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Overview of Remotely Sensed Data       35

               water resources, monitoring flooding, and in agriculture, geology, and
               oceanography. These applications are made more versatile and robust
               by a large body of data spanning over three decades.

               2.3.2 SPOT Data
               Designed by the French Centre National d’Etudes Spatiales (CNES),
               SPOT was first launched into an orbit of 832 km on February 21,
               1986. This first commercial Earth observation satellite provides
               complete world coverage with stereoscopic viewing capability at a
               high spatial resolution. A number of satellites have been launched in
               this series, all having an identical set of orbital parameters, such as a
               circular, near-polar, sun-synchronous orbit with an inclination of
               98.7° (Table 2.9).
                   The payload of the first three SPOT satellites encompasses two
               identical high resolution visible (HRV) sensors that operate in either of
               two modes, panchromatic or multispectral. In the first mode, one pan-
               chromatic band is acquired over the wavelength range of 0.51 to 0.73 μm
               at a spatial resolution of 10 m. In the second mode, three multispectral
               bands are obtained at a spatial resolution of 20 m (Table 2.10). Unlike
               Landsat TM, SPOT uses the pushbroom scanning technology to minimize
               scanning duration (Fig. 2.3). Owing to the use of a linear array of 6000
               detectors, 3000 lines of imagery in the multispectral mode or 6000 lines
               of imagery in the panchromatic mode are obtained simultaneously.
               Consequently, SPOT imagery is much more geometrically reliable than
               its Landsat counterpart obtained via cross-track scanning. Furthermore,
               the scanning mirror can be tilted in steps of 0.6° by up to 27° in either
               direction away from the nadir, reaching a maximum swath width of
               80 km (Fig. 2.4). This off-nadir viewing capability brings out two
               advantages in image acquisition.
                   First, it can curtail the revisit period of the satellite from the
               nominal 26 days to a few days. If the nadir area is under cloud cover,
               it can still be sensed during the next orbit of the same day by steering
               the scanning mirror sideway toward the missed track on the ground.



                      Height             832 km
                      Inclination        98.7°
                      Repeat cycle       26 days
                      FOV                4.14°
                      Off-nadir viewing   Up to 27° in 45 steps of 0.6°
                      Orbit type         Near polar, sun synchronous
                      Equatorial crossing  10:30 a.m.

                     TABLE 2.9  Orbital Parameters and Sensor Characteristics of
                     SPOT Satellites
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