Research Article

Refinement of GRACE-FO Kinematic Orbit by Combining Least Squares Method and Orbital Dynamic Model

Table 6

Statistics of SLR check for GRACE-FO-B kinematic and dynamical orbits.

StationMean (m)RMS (m)
KinematicDynamicalKinematicDynamical

1824−0.013−0.0030.0910.038
1893−0.001100.0480.044
7090000.0550.040
7105000.0610.050
71100.00.0490.026
71190−0.0010.0360.044
7237000.0570.046
72490.013−0.0090.0680.057
78100−0.0000.0400.034
7824−0.003−0.0030.0810.057
7825000.0440.038
7838000.0700.062
7839000.0600.030
78400−0.0010.0550.041
7841000.0470.035