In this paper, a detailed thermal model of the radiometer onboard a geostationary satellite is established and transient analyses are performed to obtain the temperature response of a scan mirror and a telescope secondary mirror assembly. The temperature distributions of the radiometer instruments are calculated based on an advanced finite difference method with control volume approach, which can deal with the radiation boundary condition efficiently. Oppenheim's method is used to calculate the radiation heat transfer inside the radiometer, and the calculation of radiation view factor of boundary surface is based on a blockage criterion. The thermal control design for the radiometer is presented, which contributes to its channel registration and focus stability. The thermal consideration for the scan mirror is discussed to obtain acceptable temperature range, which directly affects the performance of the radiometer. The results show that the scan mirror temperature can be reduced to a low level, obviously after appropriate structure design is adopted and a thermal coating is applied on it. The peak temperature of the scan mirror and secondary mirror assembly occurs during the period of the local middle night when they are exposed to the direct view of the sun. The temperature variations of radiometer key instruments are given for several typical solar declinations. Nomenclature A = area, m 2 A 0 = illuminated area of surface element, m 2 c = heat capacity, J=kg K F, F s = view factors, dimensionless G = conductance between calculation points, W=K g = conductance between boundary elements, W=K k = thermal conductivity, W=m 2 K L = length of boundary element, m Q = heat flow, W Q b = heat flow across the control volume boundary, W Q 0 = heat generated within the control volume, W q = heat flow across boundary, W q s = solar constant, W=m 2 R = distance between two surfaces, m T = temperature, K t = time, s U = internal energy, J V = volume, m 3 x, y, z = coordinates, m , , = angle between the normal vector and the axis of coordinates, deg = element thickness, m " = emissivity, , dimensionless = angle between the element surface normal and the solar vector, deg = density, kg=m 3 = Stefan-Boltzmann constant, W=m 2 K 4 = angle between the element surface normal and the connecting line, deg Subscripts b = boundary element CG = element center (center of gravity) i, j = ith and jth element or calculation point