Why Do Geostationary Satellites Have To Be Above The Equator?

Why Do Geostationary Satellites Have To Be Above The Equator? It is always directly over the same place on the Earth’s surface. … Satellites in geostationary orbit rotate with the Earth directly above the equator, continuously staying above the same spot. This position allows satellites to observe weather and other phenomena that vary on short

Why Is It Not Possible To Have A Geostationary Satellite Above The UK?

Why Is It Not Possible To Have A Geostationary Satellite Above The UK? There cannot be a geostationary satellite at the poles, basically because it would have to be at rest, which cannot happen as it would get pulled by the earth’s gravity and eventually crash to the surface. Why is it not possible to

Do Satellites Stay Stationary?

Do Satellites Stay Stationary? Because the satellite orbits at the same speed that the Earth is turning, the satellite seems to stay in place over a single longitude, though it may drift north to south. … Satellites in geostationary orbit rotate with the Earth directly above the equator, continuously staying above the same spot. Are

What Do U Mean By Geostationary Satellite?

What Do U Mean By Geostationary Satellite? Satellite that appears to be located at a fixed point in space when viewed from the earth’s surface. Satellites located in geosynchronous orbit move in time with the rotation of the earth. What do you mean by geostationary? : being or having an equatorial orbit at an altitude

How Fast Does Space Debris Travel In A Geosynchronous Orbit?

How Fast Does Space Debris Travel In A Geosynchronous Orbit? They travel at speeds up to 17,500 mph, fast enough for a relatively small piece of orbital debris to damage a satellite or a spacecraft. How long does it take for space debris to deorbit? “Below 500 km, the effect of the atmosphere, the spacecraft

How High And Fast Do Geosynchronous Satellites Travel?

How High And Fast Do Geosynchronous Satellites Travel? The aptly titled geosynchronous orbit is described in detail: “At an altitude of 124 miles (200 kilometers), the required orbital velocity is just over 17,000 mph (about 27,400 kph). To maintain an orbit that is 22,223 miles (35,786 km) above Earth, the satellite must orbit at a