The mutual gravitational force between any two objects is the force that keeps
any orbiting objects in orbit around their mutual center of mass.
In orbit, the force of gravity between the object and the celestial body it is orbiting keeps the object in orbit. This force creates a centripetal acceleration that balances the object's inertia, causing it to stay in a stable orbit.
As a noun: The rocket placed the satellite into a high Earth orbit. As a verb: The satellite had to travel very fast to orbit the Earth.
GRAVITY!A2. Centripetal force. The velocity of the satellite around the earth causes centripetal, force which balances with the gravity, holding it in a circular orbit around the earth.
F= G (m1m2)/(r2) F= the gravitational force G= gravitational constant m1= mass of the first object (the satellite) m2= mass of the second object (earth) r= the radius Plug in the values and solve for r: 690 N= 6.67 X 10-11 ((124kg) X (5.98 X 1024)/(r2) 690r2= 6.67 X10-11 (7.41 X 1026) 690r2= 4.94 X 1016 r2= (4.94 X 1016)/(690) r= square root of (7.16 x 1013) r= 8.46 x 106 m, or 846,000 Km
To launch a satellite to Mars, you would need to use a rocket to propel it out of Earth's orbit toward Mars. The satellite would need to follow a precise trajectory to intercept Mars's orbit at the right time. This would require careful planning and calculations for the satellite's speed and direction.
In orbit, the force of gravity between the object and the celestial body it is orbiting keeps the object in orbit. This force creates a centripetal acceleration that balances the object's inertia, causing it to stay in a stable orbit.
As a noun: The rocket placed the satellite into a high Earth orbit. As a verb: The satellite had to travel very fast to orbit the Earth.
Rockets are used as engines to accelerate the satellite to a speed fast enough to get it in orbit.
Geostationary should resolve in geostationary orbit because its centrimeter and gravitational force in geostationary satellite.A parking slot is provided for satellite.In geostationary satellite is maintain in this orbit in its whole life and maintain satellite in geostationary orbit is called "Station Keeping"In other words, the control routine necessary to keep the satellite in positionis known as "Station Keeping".It use to overlapping of coverage area of individual satellite.
GRAVITY!A2. Centripetal force. The velocity of the satellite around the earth causes centripetal, force which balances with the gravity, holding it in a circular orbit around the earth.
You give velocity to a satellite through rockets. The rockets use some powerful fuel - for example, a mix of hydrogen and oxygen - to push them into orbit.
It is basically used to save fuel, using the planet's gravitational force as a slingshot to gain speed.
The orbit of a satellite is determined based on the functions that the satellite needs to perform. A communications satellite.s purpose is to make communications easier. If it were in a very low orbit, the satellite would pass quickly overhead and you would only have a couple of moments to talk. A photo satellite needs to have a low orbit, to be close enough to take good pictures. Photo satellites are often in polar orbits to allow them to cover the entire globe rather than the same parts over and over again.
Many satellites contain propellant tanks used for repositioning the satellite. They also use solar arrays to collect energy from the sun. When the satellite runs out of fuel it is said to have reached its end of life and will either burn up in the earths atmosphere or will be put in another orbit, such as super synchronous orbit. This allows a replacement satellite to be launched and put in the same orbit but prevents over population of that particular orbit.
F= G (m1m2)/(r2) F= the gravitational force G= gravitational constant m1= mass of the first object (the satellite) m2= mass of the second object (earth) r= the radius Plug in the values and solve for r: 690 N= 6.67 X 10-11 ((124kg) X (5.98 X 1024)/(r2) 690r2= 6.67 X10-11 (7.41 X 1026) 690r2= 4.94 X 1016 r2= (4.94 X 1016)/(690) r= square root of (7.16 x 1013) r= 8.46 x 106 m, or 846,000 Km
In a satellite, electrical energy is transformed into kinetic energy during launch, allowing the satellite to reach its desired orbit. Once in orbit, solar panels on the satellite convert solar energy into electrical energy to power its systems. Additionally, some satellites use radioisotope thermoelectric generators to convert heat energy into electrical energy.
The magnetic force of the Earth's gravity holds the Moon in it's orbit.