At this speed, the velocity of satellite takes 1.5 hours to orbit the Earth's 24,000-mile perimeter. The astronaut does not point if he wants to land.
G is the gravitational constant, M is the mass of the attracting mass, and r is the distance from the center of that mass. This equation for the escape velocity, denoted as vesc, is written as vesc = Square root of 2GM/r.
The mass of the planet and the radius of the spacecraft's orbit path are the two factors that nature uses to calculate the speed of an orbiting spacecraft.
calculation:
velocity of satellite = 1.5 hrs
G = gravitational constant
distance = 24000 mile
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