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Fig. 10
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Comparison of the latest two versions of the DE, EPM, and INPOP ephemerides and our final FORCES-8-BARY-2024 (F8B24) solution for NSB orbit. Geocentric positional differences in the ICRF are presented in right ascension (α), declination (δ), and range (D) directions. The norm of the 3D differences (Δd) are also shown.
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