What factors affect the orbital energy of a satellite?
The factors affecting the orbital energy of a satellite include its altitude, gravitational potential energy, kinetic energy, and mass. Changes in orbital parameters, such as eccentricity and inclination, and external forces like atmospheric drag and gravitational perturbations, can also influence its orbital energy.
How does orbital energy change when a satellite moves to a higher orbit?
When a satellite moves to a higher orbit, its orbital energy increases. This is because both kinetic and potential energy components contribute to the total orbital energy, and potential energy increases as the satellite gains altitude, despite a decrease in kinetic energy.
How is orbital energy related to the conservation of energy in orbital mechanics?
Orbital energy, the sum of kinetic and potential energy of an orbiting body, remains constant if no external forces act on the system. This is due to the conservation of energy principle, which states that energy within a closed system cannot be created or destroyed, only transformed.
How does orbital energy influence the stability of an orbit?
Orbital energy determines stability by balancing kinetic and potential energy; stable orbits occur when energy levels support continuous motion without losing momentum. Higher orbital energy can lead to escape velocities, while too little results in decay or collision. Stable orbits like circles or ellipses have balanced energies.
What is the difference between kinetic and potential energy in orbital mechanics?
In orbital mechanics, kinetic energy is the energy of motion of an object in orbit, dependent on its velocity. Potential energy is the energy of position, determined by the object's distance from a central mass, like a planet, and is related to gravitational attraction. Together, they comprise an object's total orbital energy.