CICERO-6

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CICERO-6
Fully integrated PSLV-C40 seen with Mobile Service Tower retracted.jpg
The Polar Satellite Launch Vehicle, the model of rocket that launched CICERO-6
Mission type Earth observation
OperatorGeoOptics Inc.
Spacecraft properties
ManufacturerOrbital Solutions Monaco [1]
Launch mass10 kg (22 lb) [2]
Power21 watts
Start of mission
Launch date23 June 2017, 3:59 UTC [2]
Rocket PSLV-XL
Launch site Sriharikota Launching Range
Contractor ISRO
Orbital parameters
Regime Low Earth orbit [2]
Altitude505 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]

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References

  1. 1 2 Kulu, Erik (2023), CICERO, Nanosats Database, retrieved 14 January 2024
  2. 1 2 3 4 Kramer, Herbert J. (2022), CICERO (Community Initiative for Continuing Earth Radio Occultation), European Space Agency, retrieved 5 January 2024
  3. 1 2 CICERO 6 Satellite details 2017-036AE NORAD 42793, n2yo.com, 2017, retrieved 5 January 2024
  4. Krebs, Gunter D. (2023), CICERO 1, ..., 12 / OSM 1 CICERO, Gunter Space Page, retrieved 9 January 2024
  5. Yunck, T.P. (2012), CICERO: Community Initiative for Continuing Earth Radio Occultation (PDF), IROWG Annual Meeting, retrieved 9 January 2024
  6. "CICERO 6". N2YO.com. 11 June 2024. Retrieved 11 June 2024.