Doubling the mass of a satellite would result in no change in its orbital velocity. This is because the orbital velocity of a satellite only depends on the mass of the planet it is orbiting and the radius of its orbit, but not on the satellite's own mass.
it affect the path and orbital velocity of satellite due to gravitation pull
Satellite orbital spacing refers to the distance between different satellites in orbit around the Earth. This spacing is carefully planned to prevent collisions and to optimize coverage, communication, and other functions of the satellite network. Satellite operators coordinate with each other and regulatory bodies to ensure safe and efficient use of orbital space.
A geosynchronous satellite is a satellite in geosynchronous orbit, with an orbital period the same as the Earth's rotation period.
Orbital speed of a satellite: v - orbital speed G - gravitational consatnt R - radius of earth h - height of orbit
It has to be carried there by a rocket, which takes it to the required altitude and orbital speed.
Yes, it has a satellite 220 km in diameter, the orbital period is still unknown. The satellite's name is Vanth.
Well, a satellite revolves about 80 times faster than the probe. The probe masters different situations which cause orbital problems. Escape velocity doesn't have the power that regards to the probe. Scientists assume that the satellite has the power, but others don't. The probe connects to orbital velocity and has the power to control it.
Ground telescopes and orbital satellite telescopes.
Scientists must carefully set the right orbital speed for a satellite that will be orbiting Earth, so that it will orbit correctly. The wrong speed will have the satellite move too fast, or too slow, skewing information and possibly causing the satellite to fall out of orbit and back to the planet's surface.
If the orbital radius of a satellite is doubled, its orbital velocity would decrease. This is because the gravitational force between the satellite and the planet it is orbiting would be weaker at a greater distance, requiring a lower velocity to maintain orbit.
The orbital speed would be approximately 7.63 km/s and the period would be approximately 95.59 minutes for a satellite orbiting Earth at an altitude of 1.44 x 10^3 m. These values can be calculated using the formula for orbital speed (v = β(GM/r)) and the formula for orbital period (T = 2Οβ(r^3/GM)), where G is the gravitational constant, M is the mass of Earth, and r is the altitude of the satellite above Earth's surface.