| dbo:SpaceMission/missionDuration |
4383.0 (dbd:day) |
| dbo:abstract |
JCSAT-3 was a geostationary communications satellite designed and manufactured by Hughes (now Boeing) on the HS-601 satellite bus. It was originally ordered by JSAT Corporation, which later merged into the SKY Perfect JSAT Group. It has a mixed Ku-band and C-band payload and operated on the 128° East longitude until it was replaced by JCSAT-3A. (en) O JCSAT-3 foi um satélite de comunicação geoestacionário japonês construído pela Hughes, ele esteve localizado na posição orbital de 128 graus de longitude leste e era operado pela JSAT Corporation. O satélite foi baseado na plataforma e sua vida útil estimada era de 12 anos. O mesmo ficou fora de serviço em fevereiro de 2007 a órbita cemitério. (pt) |
| dbo:cosparId |
1995-043A |
| dbo:launchDate |
1995-08-29 (xsd:date) |
| dbo:launchVehicle |
dbr:Atlas_II |
| dbo:manufacturer |
dbr:Boeing_Satellite_Development_Center |
| dbo:missionDuration |
378691200.000000 (xsd:double) |
| dbo:nextMission |
dbr:JCSAT-4 |
| dbo:operator |
dbr:JSAT_Corporation |
| dbo:previousMission |
dbr:JCSAT-2 |
| dbo:satcat |
23649 |
| dbo:type |
dbr:Communications_satellite |
| dbo:wikiPageID |
51317307 (xsd:integer) |
| dbo:wikiPageLength |
8410 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID |
1105512358 (xsd:integer) |
| dbo:wikiPageWikiLink |
dbr:Cape_Canaveral_Launch_Complex_36 dbr:Cape_Canaveral_Space_Force_Station dbr:Ampere_hour dbr:Electrochemical_cell dbc:Satellites_using_the_BSS-601_bus dbr:Orbital_station-keeping dbr:Coordinated_Universal_Time dbr:Geocentric_orbit dbr:Geostationary_orbit dbr:Geostationary_transfer_orbit dbr:Lockheed_Martin dbr:Longitude dbr:Boeing_601 dbr:Boeing_Satellite_Development_Center dbr:Communications_satellite dbr:Syracuse_(satellite) dbr:Traveling-wave_tube dbr:C_band_(IEEE) dbc:Spacecraft_launched_in_1995 dbr:Transponder_(satellite_communications) dbr:Watt dbr:Liquid_apogee_engine dbr:Lockheed_Martin_A2100 dbr:JCSAT-10 dbr:Graveyard_orbit dbr:Hertz dbr:International_Launch_Services dbr:JCSAT-2 dbr:JCSAT-3A dbr:JCSAT-4 dbr:JSAT_Corporation dbc:Communications_satellites_of_Japan dbr:Ariane_5 dbr:Atlas_II dbc:Communications_satellites_in_geostationary_orbit dbc:Intelsat_satellites dbc:Satellites_of_Japan dbr:JSAT_(satellite_constellation) dbr:Spaceport_Florida_Launch_Complex_36 dbr:Hughes_Space_and_Communications_Company dbr:Thrusters_(spacecraft) dbr:Ku_band dbr:R-4D dbr:Satellite_bus dbr:Nickel–hydrogen_battery dbr:Solar_panels_on_spacecraft dbr:SKY_Perfect_JSAT dbr:Attitude_dynamics_and_control dbr:Bipropellant_rocket |
| dbp:apsis |
gee (en) |
| dbp:cosparId |
1995 (xsd:integer) |
| dbp:deactivated |
March 2007 (en) |
| 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:lastContact |
March 2007 (en) |
| dbp:launchContractor |
dbr:International_Launch_Services |
| dbp:launchDate |
0001-08-29 (xsd:gMonthDay) |
| dbp:launchRocket |
dbr:Atlas_II |
| dbp:launchSite |
