Delphi51 said:All circular satellite calculations begin with "centripetal force = force of gravity".
Fill in the formulas for the two forces and solve for the quantity you want.
Be sure to use the centripetal force formula with period in it since that is specified in the question.
The radius of a satellite's orbit around Earth can be calculated using the formula: r = (G * M * T^2 / 4π^2)^(1/3), where G is the gravitational constant, M is the mass of the Earth, and T is the orbital period of the satellite.
The radius of a satellite's orbit around Earth is affected by the mass of the Earth, the mass of the satellite, and the orbital period of the satellite. Other factors that can affect the radius include atmospheric drag, solar radiation pressure, and other gravitational forces from celestial bodies.
The radius of a satellite's orbit around Earth can change over time due to various factors such as atmospheric drag, solar radiation pressure, and gravitational forces from other celestial bodies. These changes can cause the orbit to either increase or decrease in size.
Yes, the radius of a satellite's orbit around Earth can be adjusted by changing the satellite's velocity. This can be done by using thrusters or gravity assists from other celestial bodies. Scientists and engineers carefully plan and execute these maneuvers to achieve the desired orbit.
The radius of a satellite's orbit around Earth is directly proportional to its speed. This means that the larger the radius, the slower the satellite's speed and vice versa. This relationship is governed by the law of conservation of angular momentum, which states that the product of an object's mass, velocity, and distance from the center of rotation remains constant.