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Apr 25th, 2006 at 5:26pm
The “figure 8” of an inclined orbit may not always be vertical or an “oval”. It may have a pronounced slant based upon its eccentricity and argument of perigee. Eccentricity and argument of perigee may also cause the longitude of ascending and descending nodes (center of station) to shift to the east and/or west of mean longitude. An inclination of the satellite orbit, however, causes the sub-satellite point (the point on the equator directly under the satellite orbital location) to move in a figure 8 pattern. The source of this figure 8, called the analemma, is the motion of the satellite along the inclined orbit, which will alternately fall behind and then catch up to the uniform rotation of the Earth on its axis. [Remember – inclination is the N-S movement of the satellite as it completes an orbit. Nonzero eccentricity is the second factor that may cause a non-uniform apparent motion. (Remember, this is in an E-W direction.) In general, the inclination and eccentricity motions will be superimposed upon each other, resulting in two possible shapes for the motion of the geosynchronous satellite as seen from the Earth. If the nonzero inclination dominates, then the satellite will appear to move in a figure 8. If the eccentricity is larger than the inclination effect, the the apparent motion will be a single open oval
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