Kepler 3



Kepler third law

Astronomy Ranking Task: Kepler’s Laws – Orbital Motion Exercise #3 Description: The figure below shows a star and five orbiting planets (A – E). Note that planets A, B and C are in perfectly circular orbits. In contrast, planets D and E have more elliptical orbits. Note that the closest and farthest distances for the elliptical orbits of planets D and E happen to match the orbital. 2) The Moon orbits the Earth at a center-to-center distance of 3.86 x10 5 kilometers (3.86 x10 8 meters). Now, look at the graphic with the formulas and you will see that the 'm' in the formula stands for the mass of both orbital bodies.Usually, the mass of one is insignificant compared to the other.However, since the Moon's mass is about ⅟81 that of the Earth's, it is important that we use. Eclipse IDE Kepler SR2 Packages. Eclipse Standard 4.3.2. 201 MB; 5,489,203 DOWNLOADS; The Eclipse Platform, and all the tools needed to develop and debug it: Java and Plug-in Development Tooling, Git and CVS support, including source and developer documentation.

I N S T R U C T I O N S

1) Satellites that are in geosynchronous orbit circle the Earth once per day. This eliminates the need for continuous repositioning of satellite receiving dishes because even though the satellite is moving, it stays in the same position relative to the Earth.

Given that the Earth's mass is 5.9736x1024 kilograms and that the satellite's orbital period must be 86,400 seconds (one day), what altitude is required for a geosynchronous orbit?

Even though we are supposed to use the sum of the masses of both the Earth and the satellite, in this case, the satellite's mass is roughly a trillion trillion times less than the Earth and can be considered to be insignificant.
Click on the 'RADIUS' button, enter the time and mass, click on 'CALCULATE' and the answer is 4.2244 x107 meters or 42,244 kilometers or 26,249 miles. (This is the distance as measured from the Earth's center).

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r3 = (G • m • t2) / (4 • π2)
r3 = (6.674x10-11 • 5.9736x1024 • 86,4002) / 39.4784
r3 = 2.976x1024 / 39.4784
r3 = 7.53922
radius = 42,244,000 meters

2) The Moon orbits the Earth at a center-to-center distance of 3.86 x105 kilometers (3.86 x108 meters).
Now, look at the graphic with the formulas and you will see that the 'm' in the formula stands for the mass of both orbital bodies. Usually, the mass of one is insignificant compared to the other. However, since the Moon's mass is about ⅟81 that of the Earth's, it is important that we use the sum of their masses. Since the Moon's mass= .0735 X1024 kilograms and the Earth's mass = 5.9736 x1024 kilograms, then their sum = 6.0471 x1024 kilograms.

Now that you have this information, how long does it take the Moon to make one revolution around the Earth?

Click on the 'TIME' button. Enter the radius and mass data. Click on 'CALCULATE' and the answer is 2,371,900 seconds or 27.453 days.

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t2 = (4 • π2 • r3) / (G • m)
t2 = (4 • π2 • 386,000,0003) / (6.674x10-11 • 6.0471x1024)
t2 = 2.27x1027 / 4.0414
t2 = 5,626,000,000,000
time = 2,372,000 seconds

3) Every 152,850 seconds, Io orbits Jupiter at an average orbital radius of 421,700 kilometers (4.21x108 meters). What is Jupiter's Mass?
Click on the 'MASS' button. Enter the radius and time data.
Click on 'CALCULATE' and the answer is 1.8986 x 1027 kilograms.

* * * * * * * Without Using The Calculator * * * * * * *
m = (4 • π2 • r3) / (G • t2)
m = (39.4784 • 421,700,0003) / (6.674x10-11 • 152,8502)
m = 2.961x1027 / 1.559
mass = 1.899x1027 kilograms
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