Koreasat 1: Difference between revisions
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{{Short description|South Korean communications satellite launched in 2017}} |
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{{Infobox spaceflight |
{{Infobox spaceflight |
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| name = Koreasat 1 |
| name = Koreasat 1 |
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| image = |
| image = |
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| image_caption = |
| image_caption = |
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| insignia = |
| insignia = |
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| mission_type = |
| mission_type = [[Communications]] |
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⚫ | |||
[[Software]] |
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| website = |
| website = |
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| COSPAR_ID = 1995-041A |
| COSPAR_ID = 1995-041A |
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| launch_site = [[Cape Canaveral Air Force Station|Cape Canaveral]] [[Cape Canaveral Air Force Station Launch Complex 17|LC-17B]]<ref name=astronautix/> |
| launch_site = [[Cape Canaveral Air Force Station|Cape Canaveral]] [[Cape Canaveral Air Force Station Launch Complex 17|LC-17B]]<ref name=astronautix/> |
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| launch_contractor = |
| launch_contractor = |
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| disposal_type = Decommissioned |
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| deactivated = {{end-date|December 16, 2005}} |
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| last_contact = |
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| decay_date = |
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| orbit_epoch = {{start-date|August 5, 1995}} |
| orbit_epoch = {{start-date|August 5, 1995}} |
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| trans_HPBW = |
| trans_HPBW = |
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}} |
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'''Koreasat 1''' was a South Korean |
'''Koreasat 1''' was a South Korean [[communications]] satellite launched by a [[Delta II]] rocket from [[Cape Canaveral Air Force Station]], [[Florida]], United States. Owned by [[KT Corporation]].<ref>{{Cite web |url=http://www.absatellite.com/2010/05/24/asia-broadcast-satellite-acquires-koreasat-3/ |title=Asia Broadcast Satellite Acquires Koreasat-3 |access-date=2017-10-21 |archive-date=2017-10-22 |archive-url=https://web.archive.org/web/20171022033541/http://www.absatellite.com/2010/05/24/asia-broadcast-satellite-acquires-koreasat-3/ |url-status=dead }}</ref> |
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One of the boosters of the [[Delta II]] rocket failed to separate from the first stage of the spacecraft, placing it 5,000 km short of its planned GTO apogee. The satellite had to use up 7.5 years worth of its 12-year lifetime fuel supply to make up the deficiency, shortening Koreasat 1's expected life to about 4.5 years. In order to extend its lifetime, it gave up north–south station-keeping operating in "inclined mode." In the end, the satellite managed to function for 10 years.<ref name=nssdc>{{cite web |url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1995-041A |title=Koreasat 1 |last=NASA |first=GSFC |accessdate=May 5, 2017}}</ref> |
One of the boosters of the [[Delta II]] rocket failed to separate from the first stage of the spacecraft, placing it 5,000 km short of its planned GTO apogee. The satellite had to use up 7.5 years worth of its 12-year lifetime fuel supply to make up the deficiency, shortening Koreasat 1's expected life to about 4.5 years. In order to extend its lifetime, it gave up north–south station-keeping operating in "inclined mode." In the end, the satellite managed to function for 10 years.<ref name=nssdc>{{cite web |url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1995-041A |title=Koreasat 1 |last=NASA |first=GSFC |accessdate=May 5, 2017}}</ref> |
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The satellite was equipped with a '''Star 30''' solid apogee motor. It carried {{convert|625|kg|lb|abbr=on}} of fuel for the apogee motor and {{convert|187|kg|lb|abbr=on}} of [[hydrazine]] propellant.<ref name=tbs>{{cite web |url=https://www.tbs-satellite.com/tse/online/sat_koreasat_1.html|title=Koreasat 1 |last=TBS |accessdate=May 5, 2017}}</ref> |
The satellite was equipped with a '''Star 30''' solid apogee motor. It carried {{convert|625|kg|lb|abbr=on}} of fuel for the apogee motor and {{convert|187|kg|lb|abbr=on}} of [[hydrazine]] propellant.<ref name=tbs>{{cite web |url=https://www.tbs-satellite.com/tse/online/sat_koreasat_1.html|title=Koreasat 1 |last=TBS |accessdate=May 5, 2017}}</ref> |
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It was eventually positioned in [[geosynchronous orbit]] at 116° E |
