About: JCSAT-5A

Facets (new session)
Description
Metadata
Settings
- Rule:
- Inverse Functional Properties:
- "Same As":

About: JCSAT-5A Goto Sponge NotDistinct Permalink

An Entity of Type : dbo:ArtificialSatellite, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
QRcode icon

http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FJCSAT-5A&invfp=IFP_OFF&sas=SAME_AS_OFF

JCSAT-5A or N-STAR d, known as JCSAT-9 before launch, is a geostationary communications satellite operated by SKY Perfect JSAT Group (JSAT) which was designed and manufactured by Lockheed Martin on the A2100 platform.

Attributes	Values
rdf:type	Thing schema:Event dul:Event societal event wikidata:Q1656682 wikidata:Q2133344 yago:WikicatCommunicationsSatellitesInGeostationaryOrbit yago:WikicatLockheedMartinSatellitesAndProbes yago:Artifact100021939 yago:CommunicationsSatellite103077741 yago:Equipment103294048 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 event space mission yago:Satellite104137444 yago:Whole100003553 ArtificialSatellite
rdfs:label	JCSAT-5A (en) JCSAT-5A (ja) JCSAT-9 (pt)
rdfs:comment	JCSAT-5A or N-STAR d, known as JCSAT-9 before launch, is a geostationary communications satellite operated by SKY Perfect JSAT Group (JSAT) which was designed and manufactured by Lockheed Martin on the A2100 platform. (en) O JCSAT-9 (também conhecido por JCSAT-5A e N-Star D) é um satélite de comunicação geoestacionário japonês construído pela empresa Lockheed Martin, ele está localizado na posição orbital de 132 graus de longitude leste e é operado pelas empresas NTT DoCoMo e SKY Perfect JSAT Corporation. O satélite foi baseado na plataforma A2100AXS e sua vida útil estimada é de 12 anos. (pt)
foaf:name	JCSAT-5A (en)
name	JCSAT-5A (en)
dcterms:subject	Lockheed Martin satellites and probes Communications satellites of Japan Communications satellites in geostationary orbit Satellites of Japan Satellites using the A2100 bus Spacecraft launched by Zenit and Energia rockets Spacecraft launched in 2006
Wikipage page ID	4723506 (xsd:integer)
Wikipage revision ID	1105512487 (xsd:integer)
Link from a Wikipage to another Wikipage	Coordinated Universal Time S band Geocentric orbit Geostationary orbit NTT DoCoMo NTT Docomo LEROS Lockheed Martin Lockheed Martin Space Systems Communications satellite Zenit-3SL Traveling-wave tube 2006 in spaceflight C band (IEEE) Transponder (satellite communications) Watt Launch vehicle Liquid apogee engine Lockheed Martin A2100 Lockheed Martin satellites and probes Hertz JCSAT-2A JCSAT-3A Communications satellites of Japan Asia Communications satellites in geostationary orbit Satellites of Japan Satellites using the A2100 bus Spacecraft launched by Zenit and Energia rockets Spacecraft launched in 2006 JSAT (satellite constellation) Ku band Odyssey (launch platform) Sea Launch Satellite bus Orbital maneuver Solar panels on spacecraft SKY Perfect JSAT
sameAs	JCSAT-5A JCSAT-5A JCSAT-5A JCSAT-5A JCSAT-5A JCSAT-5A
trans band	C-band: 20 x 36 MHz (en) Ku-band: 8 × 54 Mhz + 12 × 36 Mhz (en) S-band beam (en)
trans bandwidth	1584.0 (megahertz)
trans coverage	Japan, Asia (en)
trans TWTA	C-band: 45 watts (en) Ku-band: 110 watts (en) S-band: 130 watts (en)
dbp:wikiPageUsesTemplate	dbt:JCSAT dbt:Clear dbt:Cvt dbt:Infobox_spaceflight dbt:Portal dbt:Reflist dbt:Use_American_English dbt:Use_dmy_dates dbt:Orbital_launches_in_2006
spacecraft	JCSAT-5A (en)
apsis	gee (en)
COSPAR ID	2006 (xsd:integer)
image size	300 (xsd:integer)

Faceted Search & Find service v1.17_git139 as of Feb 29 2024

Alternative Linked Data Documents: ODE Content Formats:

RDF

ODATA

Microdata

About

OpenLink Virtuoso version 08.03.3330 as of Mar 19 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 59 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software