Plasma variations in geospace environment driven by the solar wind-magnetosphere interaction is one of the major causes of satellite anomaly. To mitigate the effect of satellite anomaly, risk of space weather disturbances needs to be known in advance based on space weather forecast. However, risk of satellite anomaly due to space weather disturbances is not the same as each satellite, because the risk depends not only on the space environment itself but also on the design and materials of individual satellite. For the viewpoint of satellite operator, it is not easy to apply general alert level of space environment to the risk of individual satellite. To provide tailored space weather information, we have developed SECURES (Space Environment Customized Risk Estimation for Satellite) by combining models of space environment and those of spacecraft charging. In SECURES, we are focusing on the risk of spacecraft charging (surface/internal) for geosynchronous satellites. For risk estimation of surface charging, we have combined the global magnetosphere MHD model with the satellite surface charging models. For risk estimation of internal charging, we have combined the radiation belt models with the satellite internal charging models. We have developed prototype products for both types of charging/ESD. The development of SECURES and our achievements are introduced in this paper.