Speed in circular orbit
m = mass of satellite
v = satellite speed
G = gravitational constant
M = mass of body being orbited
r = orbital radius
12.10 - Sample problem: speed of an orbiting satellite
The illustration above shows a satellite in circular orbit 500 km above the Earth’s surface. The Earth’s radius is stated in the variables table.
Variables
What is the strategy?
- Determine the satellite’s orbital radius, which is its distance from the center of the body being orbited.
- Use the orbital speed equation to determine the satellite’s speed.
Physics principles and equations
The equation for orbital speed is
What is the speed of a satellite in
circular orbit 500 kilometers above
the Earth's surface?
satellite speed v
satellite orbital radius r
satellite height h = 500 km
Earth’s radius rE = 6.38×10^6 m
Earth’s mass ME = 5.97×10^24 kg
gravitational constant G = 6.67×10í^11 N·m^2 /kg^2
(^230) Copyright 2000-2007 Kinetic Books Co. Chapter 12