Calculate all possible perturbations beforehand using the solutions to two-body and three-body problems. After the calculations are complete, launch the satellite. Adjust the satellite's position as necessary.
Launch the satellite into a higher orbit. Keep the satellite around 800 kilometers from the Earth's surface. At that distance, there is an equilibrium between atmospheric drag and solar radiation.
Avoid launching the satellite into an orbit with a high level of magnetic interference. The magnetic field causes eddy currents, which produce heat in the satellite's shell. Instead, plot a course around the Earth that has minimum magnetic disturbances.