Final answer:
The orbital velocity can be calculated using the formula V = √(GM/R), where G is the gravitational constant, M is the mass of Earth, and R is the radius of the satellite's orbit. The circular motion speed can be calculated using the formula Circular Motion Speed = 2πR/T, where R is the radius of the satellite's orbit and T is the period of the orbit.
Step-by-step explanation:
The orbital velocity is the velocity required for a satellite to maintain a circular orbit around Earth. It can be calculated using the formula:
Orbital Velocity (V) = √(GM/R)
where G is the gravitational constant, M is the mass of Earth, and R is the radius of the satellite's orbit.
In this case, the orbital velocity is given as 5129 m/s. To calculate the circular motion speed, the formula:
Circular Motion Speed = 2πR/T
can be used, where R is the radius of the satellite's orbit and T is the period of the orbit. The Earth's satellite speed and the satellite orbit analysis can be inferred from these calculations.