AE Orbital Mechanics Assessment (Part 3)
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| Draggable item | arrow_right_alt | Corresponding Item |
|---|---|---|
The "tilt" of the orbit relative to the equator. | arrow_right_alt | Inclination |
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. | arrow_right_alt | Eccentricity |
Describes the size of an orbit. For circular orbits, altitude is often used in place of this term. | arrow_right_alt | Semi-Major Axis |
The measure of how circular or elliptical an orbit is. | arrow_right_alt | Apogee |
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. | arrow_right_alt | Perigee |
| Draggable item | arrow_right_alt | Corresponding Item |
|---|---|---|
B | arrow_right_alt | 0 |
C | arrow_right_alt | 0.7 |
A | arrow_right_alt | 0.4 |
| Draggable item | arrow_right_alt | Corresponding Item |
|---|---|---|
Low Earth Orbit | arrow_right_alt | Short orbital period of approx 90 minutes |
Polar | arrow_right_alt | Period equals one day |
Geostationary | arrow_right_alt | Highly inclined AND highly elliptical orbit |
Molniya | arrow_right_alt | Inclination of 90 degrees |