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- 7.8 km/s (28,000 km/h)The speed of a satellite orbiting Earth depends on its altitude. For a circular orbit at a height of 300 km above the Earth's surface, a speed of 7.8 km/s (28,000 km/h) is needed, allowing the satellite to complete one orbit around the Earth in 90 minutes1. Satellites in geostationary orbit, which are 22,223 miles (35,786 kilometers) above Earth, orbit at a speed of about 7,000 mph (11,300 kph) to maintain their position2.Learn more:✕This summary was generated using AI based on multiple online sources. To view the original source information, use the "Learn more" links.To stay in orbit, a satellite has to travel at a very high velocity, which depends on the height. So, typically, for a circular orbit at a height of 300 km above the Earth's surface, a speed of 7.8 km/s (28,000 km/h) is needed. At this speed, the satellite will complete one orbit around the Earth in 90 minutes.www.esa.int/kids/en/learn/Technology/Mission_con…To maintain an orbit that is 22,223 miles (35,786 kilometers) above Earth, the satellite must orbit at a speed of about 7,000 mph (11,300 kph). That orbital speed and distance permit the satellite to make one revolution in 24 hours.science.howstuffworks.com/satellite6.htm
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