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AE Orbit Description Assessment (Part 2)

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Last updated about 2 hours ago
27 questions
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Question 1
1.

What two details of a satellite's orbit can be determined from examining a ground trace?

Question 2
2.

Many of Kepler's theories were based on the documentation of this philosopher that he worked with for a short time.

Question 3
3.

Label each ellipse with the correct eccentricities.

Draggable itemarrow_right_altCorresponding Item
B
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0
C
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0.7
A
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0.4
Question 4
4.

To make the pictured ellipse more circular, you should move foci A and B _________.

Question 5
5.

What is the name of the "radii" labelled A in the pictured ellipse?

Question 6
6.
Draggable itemarrow_right_altCorresponding Item
Describes the size of an orbit. For circular orbits, altitude is often used in place of this term.
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Inclination
The measure of how circular or elliptical an orbit is.
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Eccentricity
The point in the orbit of an object (such as a satellite) orbiting the earth that is the closest to the center of the earth.
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Semi-Major Axis
The point in the orbit of an object (such as a satellite) orbiting the earth that is at the greatest distance from the center of the earth.
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Apogee
The "tilt" of the orbit relative to the equator.
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Perigee
Question 7
7.

The value of which orbital parameter is 0 when the satellite is at its perigee point and 180 when the satellite is at apogee?

Question 8
8.

Label the position indicated with the A in the pictured orbit.

Question 9
9.

Both size (semi-major axis and/or altitude) and eccentricity play an important role in determining the period of the orbit.

Question 10
10.

The Voyager 1 spacecraft was launched in 1977 to explore the solar system and beyond. In 2008, it was entering the region between our solar system and interstellar space known as the heliosheath. It is the furthest manmade object from the Eatch and it continuing its journey into the unknown. Based on what you have learned about orbital elements, the eccentricity of Voyager is greater than 1.

Question 11
11.

This philosopher believed that everything rotates around the Earth.

Question 12
12.

This philosopher was the first to propose heliocentric theory.

Question 13
13.

_________________ is the angle between the Earth’s equatorial plane and the
plane of the orbit. It describes the tilt of the orbit.

Question 14
14.

The point in an orbit that is closest to the Earth.

Question 15
15.

What is the projection of a satellite's orbit onto the earth, represented in a 2D map called?

Question 16
16.

A satellite designed to take images to monitor the polar ice caps would have an inclination of ___ degrees.

Question 17
17.

A satellite crosses the equator in a northerly direction at 0 degrees longitude. On its next northerly pass over the equator it crosses at 23 degrees west longitude. How many minutes did it take this satellite to complete one orbit?

Question 18
18.

A circular orbit has an apogee roughly twice the altitude of its perigee.

Question 19
19.

Which orbital parameter must use a reference point in space, because an earth based reference point will move as the earth rotates?

Question 20
20.

Kepler has two different sets of laws of orbital motion. One set applies to planets orbiting the Sun, and the other set applies to man-made satellites orbiting the Earth.

Question 21
21.

This scientist was the first to use a telescope to help prove heliocentric theory.

Question 22
22.

An argument of perigee would be easiest to see in a picture of an orbit with which eccentricity?

Question 23
23.

Which of the following orbital parameters describes the size of the orbit?

Question 24
24.

Who developed the Keplerian Element Set which describes the orbital parameters of satellites' orbits?

Question 25
25.

All circles are ellipses and all ellipses are circles.

Question 26
26.

Which is NOT one of the six elements of the Keplerian element set?

Question 27
27.

An orbiting object is moving slowest at apogee.