Mehdi Eshagh, M. Najafi Alamdari
Abstract
The main point of this paper is to evaluate the perturbations in orbital elements of a low Earth orbiting satellite. The outcome of a numerical orbit integration process is the position and velocit ...
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The main point of this paper is to evaluate the perturbations in orbital elements of a low Earth orbiting satellite. The outcome of a numerical orbit integration process is the position and velocit ...
Key concepts: Orbital elements, Satellite, Low earth orbit, Frozen orbit, Medium Earth orbit, Orbit (dynamics), Geocentric orbit, Orbital mechanics