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This paper presents a design method of an automatic test system for satellite payload, and discusses in detail the realization of each functional module in the original tracking system, with emphasis on the OCOE internal structure design, data transmission SCOE internal structure design, payload SCOE internal structure design and system workflow of the payload automatic testing system. The automatic testing system of satellite payload introduced in this paper has the characteristics of high cohesion and low precision, and supports the co-line analysis of payload data with multiple unload processing. The test results show that the system can improve the working efficiency by more than one time, avoid the adverse effects of too much manpower consumption and manual participation on the test results, and make the limited testers focus more on the load test data itself, so as to improve the accuracy and reliability of the test results.