SUMMARY
Satellites maintain their orbits due to the balance between centripetal force and gravitational force, with gravity providing the necessary centripetal force for circular motion. In a circular orbit, the centripetal force is calculated as mv²/r, while the gravitational force is given by GMm/r², leading to the relationship v²=GM/r. It is crucial to understand that satellites are not in equilibrium; they are in constant acceleration towards the Earth. The concept of centrifugal force is a pseudo force that arises only in non-inertial frames of reference and does not play a role in the dynamics of satellite motion.
PREREQUISITES
- Understanding of Newton's laws of motion
- Familiarity with gravitational force and centripetal force concepts
- Knowledge of kinematics and dynamics in physics
- Concept of inertial vs. non-inertial frames of reference
NEXT STEPS
- Study the derivation of centripetal force in circular motion
- Explore the implications of Newton's law of gravitation
- Learn about elliptical orbits and their characteristics
- Investigate the differences between inertial and non-inertial frames of reference
USEFUL FOR
Students of physics, educators teaching orbital mechanics, and anyone interested in understanding the principles of satellite motion and gravitational interactions.