Can you help me with the MATALB code? From the initial time of the orbital state vector of the ISS propagate numerically and compute the effect of third-body perturbations, drag and SRP on its orbit over 10 revolutions. You may use JPL ephemerides or SPICE/MICE.

Can you help me with the MATALB code? From the initial time of the orbital state vector of the ISS propagate numerically and compute the effect of third-body perturbations, drag and SRP on its orbit over 10 revolutions. You may use JPL ephemerides or SPICE/MICE.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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