Question

A 345 kg satellite is orbiting on a circular orbit 8955 km above the Earth's surface....

A 345 kg satellite is orbiting on a circular orbit 8955 km above the Earth's surface. What is the gravitational acceleration at the location of the satellite? (The mass of the Earth is 5.97×1024 kg, and the radius of the Earth is 6370 km.)?

Homework Answers

Answer #1

The numerical value of acceleration due to gravity is at a distance d above the surface of the earth is

we substitute all the values in this equation

This is the acceleration due to gravity.

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
A 160 kg satellite is orbiting on a circular orbit 7655 km above the Earth's surface....
A 160 kg satellite is orbiting on a circular orbit 7655 km above the Earth's surface. Determine the speed of the satellite. (The mass of the Earth is 5.97×1024 kg, and the radius of the Earth is 6370 km.) (in km/s)
A satellite is set to orbit at an altitude of 20200 km above the Earth's surface....
A satellite is set to orbit at an altitude of 20200 km above the Earth's surface. What is the period of the satellite in hours? (Earth radius 6.378×1066.378×106 m, Earth mass 5.97×10245.97×1024 kg, Universal Gravitational constant G=6.67×10−11m3kg−1s−2G=6.67×10−11m3kg−1s−2 ).
A satellite is orbiting Earth 1,790 m above Earth's surface. Earth has a mass of 5.97×1024...
A satellite is orbiting Earth 1,790 m above Earth's surface. Earth has a mass of 5.97×1024 kg and a radius of 6371×103 m. What is the satellite's speed? Answer in SI units, rounded to the nearest whole number. Thank youuuu
NASA launches a satellite into orbit at a height above the surface of the Earth equal...
NASA launches a satellite into orbit at a height above the surface of the Earth equal to the Earth's mean radius. The mass of the satellite is 830 kg. (Assume the Earth's mass is 5.97 1024 kg and its radius is 6.38 106 m.) (a) How long, in hours, does it take the satellite to go around the Earth once? h (b) What is the orbital speed, in m/s, of the satellite? m/s (c) How much gravitational force, in N,...
A 200 kg satellite is placed in Earth’s orbit 200 km above the surface. The Radius...
A 200 kg satellite is placed in Earth’s orbit 200 km above the surface. The Radius of Earth is 6.37 x 106 m, and the Earth’s mass is 5.98 x 1024 kg. A) Assuming a circular orbit, how long does the satellite take to complete one orbit? B) What is the satellite’s speed?
A satellite of mass 180 kg is placed into Earth orbit at a height of 700 km above the surface....
A satellite of mass 180 kg is placed into Earth orbit at a height of 700 km above the surface. (a) Assuming a circular orbit, how long does the satellite take to complete one orbit?  h (b) What is the satellite's speed?  m/s (c) Starting from the satellite on the Earth's surface, what is the minimum energy input necessary to place this satellite in orbit? Ignore air resistance but include the effect of the planet's daily rotation.
A satellite orbits the Earth uniformly in a circular orbit with a velocity of magnitude 4.00...
A satellite orbits the Earth uniformly in a circular orbit with a velocity of magnitude 4.00 km/s. Use Newton's gravitation force as the force in Newton's Law of Acceleration, using also the centripetal acceleration . Solve for radius r of the satellite's orbit in terms of v . (a) Find then the altitude of the satellite above the surface of the Earth. Earth's mass and radius are 5.9810 kg and 6.3810 km. (b) Find the time it takes the satellite...
A satellite of mass m = 2.00 ×103 kg is launched into a circular orbit of...
A satellite of mass m = 2.00 ×103 kg is launched into a circular orbit of orbital period T = 4.00 hours. Newton's gravitational constant is G = 6.67 ×10−11 N∙m2/kg2, and the mass and radius of the Earth are respectively M⨁ = 5.97 ×1024 kg and r⨁ = 6.37 ×106 m. Answer the following questions. What is the total mechanical energy (kinetic energy + potential energy) of the satellite in orbit? Take the gravitational potential energy of the satellite...
a) For a satellite to be in a circular orbit 850 km above the surface of...
a) For a satellite to be in a circular orbit 850 km above the surface of the earth, what orbital speed must it be given? b) What is the period of the orbit (in hours)?
A. At what altitude above the Earth's surface would a satellite have to be for it’s...
A. At what altitude above the Earth's surface would a satellite have to be for it’s orbital period to be equal to 24 hours? Assume the satellite is in a circular orbit. Assume a spherical, uniform density for the Earth. The Earth's mass 5.98 x 10 raised to 24kg. The Earth's radius is 6380 km B. Why would a satellite in such an orbit be a useful thing?
ADVERTISEMENT
Need Online Homework Help?

Get Answers For Free
Most questions answered within 1 hours.

Ask a Question
ADVERTISEMENT