A comet has the greatest potential energy at its farthest point from the Sun, known as aphelion. At this location, the gravitational pull of the Sun is weaker, and the comet is at its maximum distance from the Sun. As the comet moves closer to the Sun in its elliptical orbit, its potential energy decreases while its kinetic energy increases due to the gravitational attraction.
In an elliptical orbit, a satellite has its greatest total energy at the point known as apogee, which is the farthest point from the central body it is orbiting. Total energy in an orbital system is the sum of kinetic and potential energy, and at apogee, the satellite's potential energy is maximized due to its distance from the central body. However, it's important to note that total energy remains constant throughout the orbit; it is the distribution between kinetic and potential energy that changes.
If you're talking about valence shells, it would be the first. The closest one to the nucleus of an atom has the most amount of POTENTIAL energy. It requires some sort of chemical or magnetic action to get the energy.
Gravity, together with the planet's total kinetic and potential energy, completely determines the size and shape of the orbit.
A comet.
The force that keeps a comet in orbit around a larger celestial body, like the sun, is gravity. The gravitational pull between the comet and the larger body keeps the comet moving in a curved path around it.
A comet has the most potential energy at its farthest point from the sun (aphelion) in its elliptical orbit. At this point, the comet's gravitational potential energy is maximized due to the distance from the sun being at its greatest.
The total energy of a satellite doesn't change. At its closest approach to the planet, it has the most kinetic energy and the least potential, whereas at its furthest retreat from the planet, it has the least kinetic energy and the most potential. But their sum ... the satellite's total mechanical energy ... is always the same. (It may gain heat energy when the sun is shining directly on it, and lose it when it's in the planet's cold shadow, but neither of those changes affects its orbit.)
In an elliptical orbit, a satellite has its greatest total energy at the point known as apogee, which is the farthest point from the central body it is orbiting. Total energy in an orbital system is the sum of kinetic and potential energy, and at apogee, the satellite's potential energy is maximized due to its distance from the central body. However, it's important to note that total energy remains constant throughout the orbit; it is the distribution between kinetic and potential energy that changes.
If you're talking about valence shells, it would be the first. The closest one to the nucleus of an atom has the most amount of POTENTIAL energy. It requires some sort of chemical or magnetic action to get the energy.
Actually a comet dosen't have energy to move. The reason it moves is because it orbits around the sun like the planets do. The gravity from the sun keeps it orbit.
in orbit.
A planet or comet's orbit that is farthest from the sun is called the aphelion. This is the point where they are at their greatest distance from the sun in their elliptical orbit.
A comets orbit is considered a cycle because a comet circles back in an elliptical orbit.
A comets orbit is considered a cycle because a comet circles back in an elliptical orbit.
It is called an orbit. A comet has an eccentric or parabolic orbit.
our earth would be then fried, becasue the orbit of a comet orbits around the sun which cause the comet to be insanely high. which in one case would fry our earth if our orbit was near the sun
An orbit