Did you use correct units? That equation assumes standard units: v in m/s, r in meters, etc.notsam said:Ok so I start with GmM/r^2=mv^2/r, and then I simplify to r= GM/v^2, solving for r I get 916025899 km
Angular Velocity of a satellite is the rate at which the satellite rotates around its axis. It is measured in radians per second and is an important factor in determining the satellite's orbit and trajectory.
Angular Velocity of a satellite can be calculated by dividing the angle of rotation by the time taken for that rotation to occur. This can be expressed as ω = Δθ/Δt, where ω is the angular velocity, Δθ is the change in angle, and Δt is the time taken.
The Angular Velocity of a satellite is affected by its distance from the center of rotation, its mass, and the amount of force acting on it. Other factors such as the shape and composition of the satellite can also have an impact.
The Angular Velocity of a satellite determines the speed at which it orbits around the body it is rotating around. A higher angular velocity means a faster orbit, while a lower angular velocity results in a slower orbit.
Yes, the Angular Velocity of a satellite can change due to various factors such as changes in gravitational force, collisions with other objects, and adjustments made by control systems on the satellite. These changes can affect the satellite's orbit and trajectory.