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- STARS-II abstract "Space Tethered Autonomous Robotic Satellite II or STARS-II, was a nanosatellite built by Japan's Kagawa University to test an electrodynamic tether in low Earth orbit. The satellite split into two parts, connected by a 300-metre (980 ft) tether, to conduct its experiments which consisted of recording a video of tether deployment and using the tether to deorbit the satellite. The spacecraft consisted of a 5-kilogram (11 lb) base vehicle, with dimensions of 160 by 160 by 253 millimetres (6.3 in × 6.3 in × 10.0 in) and a 4-kilogram (8.8 lb) vehicle at the end of the tether measuring 160 by 160 by 158 millimetres (6.3 in × 6.3 in × 6.2 in).STARS-II was launched by an H-IIA rocket, flying in the 202 configuration, as a secondary payload aboard the launch of the GPM Core Observatory on 27 February 2014. After two months in orbit, STARS-II reentered the atmosphere on 26 April 2014.".
- STARS-II cosparId "2014-009H".
- STARS-II wikiPageExternalLink spacecraftDisplay.do?id=2014-009H.
- STARS-II wikiPageExternalLink top.html.
- STARS-II wikiPageExternalLink stars-2.
- STARS-II wikiPageID "42469867".
- STARS-II wikiPageLength "3304".
- STARS-II wikiPageOutDegree "20".
- STARS-II wikiPageRevisionID "689621642".
- STARS-II wikiPageWikiLink Category:2014_in_Japan.
- STARS-II wikiPageWikiLink Category:Satellites_of_Japan.
- STARS-II wikiPageWikiLink Category:Spacecraft_launched_in_2014.
- STARS-II wikiPageWikiLink Category:Spacecraft_which_reentered_in_2014.
- STARS-II wikiPageWikiLink Electrodynamic_tether.
- STARS-II wikiPageWikiLink Geocentric_orbit.
- STARS-II wikiPageWikiLink Global_Precipitation_Measurement.
- STARS-II wikiPageWikiLink H-IIA.
- STARS-II wikiPageWikiLink Kagawa_University.
- STARS-II wikiPageWikiLink Low_Earth_orbit.
- STARS-II wikiPageWikiLink Miniaturized_satellite.
- STARS-II wikiPageWikiLink Mitsubishi_Heavy_Industries.
- STARS-II wikiPageWikiLink STS-75.
- STARS-II wikiPageWikiLink Space_tether.
- STARS-II wikiPageWikiLink Tanegashima_Space_Center.
- STARS-II wikiPageWikiLink Yoshinobu_Launch_Complex.
- STARS-II wikiPageWikiLinkText "STARS-II".
- STARS-II apsis "gee".
- STARS-II cosparId "2014".
- STARS-II decayDate "2014-04-26".
- STARS-II launchContractor Mitsubishi_Heavy_Industries.
- STARS-II launchDate "--02-27".
- STARS-II launchRocket "H-IIA 202".
- STARS-II launchSite Tanegashima_Space_Center.
- STARS-II launchSite Yoshinobu_Launch_Complex.
- STARS-II manufacturer Kagawa_University.
- STARS-II missionType "Technology".
- STARS-II name "STARS-II".
- STARS-II operator Kagawa_University.
- STARS-II orbitEccentricity "0.0010378".
- STARS-II orbitEpoch "2014-02-28".
- STARS-II orbitInclination "65".
- STARS-II orbitPeriod "5521.2".
- STARS-II orbitReference Geocentric_orbit.
- STARS-II orbitRegime Low_Earth_orbit.
- STARS-II satcat "39579".
- STARS-II wikiPageUsesTemplate Template:Convert.
- STARS-II wikiPageUsesTemplate Template:End-date.
- STARS-II wikiPageUsesTemplate Template:Infobox_spaceflight.
- STARS-II wikiPageUsesTemplate Template:Japan-spacecraft-stub.
- STARS-II wikiPageUsesTemplate Template:Orbital_launches_in_2014.
- STARS-II wikiPageUsesTemplate Template:Refimprove.
- STARS-II wikiPageUsesTemplate Template:Reflist.
- STARS-II wikiPageUsesTemplate Template:Start-date.
- STARS-II wikiPageUsesTemplate Template:Url.
- STARS-II wikiPageUsesTemplate Template:Use_British_English.
- STARS-II wikiPageUsesTemplate Template:Use_dmy_dates.
- STARS-II subject Category:2014_in_Japan.
- STARS-II subject Category:Satellites_of_Japan.
- STARS-II subject Category:Spacecraft_launched_in_2014.
- STARS-II subject Category:Spacecraft_which_reentered_in_2014.
- STARS-II hypernym Nanosatellite.
- STARS-II type ArtificialSatellite.
- STARS-II type CelestialBody.
- STARS-II type Place.
- STARS-II type Satellite.
- STARS-II type Location.
- STARS-II type Place.
- STARS-II type Thing.
- STARS-II comment "Space Tethered Autonomous Robotic Satellite II or STARS-II, was a nanosatellite built by Japan's Kagawa University to test an electrodynamic tether in low Earth orbit. The satellite split into two parts, connected by a 300-metre (980 ft) tether, to conduct its experiments which consisted of recording a video of tether deployment and using the tether to deorbit the satellite.".
- STARS-II label "STARS-II".
- STARS-II sameAs Q16323051.
- STARS-II sameAs STARS-II.
- STARS-II sameAs m.0107_tts.
- STARS-II sameAs Q16323051.
- STARS-II wasDerivedFrom STARS-II?oldid=689621642.
- STARS-II isPrimaryTopicOf STARS-II.