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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 and successfully deployed into the orbit. The CubeSat standard for nanosatellites was followed during the engineering of ESTCube-1, resulting in a 10×10×11.35 cm…
Technology, Measurement & Standards
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| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| ESTCube-1 | Apogee altitude | 665 km | 1.00 | infobox |
| ESTCube-1 | Contractor | ESA | 1.00 | infobox |
| ESTCube-1 | COSPAR ID | 2013-021C | 1.00 | infobox |
| ESTCube-1 | Deactivated | 17 Feb 2015, 10:27:00 (2015-02-17UTC10:27Z) UTC | 1.00 | infobox |
| ESTCube-1 | Decay date | 2038*estimated | 1.00 | infobox |
| ESTCube-1 | Dry mass | 1.048 kilograms (2.31 lb) | 1.00 | infobox |
| ESTCube-1 | Inclination | 98.129 degrees | 1.00 | infobox |
| ESTCube-1 | Last contact | 19 May 2015 | 1.00 | infobox |
| ESTCube-1 | Launch date | 7 May 2013, 02:06:31 (2013-05-07UTC02:06:31Z) UTC | 1.00 | infobox |
| ESTCube-1 | Launch mass | 1.048 kilograms (2.31 lb) | 1.00 | infobox |
| ESTCube-1 | Launch site | Kourou ELA-1 | 1.00 | infobox |
| ESTCube-1 | Mission duration | Planned: 12 months Final: 1 year, 9 months, 10 days | 1.00 | infobox |
| ESTCube-1 | Mission type | Technology | 1.00 | infobox |
| ESTCube-1 | Operator | University of Tartu | 1.00 | infobox |
| ESTCube-1 | Perigee altitude | 665 km | 1.00 | infobox |
| ESTCube-1 | Period | 98.03 minutes | 1.00 | infobox |
| ESTCube-1 | Power | 3.6 W | 1.00 | infobox |
| ESTCube-1 | Reference system | Geocentric | 1.00 | infobox |
| ESTCube-1 | Regime | Low Earth | 1.00 | infobox |
| ESTCube-1 | Rocket | Vega flight VV02 | 1.00 | infobox |
| ESTCube-1 | SATCAT no. | 39161 | 1.00 | infobox |
| ESTCube-1 | Website | http://www.estcube.eu/en/home | 1.00 | infobox |
| ESTCube-1 | is a | first Estonian satellite and first satellite in the world to attempt to use an electric solar wind sail | 0.90 | text |
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