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i Detection of Smoke and Dust Aerosols Using Multi-sensor Satellite ...

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Aqua spacecrafts are operated in the A-train orbit. Therefore, OMI is selected for<br />

validating smoke <strong>and</strong> dust detection derived with MODIS measurements.<br />

6.1.1 OMI <strong>sensor</strong><br />

OMI was launched successfully on July 15, 2004 onboard Aura. The Aura<br />

spacecraft is rotating in a 705 km sun-synchronous polar orbit (98.2 0 inclination angle)<br />

with a period <strong>of</strong> approximate 100 minutes. The local equatorial crossing time is 1:45 p.m.<br />

in the ascending mode. The OMI views the Earth with a wide view angle, ±57 0 relative to<br />

nadir. The large swath, up to 2600 km in scan direction, enables OMI to achieve almost<br />

daily global coverage in 14 orbits. OMI instrument employs hyperspectral imaging in a<br />

push-broom, nadir-viewing mode to measure the solar backscatter radiation in the<br />

wavelength range from 270 to 500 nm, at a spectral resolution about 0.5 nm (Levelt et al.,<br />

2006). OMI instrument characteristics (Ahmad et al., 2003) are given in Table 6.1.<br />

Wavelength<br />

range<br />

Table 6.1: OMI instrument characteristics<br />

Item Parameter<br />

Visible 365 - 500 nm<br />

UV-1 270 to 310 nm<br />

UV-2 310 to 365 nm<br />

View angle 114 0 (±57 0 )<br />

Swath 2600 km<br />

IFOV 3 km, binned to 13 x 24 km<br />

78

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