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  Geospatial Data / Remote Sensing Tutorial / Introduction to Satellites and Orbits

Introduction to Satellites and Orbits

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Shape

Satellites orbit their primary body in a shape that is called an ellipse. An ellipse can be thought of as a circle that is somewhat "out of round," although the technical definition of an ellipse is "a closed plane curve generated by a point moving in such a way that the sums of the distances from two fixed points is a constant." The characteristics of an ellipse are probably best understood when compared to a circle.

A perfect circle has a single point in its center. Each point on the circle is an equal distance from this point, known as the focus of the circle. Any line that connects two sides of the circle and passes through the focus are equal in length.

An ellipse is a circle that is slightly stretched in one dimension. An ellipse has two focal points. The sum of the distances from any point to each focal point will always remain constant. A line that connects two sides of the ellipse and passes through both focal points is called the major axis of the ellipse. A line perpendicular to the major axis that passes through the point directly between the focal points is the minor axis of the ellipse.

The degree to which an ellipse is stretched is described as the eccentricity of the ellipse. The eccentricity can be described as the ratio between the length of the major axis and the distance between the foci of the ellipse. The foci in highly eccentric ellipse are spread farther apart than those of an ellipse with a lower eccentricity. The value of eccentricity ranges from 0 (a perfect circle) and approaches a value of 1 as the ellipse becomes more eccentric.

A satellite's orbit around the Earth is in the shape of an ellipse, and the Earth's center of mass is at one of the focal points of the ellipse. A satellite orbit can be described by the eccentricity of the orbit. Satellite orbits range from nearly circular orbits (with a low eccentricity) to very highly elliptical orbits (with a high eccentricity). A satellite with a nearly circular orbit maintains a relatively constant altitude above the Earth's surface, while the altitude of a satellite with a very highly elliptical orbit is constantly changing.

Size

Another of the orbital elements used to describe a satellite's orbits is the semi-major axis, which is defined as half the distance of the major axis. In general, the larger the semi-major axis, the larger the orbit. The larger the orbit, the greater the amount of energy required to place the satellite into the orbit. Thus, satellites with larger orbits with higher altitudes above earth are much more expensive to launch and maintain.

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