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Its mass won't affect the orbital velocity.
The semi-major axis.
AUs
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Mars' average distance from the sun during the course of a complete orbital revolution is 141.6 million miles. That's about 52% farther than the earth's average distance from the sun.
Its mass won't affect the orbital velocity.
orbital spacing is the satellite spacing between the satellites orbiting in same frequency band
You can calculate this with Kepler's Third Law. "The square of the orbital period of a planet is directly proportional to the cube of the semi-major axis of its orbit." This is valid for other orbiting objects; in this case you can replace "planet" with "satellite". Just assume, for simplicity, that the satellite orbits Earth in a circular orbit - in this case, the "semi-major axis" is equal to the distance from Earth's center. For your calculations, remember also that if the radius is doubled, the total distance the satellite travels is also doubled.
it affect the path and orbital velocity of satellite due to gravitation pull
The semi-major axis.
AUs
The semi-major axis.
A geosynchronous satellite is a satellite in geosynchronous orbit, with an orbital period the same as the Earth's rotation period.
Because its distance from Earth is roughly 238,000 miles. The time it takes a satellite body to revolve around its central body is completely determined by the shape and size of its orbit, and has nothing to do with the size or mass of the satellite. In the case of the Earth as the central body ... -- satellites at an orbital distance of 350 km, like the International Space Station, take about 90 minutes to revolve; -- satellites at an orbital distance of about 22,000 miles are 'geosynchronous' ... they take 24 hours to revolve; -- satellites at an orbital distance of 238,000 miles, like the moon, take 27.32 days to revolve.
the distance between their "average" orbital paths is 78,341,212 Km
The speed is variable; faster while closer to the Earth, and slower further away. But the actual speed varies by the orbital distance.
The Roche limit is the orbital distance at which a satellite with no tensile strength (a "liquid" satellite) will begin to be tidally torn apart by the body it is orbiting. A real satellite can pass well within its Roche limit before being torn apart.