SUMMARY
The total mechanical energy of a 400kg satellite in a circular orbit 1100km above Earth's surface can be calculated using gravitational potential energy and kinetic energy formulas. The gravitational potential energy is given by U = -(Gm1m2)/r, while kinetic energy is calculated using k = 1/2mv^2. To find the velocity of the satellite, one must equate centripetal force to gravitational force, assuming the mass of the Earth is significantly greater than that of the satellite.
PREREQUISITES
- Understanding of gravitational potential energy and kinetic energy equations
- Familiarity with the concept of centripetal force
- Knowledge of the gravitational constant (G) and its application
- Basic principles of circular motion and orbital mechanics
NEXT STEPS
- Learn how to derive the velocity of an object in circular orbit using centripetal force
- Study the implications of gravitational potential energy in orbital mechanics
- Explore the relationship between angular velocity and linear velocity in circular motion
- Investigate the effects of altitude on gravitational potential energy
USEFUL FOR
Students studying physics, particularly those focused on mechanics and orbital dynamics, as well as educators looking for practical examples of energy calculations in satellite motion.