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2 slots was requested by the Philippine government

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βˆ™ 13y ago
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Q: How many satellite orbital slots are requested by Philippine government from ITU?
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What would be the effect on the orbital velocity of satellite if mass of satellite is double?

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.


What does perturbation do to a satellite?

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What is a geo synchronus satellite?

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How does a satellite get into the exosphere?

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Does 90482 Orcus have a moon?

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What is the difference between a satellite and a probe with regard to orbital velocity and escape velocity?

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.


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Why scientist must carefully set the right orbital speed of a satellite orbiting earth?

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.


What is the effect on the orbital velocity of the sattelite if its orbital radius is doubled?

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.


What would be the orbital speed and period of a satellite in orbit 1.44 times 10 to the power of 3m above earth?

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 = √(GM/r)) and the formula for orbital period (T = 2Ο€βˆš(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.