Precise Orbit Determination of the MESSENGER Spacecraft
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This dataset contains the reconstructed trajectory of NASA's MESSENGER spacecraft (SPK SPICE kernel), derived using a refined dynamical model that includes thermal recoil accelerations. Auxiliary information for each trajectory arc (e.g., start and end epoch) is provided in a companion text file. Citation. Andolfo, S., Genova, A., & Del Vecchio, E. (2024). Precise orbit determination of the messenger spacecraft. Journal of Guidance, Control, and Dynamics, 47(3), 518-530. https://doi.org/10.2514/1.G007690
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Zenodo创建时间：
2025-09-04
