JCSAT-4A: Difference between revisions
→See also: {{Portal|Spaceflight}} |
Rescuing 1 sources and tagging 0 as dead. #IABot (v1.6.1) |
||
| Line 53: | Line 53: | ||
}} |
}} |
||
'''JCSAT-4A''', previously designated '''JCSAT-6''', is a [[Japan]]ese geostationary [[communications satellite]] which is operated by [[JSAT Corporation]] (now [[SKY Perfect JSAT Group]]). It is positioned in [[geostationary orbit]] at a [[longitude]] of 124° East, from where it is used to provide broadcasting and corporate network communications to Japan.<ref>{{cite web|url=http://www.sptvjsat.com/en/business/satellite/list/jcsat_4a.html|title=JCSAT-4A|publisher=Sky Perfect JSAT Corporation|accessdate=2009-08-08}}</ref> |
'''JCSAT-4A''', previously designated '''JCSAT-6''', is a [[Japan]]ese geostationary [[communications satellite]] which is operated by [[JSAT Corporation]] (now [[SKY Perfect JSAT Group]]). It is positioned in [[geostationary orbit]] at a [[longitude]] of 124° East, from where it is used to provide broadcasting and corporate network communications to Japan.<ref>{{cite web|url=http://www.sptvjsat.com/en/business/satellite/list/jcsat_4a.html|title=JCSAT-4A|publisher=Sky Perfect JSAT Corporation|accessdate=2009-08-08|deadurl=yes|archiveurl=https://web.archive.org/web/20090713034304/http://www.sptvjsat.com/en/business/satellite/list/jcsat_4a.html|archivedate=2009-07-13|df=}}</ref> |
||
JCSAT-6 was constructed by Hughes, based on the [[HS-601]] [[satellite bus]]. It is equipped with 32 J band (IEEE Ku band) [[transponder]]s, and at launch it had a mass of {{convert|2900|kg}}, with an expected operational lifespan of fourteen and a half years<ref name="UCS">{{cite web|url=http://www.ucsusa.org/nuclear_weapons_and_global_security/space_weapons/technical_issues/ucs-satellite-database.html|title=UCS Satellite Database|publisher=Union of Concerned Scientists|date=2009-07-01|accessdate=2009-08-08}}</ref><ref name="GSP">{{cite web|url=http://space.skyrocket.de/doc_sdat/jcsat-5.htm|title=JCSat 5, 6|first=Gunter|last=Krebs|publisher=Gunter's Space Page|accessdate=2009-08-08}}</ref> |
JCSAT-6 was constructed by Hughes, based on the [[HS-601]] [[satellite bus]]. It is equipped with 32 J band (IEEE Ku band) [[transponder]]s, and at launch it had a mass of {{convert|2900|kg}}, with an expected operational lifespan of fourteen and a half years<ref name="UCS">{{cite web|url=http://www.ucsusa.org/nuclear_weapons_and_global_security/space_weapons/technical_issues/ucs-satellite-database.html|title=UCS Satellite Database|publisher=Union of Concerned Scientists|date=2009-07-01|accessdate=2009-08-08}}</ref><ref name="GSP">{{cite web|url=http://space.skyrocket.de/doc_sdat/jcsat-5.htm|title=JCSat 5, 6|first=Gunter|last=Krebs|publisher=Gunter's Space Page|accessdate=2009-08-08}}</ref> |
||
Revision as of 20:25, 18 November 2017
| Names | JCSAT-6 (order to Feb 1999) JCSAT-4A (Feb 1999 onward) |
|---|---|
| Mission type | Communication |
| Operator | SKY Perfect JSAT Group |
| COSPAR ID | 1999-006A |
| SATCAT no. | 25630 |
| Mission duration | 14+1⁄2 years (planned) |
| Spacecraft properties | |
| Bus | HS-601 |
| Manufacturer | Hughes |
| Launch mass | 2,900 kilograms (6,400 lb) |
| Start of mission | |
| Launch date | 16 February 1999, 01:45:26 UTC |
| Rocket | Atlas IIAS |
| Launch site | Cape Canaveral SLC-36A |
| Contractor | ILS |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Geostationary |
| Longitude | 124° East |
| Transponders | |
| Band | 32 Ku band |
JCSAT-4A, previously designated JCSAT-6, is a Japanese geostationary communications satellite which is operated by JSAT Corporation (now SKY Perfect JSAT Group). It is positioned in geostationary orbit at a longitude of 124° East, from where it is used to provide broadcasting and corporate network communications to Japan.[1]
JCSAT-6 was constructed by Hughes, based on the HS-601 satellite bus. It is equipped with 32 J band (IEEE Ku band) transponders, and at launch it had a mass of 2,900 kilograms (6,400 lb), with an expected operational lifespan of fourteen and a half years[2][3]
It was launched atop an Atlas IIAS carrier rocket flying from Space Launch Complex 36A at the Cape Canaveral Air Force Station. The launch occurred at 01:45:26 GMT on 16 February 1999,[4] and successfully placed JCSAT-6 into a geostationary transfer orbit. From this orbit, the satellite raised itself into a geostationary orbit using an R-4D apogee motor.[5] The final burn to complete its insertion into geosynchronous orbit occurred on 1 March 1999.[6]
See also
References
- ^ "JCSAT-4A". Sky Perfect JSAT Corporation. Archived from the original on 2009-07-13. Retrieved 2009-08-08.
{{cite web}}: Unknown parameter|deadurl=ignored (|url-status=suggested) (help) - ^ "UCS Satellite Database". Union of Concerned Scientists. 2009-07-01. Retrieved 2009-08-08.
- ^ Krebs, Gunter. "JCSat 5, 6". Gunter's Space Page. Retrieved 2009-08-08.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 2009-08-08.
- ^ Wade, Mark. "JCSAT". Encyclopedia Astronautica. Retrieved 2009-08-08.
- ^ McDowell, Jonathan. "Index". Geostationary Orbit Catalog. Jonathan's Space Page. Retrieved 2009-08-08.
 | This article about one or more communications satellites is a stub. You can help Wikipedia by expanding it. |
 | This article about one or more spacecraft of Japan is a stub. You can help Wikipedia by expanding it. |