Satellite Orbits


Satellite orbits are at the heart of every satellite’s function. Without a proper understanding of the orbit of a satellite, it would be impossible to launch and maintain a satellite in space. In this article, we will provide an overview of satellite orbits, including their types, properties, and applications.

An orbit refers to the path that a satellite follows around a celestial body like the Earth, Moon, or any other planet. The most common orbit that satellites follow is a circular or elliptical path around the Earth. Satellites move around the Earth due to the gravitational pull of the planet. However, the type of orbit depends on the satellite's purpose and requirements.

There are different types of satellite orbits designed for different applications. The most common types of satellite orbits include the Low Earth Orbit (LEO), Geosynchronous Orbit (GEO), and Molniya Orbit.

Low Earth Orbit (LEO)
LEO is the most common type of orbit used for satellites. A LEO is an orbit that is at a low altitude, typically between 100 to 1200 kilometers above the Earth's surface. Satellites in LEO orbits have a speed of about 28,000 kilometers per hour and take about 90 minutes to orbit the Earth. LEO orbits are mostly used for communication, weather monitoring, Earth observation, and scientific observation.

Geosynchronous Orbit (GEO)
GEO is an orbit at about 36,000 kilometers above the equator, and satellites in this orbit take about 24 hours to complete an orbit around the Earth. Satellites in GEO orbits remain in the same position relative to the Earth because they move around the Earth at the same rate as the Earth rotates. Satellites in GEO orbits are commonly used for communication, direct broadcast, and meteorological observation.

Molniya Orbit
A Molniya orbit is a highly elliptical orbit used in communication, navigation, and surveillance. Satellites in Molniya orbits have a period of 12 hours but move at a very high altitude. The orbit allows the satellite to remain in constant contact with the ground station due to its high eccentricity. These orbits are typically used by Russian communication satellites to cover the high latitudes of the northern hemisphere.

Satellite orbits have various properties that are essential for analyzing their function. These properties include the period, altitude, inclination, eccentricity, and apogee.

Period: The period of a satellite refers to the time it takes to complete one orbit around the Earth. The period of a satellite depends on its altitude.

Altitude: Altitude refers to the height of the orbit above the Earth's surface. The higher the altitude, the longer the period and slower the speed of the satellite.

Inclination: The inclination of a satellite refers to the angle between the plane of the satellite's orbit and the equatorial plane of the Earth.

Eccentricity: The eccentricity of an orbit refers to the shape of the orbit. If the eccentricity of the orbit is zero, the orbit is circular, and if it is greater than zero, the orbit is elliptical.

Apogee: Apogee refers to the point in an orbit that is farthest from the Earth.

Satellite orbits have many applications in our lives. They are used for communication, navigation, weather forecasting, scientific observations, and military surveillance. For example, the Global Positioning System (GPS) depends on a network of satellites in orbit to provide accurate location information. Weather forecasts and severe weather alerts are possible due to satellite imagery and data transmitted from orbits above the Earth.

In conclusion, satellite orbits are critical components of satellite function and operation. The choice of orbit depends on the satellite's function and application, and its properties determine the satellite's function and purpose. By understanding satellite orbits, we have been able to develop and launch many satellites into space, which has revolutionized our lives and the way we interact with the world around us.