| dbo:SpaceMission/missionDuration |
2922.0 (dbd:day) |
| dbo:abstract |
JCSAT-2 was a geostationary communications satellite designed and manufactured by Hughes (now Boeing) on the HS-393 satellite bus. It was originally ordered by Japan Communications Satellite Company (JCSAT), which later merged into the JSAT Corporation. It had a Ku-band payload and operated on the 154° East longitude until it was replaced by JCSAT-2A. (en) O JCSAT-2 O JCSAT-1 foi um satélite de comunicação geoestacionário japonês que foi construído pela Hughes e era operado pela JSAT Corporation. O satélite foi baseado na plataforma e sua vida útil estimada era de 10 anos. O mesmo ficou fora de serviço em julho de 2002 e foi enviado para a órbita cemitério. (pt) |
| dbo:cosparId |
1990-001B |
| dbo:launchDate |
1990-01-01 (xsd:date) |
| dbo:launchVehicle |
dbr:Commercial_Titan_III |
| dbo:manufacturer |
dbr:Hughes_Space_and_Communications_Company |
| dbo:missionDuration |
252460800.000000 (xsd:double) |
| dbo:nextMission |
dbr:JCSAT-3 |
| dbo:operator |
dbr:JSAT_Corporation |
| dbo:previousMission |
dbr:JCSAT-1 |
| dbo:satcat |
20402 |
| dbo:type |
dbr:Communications_satellite |
| dbo:wikiPageID |
51344978 (xsd:integer) |
| dbo:wikiPageLength |
7453 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID |
1105512300 (xsd:integer) |
| dbo:wikiPageWikiLink |
dbr:Cape_Canaveral_Space_Force_Station dbr:Cape_Canaveral_Space_Launch_Complex_40 dbr:Ampere_hour dbr:Orbital_station-keeping dbr:Coordinated_Universal_Time dbr:Geocentric_orbit dbr:Geostationary_orbit dbr:Geostationary_transfer_orbit dbr:Longitude dbr:Boeing_Satellite_Development_Center dbr:Commercial_Titan_III dbr:Communications_satellite dbr:Traveling-wave_tube dbr:Transponder_(satellite_communications) dbr:Watt dbc:Satellites_using_the_HS-393_bus dbr:Liquid_apogee_engine dbr:Graveyard_orbit dbr:HS-393 dbr:Hertz dbr:JCSAT-1 dbr:JCSAT-2A dbr:JCSAT-3 dbr:JSAT_Corporation dbc:Communications_satellites_of_Japan dbc:Communications_satellites_in_geostationary_orbit dbc:Satellites_of_Japan dbc:Spacecraft_launched_in_1990 dbr:JSAT_(satellite_constellation) dbr:Martin_Marietta dbr:Hughes_Space_and_Communications_Company dbr:Thrusters_(spacecraft) dbr:Ku_band dbr:R-4D dbr:Satellite_bus dbr:Nickel–hydrogen_battery dbr:Spin-stabilized_satellite dbr:Skynet_4A dbr:Solar_panels_on_spacecraft dbr:Japan_Communications_Satellite_Company dbr:Hughes_Space_and_Communications dbr:Attitude_dynamics_and_control dbr:Bipropellant_rocket |
| dbp:apsis |
gee (en) |
| dbp:cosparId |
1990 (xsd:integer) |
| dbp:deactivated |
2002 (xsd:integer) |
| dbp:dimensions |
with solar panels and antennas deployed. (en) |
| dbp:disposalType |
dbr:Graveyard_orbit |
| dbp:imageSize |
300 (xsd:integer) |
| dbp:insigniaSize |
200 (xsd:integer) |
| dbp:launchContractor |
dbr:Martin_Marietta |
| dbp:launchDate |
0001-01-01 (xsd:gMonthDay) |
| dbp:launchRocket |
dbr:Commercial_Titan_III |
