Research Article

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

Table 5

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

StationMean (m)RMS (m)
KinematicDynamicalKinematicDynamical

1824−0.013−0.0230.1080.077
1893−0.00100.0540.050
7090000.0560.041
7105000.0490.041
7110000.0390.038
7119−0.00100.0790.047
7237000.0510.048
7249−0.0130−0.01890.1030.081
7810000.0450.042
7811−0.001−0.0020.0930.046
7824−0.003−0.0060.0710.055
7825000.0340.036
7838000.0720.063
7839000.0500.018
7840000.0410.026
7841000.0310.022