SUMMARY
The height of a geostationary satellite from the Earth's center is calculated to be 2.16 x 109 meters using the formula r3/T2 = GM/4π2. The period (T) for a geostationary satellite is 86,400 seconds, which corresponds to one full rotation of the Earth. This ensures that the satellite remains stationary relative to a point on the Earth's surface. The discussion clarifies the importance of using the correct orbital period for accurate calculations.
PREREQUISITES
- Understanding of gravitational constant (G = 6.67 x 10-11 N·m2/kg2)
- Knowledge of Earth's mass (M = 5.98 x 1024 kg)
- Familiarity with orbital mechanics and geostationary satellites
- Ability to perform cube root calculations
NEXT STEPS
- Research the concept of synchronous satellites and their applications
- Learn about the Lagrangian points and their significance in satellite positioning
- Explore the mathematical derivation of orbital mechanics equations
- Read about the practical implications of geostationary satellites in telecommunications
USEFUL FOR
Students studying physics, aerospace engineers, satellite communication professionals, and anyone interested in orbital mechanics and satellite technology.