2021
DOI: 10.3319/tao.2021.11.15.02
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Atmospheric remote sensing using global navigation satellite systems: From FORMOSAT-3/COSMIC to FORMOSAT-7/COSMIC-2

Abstract: FORMOSAT-3/COSMIC global atmospheric and ionospheric investigation. (2) The rise Of FORMOSAT-7/COSMIC-2 Operational Mission. (3) First results from FORMOSAT-7/COSMIC-2.

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Cited by 7 publications
(3 citation statements)
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“…Following the success of the F3/C program, NSPO and the National Oceanic and Atmospheric Administration (NOAA) of the US launched FORMOSAT-7/COSMIC-2 (F7/C2) satellites on June 25, 2019 (Chu et al 2021). F7/ C2 constellation consists of six small satellites at an altitude of 550 km, with an inclination angle of 24 degrees, and orbiting period of about 97 min.…”
Section: Introductionmentioning
confidence: 99%
“…Following the success of the F3/C program, NSPO and the National Oceanic and Atmospheric Administration (NOAA) of the US launched FORMOSAT-7/COSMIC-2 (F7/C2) satellites on June 25, 2019 (Chu et al 2021). F7/ C2 constellation consists of six small satellites at an altitude of 550 km, with an inclination angle of 24 degrees, and orbiting period of about 97 min.…”
Section: Introductionmentioning
confidence: 99%
“…Both receive the level 0 downlink data and perform processing to level 1 and 2 products in near real-time (NRT) with the COSMIC Data Analysis and Archive Center (CDAAC) software framework [17]. The CWB additionally runs the TROPS system [18]. The DPCs are configured and maintained to provide automated processing with high availability.…”
Section: Data Processing Centersmentioning
confidence: 99%
“…After such dedicated service lasting about 14 years, far exceeding the expected mission lifetime, which saw more than 4.6 million RO profiles, the F3/C mission was officially decommissioned in May 2020. A follow-up mission named FORMOSAT-7/COSMIC-2 (F7/C2) has already been launched on 25 June 2019, which also consists of a cluster of six satellites identical to that of the F3/C, circumnavigating the Earth with a period of about 97 min from low-inclination (24 • ) orbits at an altitude of ~550 km [63]. The Tri-GNSS radio occultation system (TGRS), the main mission payload of F7/C2, receives the refracted signals from GNSS (global navigation satellite system) satellites, including GPS, GLONASS, and Galileo systems, providing many more soundings than its predecessor.…”
Section: Introductionmentioning
confidence: 99%