Effect of Orbit Perturbations on the Ground Track of Low Earth Orbit Satellite

PERTURBED GROUND TRACK UNDER THE INFLUENCE OF J2 AND LUNISOLAR FORCES

A semi-analytical solution for the motion of a low altitude Earth satellite under J2-gravity and air drag perturbations

MODEL OF REFERENCE ORBIT FOR SATELLITES CONSTELLATION

Eclipses intervals for satellites in elliptical orbit under effects of solar radiation pressure and earth’s oblatness

THE EFFECT OF THE EARTH'S OBLATENESS AND ATMOSPHERIC DRAG ON AN ARTIFICIAL SATELLITE IN TERMS OF THE EULER PARAMETERS

PREDICTION OF THE ORBITAL MOTION OF AN ARTIFICIAL SATELLITE FROM RADAR MEASUREMENTS

NUMERICAL SOLUTION OF SATELLITE MOTION UNDER THE EFFECTS OF THE EARTH’S GRAVITY OF THE AXIAL SYMMETRY AND DRAG FORCE IN TERMS OF THE KS-REGULARIZED VARIABLES

VISIBILITY INTERVALS BETWEEN TWO SATELLITES ORBITS UNDER J2-GRAVITY AND DRAG FORCE

BALANCED EARTH SATELLITE ORBITS