The earth's gravitational attraction is the centripetal force mGMe/r^2= mv^/r;
mGMe/r^2=mrw^2 gives GMe/r^3 = w^2= (2pi /T)^2.
for the circular motion of a satellite a centripetal force is requid. these force is supplied by the gravitional force between the earth and satellite this is trueall objects in the satellite is zero ie, the object in a satellite feel weightlessness
The force responsible for artificial satellites following their paths around the Earth is gravitational force. Gravity pulls the satellite towards the Earth, while its orbital velocity allows it to travel forward, creating a balance that results in a stable orbit. This interplay between gravitational pull and the satellite's inertia keeps it in a continuous path around the planet.
the moon rotates around the earth. The force keeping it in orbit around the earth aka the centripital force is caused by the gravitational force between the moon and the earth. If the gravitational force and thus the centripital force dissapeared, the moon would fly off tangent to its circular orbit
They orbit around their common centre of gravity, the orbital radius and velocity of both (centripital force) is exactly enough to overcome the force of gravity between them.
The centripetal force acts towards the center of the circular path followed by the satellite, allowing it to maintain its orbit. In the case of a satellite orbiting Earth, the force of gravity provides the centripetal force required to keep the satellite in its orbit.
yes, this ADG helps the satellite to orbit earth. This is the centripital force
the gravitational force of earth keeps the satellite(better write artificial satellite)in orbit.
for the circular motion of a satellite a centripetal force is requid. these force is supplied by the gravitional force between the earth and satellite this is trueall objects in the satellite is zero ie, the object in a satellite feel weightlessness
An artificial satellite travels in a circular orbit around the Earth due to the balance between gravitational force and its inertia. The gravitational pull from the Earth acts as the centripetal force, keeping the satellite in orbit. If the satellite moves at a constant speed, it maintains a stable trajectory, ensuring that the gravitational force is equal to the required centripetal force. This results in a perfect circular orbit, with no change in speed or altitude as long as external forces, such as atmospheric drag, are negligible.
if you mean when they do a loop-de-loop-centripital force (centrifical force dosent exist)keeps them in their seets
The force responsible for artificial satellites following their paths around the Earth is gravitational force. Gravity pulls the satellite towards the Earth, while its orbital velocity allows it to travel forward, creating a balance that results in a stable orbit. This interplay between gravitational pull and the satellite's inertia keeps it in a continuous path around the planet.
Centripetal force is found using the equation F=mv2/r m=mass v=velocity r=radius
the moon rotates around the earth. The force keeping it in orbit around the earth aka the centripital force is caused by the gravitational force between the moon and the earth. If the gravitational force and thus the centripital force dissapeared, the moon would fly off tangent to its circular orbit
The force that keeps a satellite in motion is the gravitational force of the planet it is orbiting. This force acts as a centripetal force, pulling the satellite towards the planet and keeping it in its orbit.
The gravitation of the central body. For example, for the Moon moving around the Earth, the centripetal force is the gravity between Earth and Moon.
They orbit around their common centre of gravity, the orbital radius and velocity of both (centripital force) is exactly enough to overcome the force of gravity between them.
The mass in orbit around another mass is referred to as a satellite. This can be a natural satellite, like a moon, or an artificial satellite, like a spacecraft. The gravitational pull of the larger mass keeps the satellite in orbit, balancing the gravitational force with the satellite's velocity. The specific characteristics of the orbit, such as its shape and altitude, depend on the masses involved and the initial conditions of the satellite's motion.