dbr:Cape_Canaveral_Space_Force_Station dbr:Spaceport_Florida_Launch_Complex_36 |
| dbp:manufacturer |
dbr:Boeing_Satellite_Development_Center |
| dbp:missionDuration |
3.786912E8 (dbd:second) |
| dbp:missionType |
dbr:Communications_satellite |
| dbp:name |
JCSAT-3 (en) |
| dbp:nextMission |
dbr:JCSAT-4 |
| dbp:operator |
dbr:JSAT_Corporation |
| dbp:orbitLongitude |
128 (xsd:integer) |
| dbp:orbitReference |
dbr:Geocentric_orbit |
| dbp:orbitRegime |
dbr:Geostationary_orbit |
| dbp:power |
5.0 (dbd:kilowatt) |
| dbp:previousMission |
dbr:JCSAT-2 |
| dbp:programme |
dbr:SKY_Perfect_JSAT |
| dbp:satcat |
23649 (xsd:integer) |
| dbp:spacecraft |
JCSAT-3 (en) |
| dbp:spacecraftBus |
dbr:Boeing_601 |
| dbp:spacecraftType |
dbr:JSAT_(satellite_constellation) |
| dbp:transBand |
12 (xsd:integer) dbr:C_band_(IEEE) dbr:Ku_band |
| dbp:transBandwidth |
1296.0 (dbd:megahertz) |
| dbp:transCoverage |
Japan (en) |
| dbp:transTwta |
C-band: 34 watts (en) Ku-band: 63 watts (en) |
| dbp:wikiPageUsesTemplate |
dbt:JCSAT dbt:Cvt dbt:Infobox_spaceflight dbt:Portal dbt:Reflist dbt:Use_American_English dbt:Use_dmy_dates dbt:Intelsat dbt:Orbital_launches_in_1995 |
| dct:subject |
dbc:Satellites_using_the_BSS-601_bus dbc:Spacecraft_launched_in_1995 dbc:Communications_satellites_of_Japan dbc:Communications_satellites_in_geostationary_orbit dbc:Intelsat_satellites dbc:Satellites_of_Japan |
| rdf:type |
owl:Thing schema:Event dul:Event dbo:SocietalEvent wikidata:Q1656682 wikidata:Q2133344 dbo:Event dbo:SpaceMission |
| rdfs:comment |
JCSAT-3 was a geostationary communications satellite designed and manufactured by Hughes (now Boeing) on the HS-601 satellite bus. It was originally ordered by JSAT Corporation, which later merged into the SKY Perfect JSAT Group. It has a mixed Ku-band and C-band payload and operated on the 128° East longitude until it was replaced by JCSAT-3A. (en) O JCSAT-3 foi um satélite de comunicação geoestacionário japonês construído pela Hughes, ele esteve localizado na posição orbital de 128 graus de longitude leste e era operado pela JSAT Corporation. O satélite foi baseado na plataforma e sua vida útil estimada era de 12 anos. O mesmo ficou fora de serviço em fevereiro de 2007 a órbita cemitério. (pt) |
| rdfs:label |
JCSAT-3 (en) JCSAT-3 (ja) JCSAT-3 (pt) |
| owl:sameAs |
yago-res:JCSAT-3 wikidata:JCSAT-3 dbpedia-ja:JCSAT-3 dbpedia-pt:JCSAT-3 https://global.dbpedia.org/id/az1U |
| prov:wasDerivedFrom |
wikipedia-en:JCSAT-3?oldid=1105512358&ns=0 |
| foaf:isPrimaryTopicOf |
wikipedia-en:JCSAT-3 |
| foaf:name |
JCSAT-3 (en) |
| is dbo:nextMission of |
dbr:JCSAT-2 |
| is dbo:previousMission of |
dbr:JCSAT-4 |
| is dbo:wikiPageWikiLink of |
dbr:Horizons_Satellite dbr:1995_in_spaceflight dbr:Boeing_601 dbr:List_of_Atlas_launches_(1990–1999) dbr:JCSAT-2 dbr:JCSAT-4 dbr:JSAT_Corporation dbr:JSAT_(satellite_constellation) |
| is dbp:nextMission of |
dbr:JCSAT-2 |
| is dbp:previousMission of |
dbr:JCSAT-4 |
| is foaf:primaryTopic of |
wikipedia-en:JCSAT-3 |