The success of on-line deployment of satellite solar wings is a critical factor influencing their operational performance, and the ground deployment test of satellite solar wings serves as a crucial development step to verify the deployment and locking performance of the mechanism and ensure the compliance of deployment indicators. To address the challenges such as limited data monitoring, low simulation accuracy, and difficulties in predicting outcomes in the process of satellite solar wing ground deployment testing, a digital twin-driven simulation and prediction method along with a system architecture for satellite solar wing ground deployment testing was proposed. Based on the digital twin modeling of typical satellite solar wing products, related tooling and equipment for ground deployment testing, and deployment testing units, a multidisciplinary joint simulation for satellite solar wing ground deployment testing was conducted, and a simulation database was output. A prediction model training dataset was constructed by combining the simulation data and historical test data. Subsequently, the training and optimization of the satellite solar wing deployment process prediction model were completed. Through the real-time collection of key parameters in the ground deployment testing process via the Internet of Things platform, inputting these parameters into the optimized key parameter prediction model, the rapid and accurate prediction of key parameters such as pose, force, velocity, and deployment time in the satellite solar wing ground deployment testing process were achieved. Finally, based on the digital twin model, by integrating the actually collected and predicted data, the real-time monitoring of the mechanism deployment process and the visualization of prediction results were realized. This approach supported the intelligent management and control and decision-making in the satellite solar wing ground deployment testing process, guided the optimization of the deployment process and on-site adjustments, and effectively enhanced the deployment success rate and efficiency. Through the deployment in the satellite deployment unit and the application verification on typical satellite models, the proposed method achieved an online prediction accuracy rate of over 90% for key parameters such as the deployment time and pose of typical solar wings, verifying its effectiveness and feasibility.