A satellite consists of various components, part of which includes electronic housing whose prime function is to protect the electronic components structurally. This paper mainly focuses on the structural analysis of the electronic housing of a satellite as it undergoes a specific amount of load in real flight conditions. This helps to estimate the margin of safety of different materials in a situation which replicates loads being applied in three cartesian coordinate directions which are x, y and z respectively. The end results were obtained by performing simulations, which were carried out using commercial software ANSYS Workbench.