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{{infobox spaceflight |
{{infobox spaceflight |
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| name = CICERO-6 |
| name = CICERO-6 |
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| image = Fully integrated PSLV-C40 seen with Mobile Service Tower retracted.jpg |
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| image_caption = The [[Polar Satellite Launch Vehicle]], the model of rocket that launched CICERO-6 |
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| mission_type = [[Earth observation]] |
| mission_type = [[Earth observation]] |
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| operator = GeoOptics Inc. |
| operator = GeoOptics Inc. |
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| manufacturer = Orbital Solutions Monaco<ref name=nanosats.eu>{{Citation |last=Kulu|first=Erik|year=2023|title=CICERO|publisher=Nanosats Database|url=https://www.nanosats.eu/sat/cicero|access-date=14 January 2024}}</ref> |
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| manufacturer = |
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| launch_mass = {{cvt|10|kg}}<ref name=eoportal.org>{{Citation |last=Kramer|first=Herbert J.|year=2022|title=CICERO (Community Initiative for Continuing Earth Radio Occultation)|publisher=European Space Agency|publication-place=|page=|url=https://www.eoportal.org/satellite-missions/cicero|access-date=5 January 2024 }}</ref> |
| launch_mass = {{cvt|10|kg}}<ref name=eoportal.org>{{Citation |last=Kramer|first=Herbert J.|year=2022|title=CICERO (Community Initiative for Continuing Earth Radio Occultation)|publisher=European Space Agency|publication-place=|page=|url=https://www.eoportal.org/satellite-missions/cicero|access-date=5 January 2024 }}</ref> |
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| power = 21 [[watt|watts]] |
| power = 21 [[watt|watts]] |
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| launch_date = 23 June 2017, 3:59 [[Coordinated Universal Time|UTC]]<ref name=eoportal.org/> |
| launch_date = 23 June 2017, 3:59 [[Coordinated Universal Time|UTC]]<ref name=eoportal.org/> |
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| launch_rocket = [[ |
| launch_rocket = [[PSLV]]-XL |
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| launch_site = [[Sriharikota Launching Range]] |
| launch_site = [[Sriharikota Launching Range]] |
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| launch_contractor = [[ISRO]] |
| launch_contractor = [[ISRO]] |
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| orbit_period = 92.7 minutes |
| orbit_period = 92.7 minutes |
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'''CICERO-6 (Community Initiative for Continuing Earth Radio Occultation |
'''CICERO-6''' ('''Community Initiative for Continuing Earth Radio Occultation''') was a [[CubeSat]] designed and operated by GeoOptics, Inc.<ref name=nanosats.eu/> It was the first launched of the CICERO [[satellite constellation]]. Its purpose, as part of the constellation, was to use [[GPS]] and [[Galileo (satellite navigation)|Galileo]] [[radio occultation]] (GNSS-RO) and [[GNSS reflectometry]] (GNSS-R) to provide data on [[atmosphere of Earth|Earth's atmosphere]] and [[climate]].<ref name=eoportal.org/><ref>{{citation|last=Krebs|first=Gunter D.|year=2023|title=CICERO 1, ..., 12 / OSM 1 CICERO|publisher=Gunter Space Page|url=https://space.skyrocket.de/doc_sdat/cicero.htm|access-date=9 January 2024}}</ref> The CICERO project aimed to have a lower cost compared to other Earth observation projects.<ref>{{Citation |last=Yunck |first= T.P.|year= 2012|title= CICERO: Community Initiative for Continuing Earth Radio Occultation|publisher= IROWG Annual Meeting|publication-place= |page= |url= https://irowg.org/wpcms/wp-content/uploads/2013/12/yunck.pdf|access-date=9 January 2024}}</ref> |
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The satellite re-entered the atmosphere on 11 June 2024.<ref>{{cite web |url=https://www.n2yo.com/satellite/?s=42793 |title=CICERO 6 |work=N2YO.com |date=11 June 2024 |access-date=11 June 2024 }}</ref> |
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==References== |
==References== |
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{{reflist}} |
{{reflist}} |
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{{Orbital launches in 2017}} |
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[[Category:Microsatellites]] |
[[Category:Microsatellites]] |
Latest revision as of 22:30, 15 November 2024
Mission type | Earth observation |
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Operator | GeoOptics Inc. |
Spacecraft properties | |
Manufacturer | Orbital Solutions Monaco[1] |
Launch mass | 10 kg (22 lb)[2] |
Power | 21 watts |
Start of mission | |
Launch date | 23 June 2017, 3:59 UTC[2] |
Rocket | PSLV-XL |
Launch site | Sriharikota Launching Range |
Contractor | ISRO |
Orbital parameters | |
Regime | Low Earth orbit[2] |
Altitude | 505 km (314 mi) |
Periapsis altitude | 407.8 km (253.4 mi)[3] |
Apoapsis altitude | 417.1 km (259.2 mi)[3] |
Inclination | 97.1° |
Period | 92.7 minutes |
CICERO-6 (Community Initiative for Continuing Earth Radio Occultation) was a CubeSat designed and operated by GeoOptics, Inc.[1] It was the first launched of the CICERO satellite constellation. Its purpose, as part of the constellation, was to use GPS and Galileo radio occultation (GNSS-RO) and GNSS reflectometry (GNSS-R) to provide data on Earth's atmosphere and climate.[2][4] The CICERO project aimed to have a lower cost compared to other Earth observation projects.[5]
The satellite re-entered the atmosphere on 11 June 2024.[6]
References
[edit]- ^ a b Kulu, Erik (2023), CICERO, Nanosats Database, retrieved 14 January 2024
- ^ a b c d Kramer, Herbert J. (2022), CICERO (Community Initiative for Continuing Earth Radio Occultation), European Space Agency, retrieved 5 January 2024
- ^ a b CICERO 6 Satellite details 2017-036AE NORAD 42793, n2yo.com, 2017, retrieved 5 January 2024
- ^ Krebs, Gunter D. (2023), CICERO 1, ..., 12 / OSM 1 CICERO, Gunter Space Page, retrieved 9 January 2024
- ^ Yunck, T.P. (2012), CICERO: Community Initiative for Continuing Earth Radio Occultation (PDF), IROWG Annual Meeting, retrieved 9 January 2024
- ^ "CICERO 6". N2YO.com. 11 June 2024. Retrieved 11 June 2024.