What is the altitude of geosynchronous satellite?

What is the altitude of geosynchronous satellite?

22,236 miles
1 Geostationary satellites. A geostationary satellite is in an orbit that can only be achieved at an altitude very close to 35,786 km (22,236 miles) and which keeps the satellite fixed over one longitude at the equator.

What is geosynchronous orbit equation?

re−s=(0. 667×6×8.64240×10−10+24+2×4)13 km.

What is the velocity of a geosynchronous satellite?

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 speed of about 7,000 mph (11,300 kph).

Is the ISS in geosynchronous orbit?

The International Space Station and the Hubble Space Telescope are both in LEO. A geostationary or geosynchronous orbit is located at an altitude of 36,000 km, and takes a lot more energy to reach than LEO. At this higher altitude it takes the satellite a full 24 hours to orbit the Earth.

What is the orbital speed of a geosynchronous satellite?

What are the altitude and orbital speed of a satellite in a geosynchronous orbit?

What is a geosynchronous orbit in physics?

A geosynchronous orbit (sometimes abbreviated GSO) is an Earth-centered orbit with an orbital period that matches Earth’s rotation on its axis, 23 hours, 56 minutes, and 4 seconds (one sidereal day).

Are all geostationary satellites at the same altitude?

Orbital stability A geostationary orbit can be achieved only at an altitude very close to 35,786 kilometres (22,236 miles) and directly above the equator.

What is geosynchronous orbit velocity?

What is the altitude of the geosynchronous orbit of the Earth?

The geosynchronous orbit (synchronous orbit of the Earth) is at an altitude of 35,796 km (≈ 36,000 km) and has a semi-major axis of 42,167 km. Excel formula used in this table to calculate the altitude of the satellite in synchronous orbit of the planet: = ((((G*M*T^2)/ (4*PI ()^2))^ (1/3))-R*1000)/1000

How do you calculate the radius of a geosynchronous orbit?

R = Radius of the planet The geosynchronous orbit (synchronous orbit of the Earth) is at an altitude of 35,796 km (≈ 36,000 km) and has a semi-major axis of 42,167 km. Excel formula used in this table to calculate the altitude of the satellite in synchronous orbit of the planet: = ((((G*M*T^2)/ (4*PI ()^2))^ (1/3))-R*1000)/1000

How to calculate the altitude of the satellite in synchronous orbit?

Excel formula used in this table to calculate the altitude of the satellite in synchronous orbit of the planet: =((((G*M*T^2)/(4*PI()^2))^(1/3))-R*1000)/1000.

How do you calculate the geostationary orbit?

In order to calculate the geostationary orbit around any given body, we must first create an equation with the force of gravity and the centripetal force. The force of gravity is equal to: ), M 1 is the mass of the body, M 2 is the mass of the satellite, and r is the distance between the center of mass of the planet and that of the satellite.