Expected Interferometric Baseline Statistics for Sentinel 1
Barat, Itziar1; Duesmann, Berthyl1; Martin Serrano, Miguel Angel2

The Sentinel 1 mission calls for a very tight orbit control. The requirement is to maintain the orbit within an orbital tube of 50 meters radius (RMS). To allow the control a reference orbit has been defined and a manoeuvring strategy was derived. Based on the simulated manoeuvre strategy by ESA Flight Dynamics team, the resulting interferometric baselines have been calculated. This paper intends to show to the In-SAR users community these expected baseline statistics.