dbo:SpaceMission/missionDuration |
3652.5 |
dbo:abstract |
N-STAR b, was a geostationary communications satellite originally ordered by a consortium including NTT DoCoMo and JSAT Corporation, and later fully acquired by JSAT, which was merged into SKY Perfect JSAT Group. It was designed and manufactured by Space Systems/Loral on the SSL 1300 platform. It had a launch weight of 3,400 kg (7,500 lb), and a 10-year design life. Its payload is composed of 6 C-band, 11 Ka-band, 8 Ku-band and 1 S-band transponders. (en) O N-Star B foi um satélite de comunicação geoestacionário japonês construído pela empresa Space Systems/Loral (SS/L), e foi operado pela NTT DoCoMo. O satélite foi baseado na plataforma LS-1300 e sua vida útil estimada era de 10 anos. (pt) |
dbo:cosparId |
1996-007A |
dbo:launchDate |
1996-02-05 (xsd:date) |
dbo:launchVehicle |
dbr:Ariane_4 |
dbo:manufacturer |
dbr:SSL_(company) |
dbo:missionDuration |
315576000.000000 (xsd:double) |
dbo:nextMission |
dbr:N-STAR_c |
dbo:operator |
dbr:SKY_Perfect_JSAT |
dbo:previousMission |
dbr:N-STAR_a |
dbo:satcat |
23781 |
dbo:type |
dbr:Communications_satellite |
dbo:wikiPageExternalLink |
http://www.jsat.net/en/contour/satellite-fleet.html |
dbo:wikiPageID |
51386256 (xsd:integer) |
dbo:wikiPageLength |
8398 (xsd:nonNegativeInteger) |
dbo:wikiPageRevisionID |
1105512609 (xsd:integer) |
dbo:wikiPageWikiLink |
dbr:SSL_1300 dbr:Coordinated_Universal_Time dbr:S_band dbr:Geocentric_orbit dbr:Geostationary_orbit dbr:N-STAR_a dbr:N-STAR_c dbr:NTT_Communications dbr:NTT_Docomo dbr:Communications_satellite dbr:C_band_(IEEE) dbr:Transponder_(satellite_communications) dbr:ELA-2 dbr:Nippon_Telegraph_and_Telephone dbr:Ka_band dbr:Guiana_Space_Centre dbr:JCSAT-5A dbr:JSAT_Corporation dbc:Communications_satellites_of_Japan dbr:Ariane_4 dbr:Arianespace dbc:Communications_satellites_in_geostationary_orbit dbc:Satellites_of_Japan dbc:Satellites_using_the_SSL_1300_bus dbc:Spacecraft_launched_in_1996 dbr:JSAT_(satellite_constellation) dbr:Ku_band dbr:SSL_(company) dbr:SKY_Perfect_JSAT |
dbp:apsis |
gee (en) |
dbp:cosparId |
1996 (xsd:integer) |
dbp:imageSize |
300 (xsd:integer) |
dbp:insigniaSize |
200 (xsd:integer) |
dbp:launchContractor |
dbr:Arianespace |
dbp:launchDate |
0001-02-05 (xsd:gMonthDay) |
dbp:launchRocket |
dbr:Ariane_4 |
dbp:launchSite |
dbr:ELA-2 dbr:Guiana_Space_Centre |
dbp:manufacturer |
dbr:SSL_(company) |
dbp:missionDuration |
3.15576E8 |
dbp:missionType |
dbr:Communications_satellite |
dbp:name |
N-STAR b (en) |
dbp:nextMission |
dbr:N-STAR_c |
dbp:operator |
dbr:SKY_Perfect_JSAT |
dbp:orbitReference |
dbr:Geocentric_orbit |
dbp:orbitRegime |
dbr:Geostationary_orbit |
dbp:previousMission |
dbr:N-STAR_a |
dbp:programme |
dbr:JSAT_(satellite_constellation) |
dbp:satcat |
23781 (xsd:integer) |
dbp:spacecraft |
N-STAR b (en) |
dbp:spacecraftBus |
dbr:SSL_1300 |
dbp:transBand |
1 (xsd:integer) 6 (xsd:integer) 8 (xsd:integer) 11 (xsd:integer) |
dbp:transCoverage |
Japan (en) |
dbp:wikiPageUsesTemplate |
dbt:Cvt dbt:Infobox_spaceflight dbt:Portal dbt:Reflist dbt:Use_American_English dbt:Use_dmy_dates dbt:Orbital_launches_in_1996 |
dcterms:subject |
dbc:Communications_satellites_of_Japan dbc:Communications_satellites_in_geostationary_orbit dbc:Satellites_of_Japan dbc:Satellites_using_the_SSL_1300_bus dbc:Spacecraft_launched_in_1996 |
rdf:type |
owl:Thing schema:Event dul:Event dbo:SocietalEvent wikidata:Q1656682 wikidata:Q2133344 dbo:Event dbo:SpaceMission |
rdfs:comment |
N-STAR b, was a geostationary communications satellite originally ordered by a consortium including NTT DoCoMo and JSAT Corporation, and later fully acquired by JSAT, which was merged into SKY Perfect JSAT Group. It was designed and manufactured by Space Systems/Loral on the SSL 1300 platform. It had a launch weight of 3,400 kg (7,500 lb), and a 10-year design life. Its payload is composed of 6 C-band, 11 Ka-band, 8 Ku-band and 1 S-band transponders. (en) O N-Star B foi um satélite de comunicação geoestacionário japonês construído pela empresa Space Systems/Loral (SS/L), e foi operado pela NTT DoCoMo. O satélite foi baseado na plataforma LS-1300 e sua vida útil estimada era de 10 anos. (pt) |
rdfs:label |
N-STAR b (en) N-Star B (pt) |
owl:sameAs |
yago-res:N-STAR b wikidata:N-STAR b dbpedia-pt:N-STAR b https://global.dbpedia.org/id/aymP |
prov:wasDerivedFrom |
wikipedia-en:N-STAR_b?oldid=1105512609&ns=0 |
foaf:isPrimaryTopicOf |
wikipedia-en:N-STAR_b |
foaf:name |
N-STAR b (en) |
is dbo:nextMission of |
dbr:N-STAR_a |
is dbo:previousMission of |
dbr:N-STAR_c |
is dbo:wikiPageWikiLink of |
dbr:SSL_1300 dbr:N-STAR_a dbr:N-STAR_c dbr:1996_in_spaceflight dbr:List_of_Ariane_launches_(1990–1999) dbr:JSAT_Corporation dbr:JSAT_(satellite_constellation) |
is dbp:nextMission of |
dbr:N-STAR_a |
is dbp:previousMission of |
dbr:N-STAR_c |
is foaf:primaryTopic of |
wikipedia-en:N-STAR_b |