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Table 7

Gravitational field solutions for the strong-field dynamo case, obtained with the simulated missions adopting polar orbits of moderate eccentricity 0.5.

Coefficient Forward modeling One-month tracking solution Three-month tracking solution Five-month tracking solution
1.7000 × 10−7 1.6995 × 10−7 1.7004 × 10−7 1.7000 × 10−7
7.5000 × 10−8 7.4966 × 10−8 7.4962 × 10−8 7.4977 × 10−8
− 1.500 × 10−8 − 1.4924 × 10−8 − 1.4919 × 10−8 − 1.4937 × 10−8
6.00 × 10−9 5.8140 × 10−9 6.1041 × 10−9 5.8631 × 10−9
− 3.00 × 10−9 − 2.6508 × 10−9 − 3.5228 × 10−9 − 2.9098 × 10−9
2.00 × 10−9 1.4235 × 10−9 2.3754 × 10−9 1.9532 × 10−9

Notes. The typical flow strength in the forward modeling of the gravitational field is . The ormal uncertainty RMS quantities δn for the solutions are uniformly below 10−10.

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