The Influence of the Solar Radiation Pressure on the Motion of an Artificial Satellite
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This article reports an investigation of the effect of solar radiation pressure on the motion of an artificial satellite. The theory has been applied to the orbit of the Vanguard I satellite, and is found to produce significant perturbations in the perigee height of that satellite. In the case of a satellite with a large ratio of area to mass the major terms introduced by solar radiation pressure can reduce the perigee distance at the rate of 1 to 2 km per day, so that the lifetime of the satellite will become considerably shorter than it would be without this effect.
[1] P. Musen,et al. Perturbations in Perigee Height of Vanguard I , 1960, Science.