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- UniSat_6 abstract "UniSat 6 is an Italian micro-satellite launched in 2014. The satellite is built in a 0.5x0.5x0.5m box-shaped bus, optimized for piggy-back launch. All instruments are powered by solar cells mounted on the spacecraft body, with maximal electrical power of 11W. The satellite has no on-orbit propulsion, it makes use of an attitude stabilization system based on permanent magnets.".
- UniSat_6 wikiPageExternalLink www.gaussteam.com.
- UniSat_6 wikiPageID "43139666".
- UniSat_6 wikiPageRevisionID "637990528".
- UniSat_6 apoapsis "700".
- UniSat_6 caption "UNISAT-6 satellite during integration".
- UniSat_6 cosparId "2014".
- UniSat_6 eccentricity "0".
- UniSat_6 inclination "97.9".
- UniSat_6 launchVehicle Dnepr-1.
- UniSat_6 mass "26.0".
- UniSat_6 missionDuration "ongoing".
- UniSat_6 missionType "technology demonstration".
- UniSat_6 name "UNISAT-6".
- UniSat_6 organization GAUSS_Srl.
- UniSat_6 periapsis "620".
- UniSat_6 webpage www.gaussteam.com.
- UniSat_6 subject Category:2014_in_Italy.
- UniSat_6 subject Category:Satellites_of_Italy.
- UniSat_6 subject Category:Spacecraft_launched_in_2014.
- UniSat_6 subject Category:Student_satellites.
- UniSat_6 comment "UniSat 6 is an Italian micro-satellite launched in 2014. The satellite is built in a 0.5x0.5x0.5m box-shaped bus, optimized for piggy-back launch. All instruments are powered by solar cells mounted on the spacecraft body, with maximal electrical power of 11W. The satellite has no on-orbit propulsion, it makes use of an attitude stabilization system based on permanent magnets.".
- UniSat_6 label "UniSat 6".
- UniSat_6 sameAs m.01112d8m.
- UniSat_6 sameAs Q17285883.
- UniSat_6 sameAs Q17285883.
- UniSat_6 wasDerivedFrom UniSat_6?oldid=637990528.
- UniSat_6 isPrimaryTopicOf UniSat_6.