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Fig. 9 | Earth, Planets and Space

Fig. 9

From: First two-way laser ranging to a lunar orbiter: infrared observations from the Grasse station to LRO’s retro-reflector array

Fig. 9

Time series of the detrended residuals for the four successful passes. The residuals and their RMS are computed from the time of flight difference with the reconstructed LRO trajectory prediction made by the Paris Observatory Lunar Analysis Center (POLAC) and after a polynomial detrending (degree 3) to remove the remaining prediction errors

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