Modal Analysis is a method for finding a structure’s vibration properties, such as natural frequencies, mode shapes and damping factors also known as Modal Parameters. Modal analysis allows the structure to vibrate at particular frequency. Modal analysis has been widely used in Vibration troubleshooting, structural dynamics modification, Vibration control and vibration-based health monitoring in various engineering domains such as aerospace, mechanical and civil. For determining the modes of a vibrating structure, impact modal testing is currently a common approach. In this paper, two composite plates were fabricated by using E-glass fiber mat and Isopthalic polyester resin of 3 ply and 5 ply of stacking sequence (0°/0°/0°) and (0°/0°/0°/0°/0°) with dimensions 330 × 330 × 3 mm and 330 × 330 × 6.5 mm.The purpose of this study is to use the Roving Impact Hammer Test to undertake Experimental Modal Testing of a composite plate with boundary conditions C-F-C-F and C-F-F-F. The experimental approach included a 3 ply and 5 ply composite laminate construction, an impact hammer and an accelerometer to provide an excitation force and quantify the response. The vibration response of the composite laminate plate extracted using an 8 channel DAQ. The SAMURAI software was used to evaluate the frequency response functions (FRF’S). The laminated composite plate was modelled in ME’scope software, and FRF data from SAMURAI was imported into ME’scope software followed by an alternative mode forms of the specific composite plate. Experimental Modal Testing results are validated using standard ANSYS-APDL software.