Selection of an orbit for communication satellite based on inclination and eccentricity

The work mainly deals with the design of a geostationary orbit for a communication satellite. The mission and requirements are determined by the ∆V budget calculation been done for four different cases and obtained the low ∆V total which will be more efficient for the fuel consumption. Six Keplerian Orbital elements and orbital perturbations for the low earth parking orbit and finally attained geostationary orbit is been calculated theoretically and shown. Further using GMAT software, the simulation of the geostationary orbit is attained and various analysis (Iterations, Differential corrector, Report and Ephemeris files, Graphs) are done based on the altitude of the orbit. In this paper a brief introduction is given for communication satellites and its importance and detailed study about various orbits which helps in obtaining a result of choosing a suitable orbit based on eccentricity and inclination classifications. Detailed explanation is given for the chosen orbit for communication satellite.