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870 km is its altitude according to NASA (answred bt divyansh tiwari)

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How does a satellite get into the exosphere?

It has to be carried there by a rocket, which takes it to the required altitude and orbital speed.


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 = 2π√(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.


What does the speed of a satellite depend on when orbiting earth?

The speed of a satellite orbiting Earth primarily depends on its altitude and the gravitational pull of the Earth. According to Kepler's laws of planetary motion, a satellite in a lower orbit must travel faster to counteract the stronger gravitational force compared to one in a higher orbit. The relationship can be expressed using the formula for orbital speed, which shows that speed decreases as altitude increases. Additionally, the mass of the Earth affects this gravitational force, but it remains constant for all satellites orbiting the planet.


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 is geosatelite?

A geostationary satellite is an earth-orbiting satellite, placed at an altitude of approximately 35,800 kilometers (22,300 miles) directly over the equator, that revolves in the same direction the earth rotates (west to east). A geosynchronous satellite is a satellite whose orbital track on the Earth repeats regularly over points on the Earth over time.


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 satellite orbital spacing?

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.


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

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.


What do they call the Big grass Field on an Orbiting Satellite algebra with pizzazz?

The "Big Grass Field" on an orbiting satellite is often whimsically referred to as "The Cosmic Pasture" in the realm of orbiting satellite algebra. This playful term captures the vast expanse of space, likening it to a field where celestial bodies graze in the grand tapestry of the universe. It adds a touch of flair to the otherwise technical discussion of orbital mechanics!


An object has been located orbiting the sun at a distance from the sun of 65 AU what is the approximate orbital period of this object?

The approximate orbital period of an object at a distance of 65 AU from the sun would be around 177 years. This corresponds to Kepler's third law of planetary motion, which relates the orbital period of a planet to its distance from the sun.


What is the typical altitude for a global positioning system satellite?

Orbiting at an altitude of approximately 20,200 kilometers (12,600 miles or 10,900 nautical miles; orbital radius of 26,600 km (16,500 mi or 14,400 NM)), each SV makes two complete orbits each sidereal day.[10] The ground track of each satellite therefore repeats each (sidereal) day. This is a quote from Wikipedia's article on GPS http://en.wikipedia.org/wiki/Global_Positioning_System


What is the value of orbital velocity?

The orbital velocity of an object depends on its distance from the center of mass it is orbiting. For example, the orbital velocity of the Moon around Earth is about 1 km/s, while the orbital velocity of the International Space Station (ISS) around Earth is about 8 km/s.