Question

2. Calculate the speed of a Satellite moving in a stable circular orbit 6800 Km above...

2. Calculate the speed of a Satellite moving in a stable circular orbit 6800 Km above the Earth.

Homework Answers

Answer #1

Speed of the satellite is 5459.5 m/s

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) 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 satellite in a stable circular orbit around the earth, traveling 2.3 x 10 ^ 2...
a satellite in a stable circular orbit around the earth, traveling 2.3 x 10 ^ 2 km above the ocean, has a period of:
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 1000-kg satellite in circular orbit around the Earth is moving at a speed of 7
A 1000-kg satellite in circular orbit around the Earth is moving at a speed of 7
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.)?
A satellite is in circular orbit at an altitude of 1800 km above the surface of...
A satellite is in circular orbit at an altitude of 1800 km above the surface of a nonrotating planet with an orbital speed of 3.7 km/s. The minimum speed needed to escape from the surface of the planet is 8.4 km/s, and G = 6.67 × 10-11 N · m2/kg2. The orbital period of the satellite is closest to 59 min. 83 min. 75 min. 67 min. 51 min.
a) What linear speed must an Earth satellite have to be in a circular orbit at...
a) What linear speed must an Earth satellite have to be in a circular orbit at an altitude of 141 km above Earth's surface? (b) What is the period of revolution?
1. A satellite is in a circular orbit about the earth (ME = 5.98 x 1024...
1. A satellite is in a circular orbit about the earth (ME = 5.98 x 1024 kg). The period of the satellite is 2.35 x 104 s. What is the speed at which the satellite travels? 2. Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 545 km above the earth’s surface, while that for satellite B is at a height of 787 km. Find the orbital speed for (a)...
A satellite is in circular orbit at an altitude of 1500 km above the surface of...
A satellite is in circular orbit at an altitude of 1500 km above the surface of a nonrotating planet with an orbital speed of 3.4 km/s. The minimum speed needed to escape from the surface of the planet is 8 km/s, and G = 6.67 × 10-11 N · m2/kg2. The orbital period of the satellite is closest to A)59 min. B)45 min. C)72 min. D)65 min. E)52 min.
A 400 kg satellite is in a circular orbit at an altitude of 550 km above...
A 400 kg satellite is in a circular orbit at an altitude of 550 km above the Earth's surface. Because of air friction, the satellite eventually falls to the Earth's surface, where it hits the ground with a speed of 1.90 km/s. How much energy was transformed into internal energy by means of air friction? J
ADVERTISEMENT
Need Online Homework Help?

Get Answers For Free
Most questions answered within 1 hours.

Ask a Question
ADVERTISEMENT