About: Raijin-2

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Raijin-2 (Rising-2) is a Japanese micro-satellite launched in 2014. The satellite is built around a 10 cm diameter, 1m focal length Cassegrain telescope and features the following instruments: * HPT - main telescope with 5m resolution at nadir, operating in visible and near-infrared bands * BOL - bolometer array camera for cloud temperature measurement * WFC - wide field-of-view CCD camera * LSI-N and LSI-W - 2 CMOS medium field-of-view cameras for near-infrared imaging * VLF-ANT, R - radio antenna to receive signatures of lighting events

Attributes	Values
rdf:type	Thing schema:Event dul:Event societal event wikidata:Q1656682 wikidata:Q2133344 yago:Artifact100021939 yago:Conveyance103100490 yago:Craft103125870 yago:Equipment103294048 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:WikicatJapaneseSatellitesAndSpaceProbes event space mission yago:Satellite104137444 yago:Spacecraft104264914 yago:Vehicle104524313 yago:Whole100003553 yago:WikicatEarthObservationSatellites
rdfs:label	Raijin-2 (in) Raijin-2 (en)
rdfs:comment	Raijin-2 (Rising-2) adalah mikro-satelit Jepang diluncurkan pada 2014. Satelit itu dibangun di sekitar diameter 10 cm. (in) Raijin-2 (Rising-2) is a Japanese micro-satellite launched in 2014. The satellite is built around a 10 cm diameter, 1m focal length Cassegrain telescope and features the following instruments: * HPT - main telescope with 5m resolution at nadir, operating in visible and near-infrared bands * BOL - bolometer array camera for cloud temperature measurement * WFC - wide field-of-view CCD camera * LSI-N and LSI-W - 2 CMOS medium field-of-view cameras for near-infrared imaging * VLF-ANT, R - radio antenna to receive signatures of lighting events (en)
foaf:name	Raijin-2 (en)
foaf:homepage	http://www.astro.mech.tohoku.ac.jp/~rising2/en/index.php%3FRISING-2
name	Raijin-2 (en)
dcterms:subject	Earth observation satellites of Japan Spacecraft launched by H-II rockets Spacecraft launched in 2014
Wikipage page ID	42864086 (xsd:integer)
Wikipage revision ID	1062839000 (xsd:integer)
Link from a Wikipage to another Wikipage	Earth observation satellite Geocentric orbit Sprite (lightning) Tohoku University 2014 in spaceflight H-IIA Tanegashima Tanegashima Space Center Earth observation satellites of Japan Spacecraft launched by H-II rockets Spacecraft launched in 2014 H-IIA rocket Cassegrain reflector Satellite
Link from a Wikipage to an external page	https://directory.eoportal.org/web/eoportal/satellite-missions/r/rising-2 http://www.astro.mech.tohoku.ac.jp/~rising2/en/index.php%3FMission http://www.astro.mech.tohoku.ac.jp/~rising2/en/index.php%3FRISING-2
sameAs	Raijin-2 Raijin-2 Raijin-2 Raijin-2
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_spaceflight dbt:Portal dbt:Reflist dbt:Start_date dbt:Unreferenced dbt:Age_in_years,_months_and_days dbt:Orbital_launches_in_2014 dbt:Japanese_space_program
apsis	gee (en)
COSPAR ID	2014 (xsd:integer)
launch date	2014-05-24 (xsd:date)
launch rocket	H-IIA 202 (en)
launch site	Tanegashima Space Center
mission type	Earth observation satellite
names list	Rising-2 (en) SpriteSat (en)
operator	Tohoku University
orbit inclination	97.900000 (xsd:double)
orbit period	5850.0 (second)
orbit reference	Geocentric orbit
SATCAT	39769 (xsd:integer)
website	http://www.astro.mech.tohoku.ac.jp/~rising2/en/index.php%3FRISING-2
has abstract	Raijin-2 (Rising-2) is a Japanese micro-satellite launched in 2014. The satellite is built around a 10 cm diameter, 1m focal length Cassegrain telescope and features the following instruments: * HPT - main telescope with 5m resolution at nadir, operating in visible and near-infrared bands * BOL - bolometer array camera for cloud temperature measurement * WFC - wide field-of-view CCD camera * LSI-N and LSI-W - 2 CMOS medium field-of-view cameras for near-infrared imaging * VLF-ANT, R - radio antenna to receive signatures of lighting events All instruments are powered by GaAs solar cells mounted on the spacecraft body, with estimated electrical power of 47.6W. The spacecraft features an unusual central-pillar bus, inherited from the Sprite-Sat satellite. The attitude control is done by means of reaction wheels and magneto-torquers, and qualified for 0.1 degrees angular accuracy. (en) Raijin-2 (Rising-2) adalah mikro-satelit Jepang diluncurkan pada 2014. Satelit itu dibangun di sekitar diameter 10 cm. (in)
orbit eccentricity	0.001300 (xsd:double)
prov:wasDerivedFrom	wikipedia-en:Raijin-2?oldid=1062839000&ns=0
page length (characters) of wiki page	8703 (xsd:nonNegativeInteger)
alternative name	Rising-2 (en) SpriteSat (en)
COSPAR id	2014-029D
launch date	2014-05-24 (xsd:date)
SATCAT	39769
launch vehicle	H-IIA
operator	Tohoku University
type	Earth observation satellite
foaf:isPrimaryTopicOf	wikipedia-en:Raijin-2
is Link from a Wikipage to another Wikipage of	List of H-II series and H3 launches List of JAXA launches Raijin (disambiguation) Diwata-1 PHL-Microsat RISING-2
is Wikipage redirect of	RISING-2
is Wikipage disambiguates of	Raijin (disambiguation)
is foaf:primaryTopic of	wikipedia-en:Raijin-2

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