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Modern Geomatics Technologies and Applications

                               Table 2.Characteristics of Real and hypothetical of Maule faults
                                     STRIKE    DEPTH     DIP    LENGTH     WIDTH     RAKE     SLIP
                         Maule         19        35       15      429        145       90      8.1
                       hypothetical    90        35       15      429        145       90      8.1
                        of Maule

             If the first row of the table 2Wang et al. (2012b)is used, the results will be in real mode and for the
         second row; the results will be hypothesis mode.

             4.  Results

             As  already  mentioned,  in  this  paper  five  scenarios  are  used  including  GRACE,  GRACE-FO,
         Cartwheel, Pendulum, and Helix. Our analyses showed the range-rate part. In this section, the results of
         two modes were shown. Both of them are calculated for Maule-like fault and at the same position. One is
         real strike angle of 19 degrees and the other is hypothesis angle of 90 degrees. All five charts are drawn in
         the following figures. The Figure 3 showed the range-rate changes with real strike angle of 19 degrees.
         The range-rate changes at different scenarios in a zoom manner are shown in  Figure 4. The reason for
         zooming is to have a closer look at the changing of signals occurred due to an earthquake. For a better
         result, the hypothetical of Maule is shown in Figure 5.
             In Figure 3 the GRACE and GRACE-FO mission observations have only along-track signals and as it
         can be seen in the results the signals are between [-2.5, 3]⁡× 10 . The Cartwheel mission observations
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         include  both  along-track  and  cross-track.  In  this  scenario,  the  signals  are  between  [-3,  2]⁡× 10 .  The
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         pendulum mission observations have both along-track and radial-track. The pendulum mission’s signals
         are  between  [-7,  6]⁡× 10 −4 .  The  observations  in  a  Helix  mission  are  the  combination  of  all  three
         components including along-track, cross-track and radial. In this article, the Helix scenario’s signals are
         between [-2.5, 3]⁡× 10 .
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