Mission type | Earth observation |
---|---|
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]
A satellite navigation or satnav system is a system that uses satellites to provide autonomous geopositioning. A satellite navigation system with global coverage is termed global navigation satellite system (GNSS). As of 2024, four global systems are operational: the United States's Global Positioning System (GPS), Russia's Global Navigation Satellite System (GLONASS), China's BeiDou Navigation Satellite System (BDS), and the European Union's Galileo.
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