Chollian, (Korean: 천리안, lit. Thousand Li View, clairvoyance)[2] also known as Communication, Ocean and Meteorological Satellite 1[3] (COMS-1), was a South Korean satellite which was launched on 26 June 2010 and began operations on 1 April 2011. It was operated by the Korea Aerospace Research Institute, who used it for communication, oceanography, and meteorological observation.
Mission type | Communication Oceanography Weather |
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Operator | KARI |
COSPAR ID | 2010-032A ![]() |
SATCAT no. | 36744 |
Mission duration | Planned: 7 years Final: 9 years |
Spacecraft properties | |
Bus | Eurostar-3000S |
Manufacturer | EADS Astrium |
Launch mass | 2,460 kilograms (5,420 lb) |
Power | 2.5 kilowatts |
Start of mission | |
Launch date | 26 June 2010, 21:41 (2010-06-26UTC21:41Z) UTC |
Rocket | Ariane 5 ECA |
Launch site | Kourou ELA-3 |
Contractor | Arianespace |
End of mission | |
Deactivated | 31 March 2020, 23:59 (2020-04-01UTC00:00) UTC |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 128.2° East |
Perigee altitude | 35,791 kilometres (22,239 mi)[1] |
Apogee altitude | 35,795 kilometres (22,242 mi)[1] |
Inclination | 0.03 degrees[1] |
Period | 1436.13 minutes[1] |
Epoch | 23 January 2015, 17:05:20 UTC[1] |
COMS-1 was constructed by EADS Astrium, and was based on the Eurostar-3000S satellite bus, bringing together lessons learned from Eurostar satellites and NASA-made GOES satellites respectively. It had a mass of 2,460 kilograms (5,420 lb), and carried transponders broadcasting in the D/E and K bands of the NATO-defined spectrum, or the L/S and Ka bands of the IEEE-defined spectrum respectively. Its single solar array generated a minimum of 2.5 kilowatts of power.[4]
COMS-1 was launched by Arianespace using an Ariane 5 ECA carrier rocket lifting off from ELA-3 at the Guiana Space Centre in Kourou, French Guiana. The first launch attempt occurred on 23 June 2010; the launch was scrubbed due to a problem with one of the rocket's subsystems.[5] A subsequent attempt on 24 June was also scrubbed, due to a problem with the pressurisation of the rocket's fuel tanks.[6] The launch occurred at 21:41 UTC on 26 June 2010.[6][7] The Saudi Arabian Arabsat-5A satellite was launched by the same rocket, with a SYLDA adaptor being used to separate the spacecraft. Arabsat-5A was mounted atop the SYLDA, with COMS-1 underneath it.[8]
Following launch, COMS-1 separated into a geosynchronous transfer orbit. It used an apogee motor to raise itself into geosynchronous orbit. It then underwent testing before beginning operations at a longitude of 128.2 degrees East on 1 April 2011.[9][10] Its mission was scheduled to last seven years,[4] though the satellite had a design life of ten years.[11]
COMS-1 was deactivated on 31 March 2020, following a two-year extension of its seven-year primary mission.[9]
As follow-up satellites to Chollian-1, Chollian-2A and Chollian-2B were launched in December 2018 and in February 2020 respectively.[12]
← 2009 · Orbital launches in 2010 · 2011 → | |
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Compass-G1 | Globus-1M No.12L | Progress M-04M | STS-130 (Tranquility · Cupola) | SDO | Intelsat 16 | Kosmos 2459 · Kosmos 2460 · Kosmos 2461 | GOES 15 | Yaogan 9A · Yaogan 9B · Yaogan 9C | EchoStar XIV | Soyuz TMA-18 | STS-131 (Leonardo MPLM) | CryoSat-2 | GSAT-4 | Kosmos 2462 | USA-212 | SES-1 | Kosmos 2463 | Progress M-05M | STS-132 (Rassvet · ICC-VLD) | Akatsuki · IKAROS (DCAM-1 · DCAM-2) · Shin'en · Waseda-SAT2 · Hayato · Negai ☆'' | Astra 3B · COMSATBw-2 | USA-213 | SERVIS-2 | Compass-G3 | Badr-5 | Dragon Spacecraft Qualification Unit | STSAT-2B | Shijian XII | Prisma · Picard · BPA-1 | Soyuz TMA-19 | TanDEM-X | Ofek-9 | Arabsat-5A · Chollian | Progress M-06M | EchoStar XV | Cartosat-2B · AlSat-2A · StudSat · AISSat-1 · TIsat-1 | Compass-IGSO1 | Nilesat 201 · RASCOM-QAF 1R | Yaogan 10 | USA-214 | Tian Hui 1 | Kosmos 2464 · Kosmos 2465 · Kosmos 2466 | Chinasat-6A | Gonets-M No.2 · Kosmos 2467 · Kosmos 2468 | Progress M-07M | Michibiki | USA-215 | Yaogan 11 · Zheda Pixing 1B · Zheda Pixing 1C | USA-216 | Kosmos 2469 | Chang'e 2 | Shijian 6G · Shijian 6H | Soyuz TMA-01M | XM-5 | Globalstar 73 · Globalstar 74 · Globalstar 75 · Globalstar 76 · Globalstar 77 · Globalstar 79 | Progress M-08M | Eutelsat W3B · BSat 3B | Compass-G4 | Meridian 3 | Feng Yun 3B | COSMO-4 | SkyTerra-1 | STPSat-2 · RAX · O/OREOS · FASTSAT (NanoSail-D2) · FalconSat-5 · Sara-Lily · Emma | USA-223 | Chinasat-20A | Intelsat 17 · Hylas 1 | Glonass-M No.39 · Glonass-M No.40 · Glonass-M No.41 | SpaceX COTS Demo Flight 1 · Mayflower · SMDC-ONE 1 · QbX-1 · QbX-2 · Perseus 000 · Perseus 001 · Perseus 002 · Perseus 003 | Soyuz TMA-20 | Compass-IGSO2 | GSAT-5P | KA-SAT| Alsat-2A | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |
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