The European Remote Sensing Satellite ERS-1, launched by ESA in 1991,
carries an Active Microwave Instrument (AMI). During several phases of
its operations, ERS-1 has been operated in almost exact repeat orbits
with periods of 3 and 35 days. The data acquired during these repeat
orbits can be used to perform repeat-pass SAR interferometry, as illus
trated in Figure 1. The excellence of ERS-1's orbit and attitude contr
ol system and the high reliability of its SAR system result in excelle
nt interferograms.