| dbp:launchSite |
dbr:Cape_Canaveral_Space_Force_Station dbr:Cape_Canaveral_Space_Launch_Complex_40 |
| dbp:manufacturer |
dbr:Hughes_Space_and_Communications_Company |
| dbp:missionDuration |
2.524608E8 (dbd:second) |
| dbp:missionType |
dbr:Communications_satellite |
| dbp:name |
JCSAT-2 (en) |
| dbp:nextMission |
dbr:JCSAT-3 |
| dbp:operator |
dbr:JSAT_Corporation |
| dbp:orbitLongitude |
154 (xsd:integer) |
| dbp:orbitReference |
dbr:Geocentric_orbit |
| dbp:orbitRegime |
dbr:Geostationary_orbit |
| dbp:power |
2.35 (dbd:kilowatt) |
| dbp:previousMission |
dbr:JCSAT-1 |
| dbp:programme |
dbr:JSAT_(satellite_constellation) |
| dbp:satcat |
20402 (xsd:integer) |
| dbp:spacecraft |
JCSAT-2 (en) |
| dbp:spacecraftBus |
dbr:HS-393 |
| dbp:spacecraftType |
dbr:JSAT_(satellite_constellation) |
| dbp:transBand |
32 (xsd:integer) |
| dbp:transBandwidth |
864.0 (dbd:megahertz) |
| dbp:transCoverage |
Japan (en) |
| dbp:transTwta |
20 (xsd:integer) |
| dbp:wikiPageUsesTemplate |
dbt:JCSAT dbt:Cvt dbt:Infobox_spaceflight dbt:Portal dbt:Reflist dbt:Use_American_English dbt:Use_dmy_dates dbt:Orbital_launches_in_1990 |
| dct:subject |
dbc:Satellites_using_the_HS-393_bus dbc:Communications_satellites_of_Japan dbc:Communications_satellites_in_geostationary_orbit dbc:Satellites_of_Japan dbc:Spacecraft_launched_in_1990 |
| rdf:type |
owl:Thing schema:Event dul:Event dbo:SocietalEvent wikidata:Q1656682 wikidata:Q2133344 dbo:Event dbo:SpaceMission |
| rdfs:comment |
JCSAT-2 was a geostationary communications satellite designed and manufactured by Hughes (now Boeing) on the HS-393 satellite bus. It was originally ordered by Japan Communications Satellite Company (JCSAT), which later merged into the JSAT Corporation. It had a Ku-band payload and operated on the 154° East longitude until it was replaced by JCSAT-2A. (en) O JCSAT-2 O JCSAT-1 foi um satélite de comunicação geoestacionário japonês que foi construído pela Hughes e era operado pela JSAT Corporation. O satélite foi baseado na plataforma e sua vida útil estimada era de 10 anos. O mesmo ficou fora de serviço em julho de 2002 e foi enviado para a órbita cemitério. (pt) |
| rdfs:label |
JCSAT-2 (en) JCSAT-2 (ja) JCSAT-2 (pt) |
| owl:sameAs |
wikidata:JCSAT-2 yago-res:JCSAT-2 dbpedia-ja:JCSAT-2 dbpedia-pt:JCSAT-2 https://global.dbpedia.org/id/b9tx |
| prov:wasDerivedFrom |
wikipedia-en:JCSAT-2?oldid=1105512300&ns=0 |
| foaf:isPrimaryTopicOf |
wikipedia-en:JCSAT-2 |
| foaf:name |
JCSAT-2 (en) |
| is dbo:nextMission of |
dbr:JCSAT-1 |
| is dbo:previousMission of |
dbr:JCSAT-3 |
| is dbo:wikiPageWikiLink of |
dbr:Commercial_Titan_III dbr:List_of_Titan_launches dbr:HS-393 dbr:JCSAT-1 dbr:JCSAT-2A dbr:JCSAT-3 dbr:JSAT_Corporation dbr:JSAT_(satellite_constellation) dbr:Skynet_(satellite) |
| is dbp:nextMission of |
dbr:JCSAT-1 |
| is dbp:previousMission of |
dbr:JCSAT-3 |
| is foaf:primaryTopic of |
wikipedia-en:JCSAT-2 |