“…Recall the six orbital elements (a, e, I, ω, Ω, f), namely the semimajor axis, the eccentricity, the inclination, the argument of periapsis, the longitude of the ascending node and the true anomaly respectively, and the satellite's longitude of the ascending node (ω ⊕ ) occurs inextricably linked the Earth's celestial longitude in the frame rotating with the Earth, then the Delaunay variables (l, g, h, L, G, H) can be read as; Delhaise & Morbidelli (1993) and Rahoma (2014Rahoma ( , 2016:…”