It was eventually positioned in [[geosynchronous orbit]] at 116° E operated it at 47.5° E where it was focused on Hungary. The satellite went out of service on December 16, 2005, and was moved to the [[graveyard orbit]]. As of March 9, 2007, it was located at 152.88° E drifting at 2.155° W per day.<ref name=astronautix>{{cite web |url=http://www.astronautix.com/k/koreasat.html|archive-url=https://web.archive.org/web/20161228152510/http://astronautix.com/k/koreasat.html|url-status=live|archive-date=December 28, 2016|title=Koreasat |last= Wade|first= Mark|accessdate=May 5, 2017}}</ref> |
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== See also == |
== See also == |
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== External links == |
== External links == |
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* {{cite web|url=https://www.ktsat.com/mainPage.do|title=KT Sat|access-date=January 3, 2023}} |
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* [http://csplab.kaist.ac.kr/lecture/SatRec2007/lecture_notes/EE807_070522.pdf THE KOREASAT PROGRAM]{{Dead link|date=February 2020 |bot=InternetArchiveBot |fix-attempted=yes }} (pdf) |
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{{Use American English|date=May 2017}} |
{{Use American English|date=May 2017}} |
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{{Orbital launches in 1995}} |
{{Orbital launches in 1995}} |
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[[Category:Communications satellites]] |
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[[Category:Satellites of South Korea]] |
[[Category:Satellites of South Korea]] |
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[[Category: |
[[Category:Communications satellites]] |
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[[Category:Satellite launch anomalies]] |
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[[Category:Spacecraft launched in 1995]] |
[[Category:Spacecraft launched in 1995]] |
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[[Category:1995 in spaceflight]] |
[[Category:1995 in spaceflight]] |
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[[Category:1995 in South Korea]] |
[[Category:1995 in South Korea]] |
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[[Category:Spacecraft launched by Delta II rockets]] |
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Latest revision as of 01:41, 25 March 2024
Mission type | Communications |
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Operator | KT Corporation |
COSPAR ID | 1995-041A |
SATCAT no. | 23639 |
Mission duration | 10 years |
Spacecraft properties | |
Bus | AS-3000 |
Manufacturer | Martin Marietta / Lockheed Martin |
Launch mass | 1,464 kilograms (3,228 lb)[1] |
Dry mass | 711 kilograms (1,567 lb)[1] |
Start of mission | |
Launch date | August 5, 1995, 11:10[1] | UTC
Rocket | Delta II 7925 |
Launch site | Cape Canaveral LC-17B[2] |
End of mission | |
Disposal | Decommissioned |
Deactivated | December 16, 2005 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 116° E |
Perigee altitude | 35,776 kilometers (22,230 mi)[2] |
Apogee altitude | 35,796 kilometers (22,243 mi)[2] |
Inclination | 2.7°[2] |
Period | 1,436.1 minutes[2] |
Epoch | August 5, 1995 |
Transponders | |
Band | 12 FSS Ku band, 3 BSS Ku band |
Bandwidth | 36 MHz, 27 MHz |
Coverage area | South Korea, Asia, |
Koreasat 1 was a South Korean communications satellite launched by a Delta II rocket from Cape Canaveral Air Force Station, Florida, United States. Owned by KT Corporation.[3]
One of the boosters of the Delta II rocket failed to separate from the first stage of the spacecraft, placing it 5,000 km short of its planned GTO apogee. The satellite had to use up 7.5 years worth of its 12-year lifetime fuel supply to make up the deficiency, shortening Koreasat 1's expected life to about 4.5 years. In order to extend its lifetime, it gave up north–south station-keeping operating in "inclined mode." In the end, the satellite managed to function for 10 years.[4]
The satellite was equipped with a Star 30 solid apogee motor. It carried 625 kg (1,378 lb) of fuel for the apogee motor and 187 kg (412 lb) of hydrazine propellant.[5]
It was eventually positioned in geosynchronous orbit at 116° E operated it at 47.5° E where it was focused on Hungary. The satellite went out of service on December 16, 2005, and was moved to the graveyard orbit. As of March 9, 2007, it was located at 152.88° E drifting at 2.155° W per day.[2]
See also
[edit]References
[edit]- ^ a b c Gunter, Krebs. "Koreasat 1, 2". Retrieved May 4, 2017.
- ^ a b c d e f Wade, Mark. "Koreasat". Archived from the original on December 28, 2016. Retrieved May 5, 2017.
- ^ "Asia Broadcast Satellite Acquires Koreasat-3". Archived from the original on 2017-10-22. Retrieved 2017-10-21.
- ^ NASA, GSFC. "Koreasat 1". Retrieved May 5, 2017.
- ^ TBS. "Koreasat 1". Retrieved May 5, 2017.
External links
[edit]- "KT Sat". Retrieved January 3, 2023.