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RESEARCH ANNOUNCEMENT PRODUCTS EXAMPLES OF APPLICATIONS
 
VENµS 
MISSION 
Near polar sun synchronous orbit, altitude 720 km, inclination 98.27°
Revisit time: two days
Swath : 27.5 km
Camera spatial resolution : 5 m
Number of spectral bands : 12 (VIS-NIR)
Tilting capability : ± 30° across and along track
Constant viewing angle
Lifetime : 3.5 years
 
Satellite acquisition capabilities
Picto video VENµS acquisition capabilities [5 Mb] 7 or +

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To fulfill its scientific objectives, VENµS has to acquire frequent, high resolution, multi-spectral images of sites of interest all around the world. The satellite will fly in a near polar sun-synchronous orbit at 720 km height. The whole system will be able to be tilted up to 30 degree along and across track. This configuration will result in a 2-days revisit time, 27 km swath, a camera resolution of 5.3 m, and the capability to observe any site under a constant view angle. The system will cross the equator at around 10:30 AM.

Possible orbits Possible orbits Details
Possible coverage of VENµS
Nadir in yellow, Tilted viewing in grey, no coverage in blue
Closer view of possible coverage

The satellite will carry a super-spectral camera characterized by 12 narrow spectral bands ranging from 415 nm to 910 nm. The band setting was designed to characterize vegetation status, including through red-edge bands, and to estimate the aerosol optical depth and the water vapour content of the atmosphere for accurate atmospheric corrections. The spectral band setting could also prove useful for coastal areas and inland waters studies.

The data will be acquired over existing or planned experimental sites with size ranging from 27 x 27 km² kilometres to 27 x 54 km² or more. All data for a given site will be acquired with the same observation angle in order to minimize directional effects. The baseline product for these selected sites is time composite images of geometrically registered surface reflectances at 10 m resolution. Strong efforts are devoted to provide high quality data, both in term of radiometry (e.g. SNR around 100), geometry (e.g. multitemporal registration better than 3 m), and atmospheric corrections.

The VENµS scientific mission is planned for at least two years and a half and will be followed by the technological mission for a duration of one year.

Mission Timeline


Latest update 02/02/2007