
Span (m^2) 0.1
Contractors Danmarks Tekniske Universitet
Equipment GPPL
Propulsion None
Configuration CubeSat (1U)
Power Solar cells, batteries

DTUSat 2 (Danmarks Tekniske Universitet Satellite 2) is a Danish 1U CubeSat to demonstrate the tracking of birds from space.

The GPPL (Ground Primary Payload) tracking system was developed by students and educators at DTU Space. It comprises as a ground segment a miniature radio-transmitter to be mounted on the carrier birds, prior to the migration, and as the space component the DTUSat-2 satellite carrying a purpose-built receiver system to complement the bird transmitters. The system provides GPS position data for individual bird compact transmitters (< 5 g) and hence yield unparalleled accuracy as compared to other systems.

The satellite was successfully deployed in orbit and beacon signals were successfully received on the first pass of the satellite. Due to some problems in the electrical power supply system on the satellite and some unforeseen problems with the ground station, no two-way communications with the satellite could be established yet. The satellite is still active and transmits beacons.

Satellite COSPAR Date LS Launch Vehicle Remarks
DTUSAT 2 2014-033W 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, 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, AeroCube 6A, AeroCube 6B