2. (25 points) Compute the orbital inclination of an Earth satellite in a 500 km circular orbit w...
Problem 3) The space shuttle is in a circular orbit of 180 km altitude and inclination 30o. What is the change in east longitude (AX) of the ascending node after 1 orbit of the satellite? (answer in radians) Hint: ёл-(w Earth-A)nT for n orbits
Problem 3) The space shuttle is in a circular orbit of 180 km altitude and inclination 30o. What is the change in east longitude (AX) of the ascending node after 1 orbit of the satellite? (answer...
Derive the "Clarke radius", the altitude above the surface of the Earth where a satellite in a circular orbit has an orbital period of exactly one day. Assume a spherical Earth, and use the following constants (taken from Vallado, David A., Fundamentals of Astrodynamics and Applications, 2nd ed. 2001) Gravitational constant: G 6.673 x 10-20 km Radius of the Earth: Re = 6378.137 km 1024 kg Mass of the Earth: Me = 5.9733328 x Round your final answer to four...
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 502 km above the earth’s surface, while that for satellite B is at a height of 747 km. Find the orbital speed for (a) satellite A and (b) satellite B.
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 460 km above the earth’s surface, while that for satellite B is at a height of 774 km. Find the orbital speed for (a) satellite A and (b) satellite B.
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 364 km above the earth's surface, while that for satellite B is at a height of 880. km. Find the orbital speed for satellite A and satellite B. (a) VA = (b) VB =
An artificial satellite circles the Earth in a circular orbit at a location where the acceleration due to gravity is 9.00 m/s^2. Determine the orbital period of the satellite. I_o, a satellite of Jupiter, has an orbital period of 1.77 days and an orbital radius of 4.22 times 10^5 km. From these data, determine the mass of Jupiter. A minimum-energy transfer orbit to an outer planet consists of putting a spacecraft on an elliptical trajectory with the departure planet corresponding...
What must be the orbital speed of a satellite in a circular orbit 270 km above the surface of the moon? Answer in km/s
A satellite of mass 210 kg is placed into Earth orbit at a height of 500 km above the surface. (a) Assuming a circular orbit, how long does the satellite take to complete one orbit? (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 in a circular orbit 500 miles above the surface of
the Earth. What is the period of the orbit? You may use the
following constants:
Radius of the Earth: 4000 miles
Gravitational Constant: 66710?11m3(kgs2)
Mass of earth: 5981024kg
Number of Meters in a mile: 1609
Period= ? seconds
+-6.66 points HRW10 4.PO56 An Earth satellite moves in a circular orbit 759 km above the Earth's surface. The period of the motion is 99.8 min. (a) What is the speed of the satellite? m/s (b) What is the magnitude of the centripetal acceleration of the satellite? m/s2 Additional Materials Section 4.5 H Aigebra Squareroots & Squares