Orbital Height Of Satellite Formula

P is the orbital period.

Orbital height of satellite formula. 2 a satellite is orbiting the earth with an orbital velocity of 3200 m s. Calculates the orbital radius and period and flight velocity from the orbital altitude. R 3 897 x 10 7 m. Moon orbiting the earth.

The period of the earth as it travels around the sun is one year. You can calculate the speed of a satellite around an object using the equation. Orbit of a satellite calculator high accuracy calculation welcome guest. The equation assumes that the satellite is high enough off the ground that it orbits out of the atmosphere.

The period of a satellite is the time it takes it to make one full orbit around an object. The satellite s tendency to keep going. This is approximately 17 000 mph 27 359 kph at an altitude of 150 miles 242 kilometers. The orbit is slightly elliptical with height varying from 147 1 million km to 152 1 million km.

Shows how to calculate the orbital height of a satellite above the surface of the earth. The orbital radius can be found by rearranging the orbital velocity formula. Gravitational force of earth 6 667 x 10 11 nm 2 kgm 2 mass of earth 6x10 24 kgm radius of earth 6400 km v 86400 homework equations gm r v 2 r r h the attempt at a solution i plugged everything into the equation and got 53 583 6 for r. H is the altitude height of the object.

Mission control wishes to place a satellite in circular orbit above the earth. The equation for orbital height is derived from newton s second law. If you know the satellite s speed and the radius at which it orbits you can figure out its period. In this case you add the distance from the center of the earth to the surface of the earth 6 38 10 6 meters to the satellite s height above the earth.

Use the information below and the relationship above to calculate the t 2 r 3 ratio for the planets about the sun the moon about the earth and the moons of saturn about the planet saturn. Try this and the result is a little over 365 25 days. The orbital velocity of the international space station is 7672 m s. Orbital velocity is the velocity needed to achieve balance between gravity s pull on the satellite and the inertia of the satellite s motion.

The satellite must have a period of 12 hours. Also somewhat elliptical at perigee bottom 363 104 km at apogee top. What is the orbital radius. The orbital radius is in turn dependent upon the height of the satellite above the earth.

The orbital velocity can be found using the formula.