Mission type | Technology |
---|---|
Operator | University of Tartu |
COSPAR ID | 2013-021C |
SATCAT no. | 39161 |
Website | http://www.estcube.eu/en/home |
Mission duration | Planned: 12 months Final: 1 year, 9 months, 10 days |
Spacecraft properties | |
Launch mass | 1.048 kilograms (2.31 lb) |
Dry mass | 1.048 kilograms (2.31 lb) |
Power | 3.6 W [1] |
Start of mission | |
Launch date | 7 May 2013, 02:06:31 | UTC
Rocket | Vega flight VV02 |
Launch site | Kourou ELA-1 |
Contractor | ESA |
End of mission | |
Deactivated | 17 Feb 2015, 10:27:00[2] | UTC
Last contact | 19 May 2015[1] |
Decay date | 2038*estimated |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 665 km |
Apogee altitude | 665 km |
Inclination | 98.129 degrees |
Period | 98.03 minutes |
ESTCube-1 is the first Estonian satellite and first satellite in the world to attempt to use an electric solar wind sail (E-sail). It was launched on 7 May, 2013, aboard Vega VV02 carrier rocket[3][4] and successfully deployed into the orbit.[5] The CubeSat standard for nanosatellites was followed during the engineering of ESTCube-1, resulting in a 10×10×11.35 cm cube, with a volume of 1 liter and a mass of 1.048 kg.[6][7]
The mission ended officially on 17 February, 2015, and it was said that during this time it resulted in 29 bachelor's and 19 master's dissertations, 5 doctoral theses and 4 start-ups.[8] The deployment of the E-sail tether was unsuccessful, and thus no measurements were taken of the E-sail or of the plasma braking deployment system.[9] The last signal from ESTCube-1 was received on 19 May, 2015.
Amsat
was invoked but never defined (see the help page).photo
was invoked but never defined (see the help page).