The orbital time period of a geostationary satellite is approximately 24 hours, specifically about 23 hours, 56 minutes, and 4 seconds. This allows the satellite to maintain a fixed position relative to a point on the Earth's surface, as it orbits the Earth at the same rotational speed. Geostationary satellites are positioned at an altitude of about 35,786 kilometers (22,236 miles) above the equator.
The time it takes for a satellite to complete one full orbit around the Earth, known as its orbital period, can vary depending on the altitude of the satellite. On average, a satellite in low Earth orbit (LEO) typically takes about 90 minutes to complete one orbit, while a geostationary satellite orbits the Earth every 24 hours.
A geostationary satellite takes approximately 24 hours to complete one revolution around the Earth. This period matches the Earth's rotation period, allowing the satellite to remain fixed over a specific point on the equator. As a result, it appears stationary relative to the surface of the Earth.
this is if it is not a geostationary orbit, in which case it is always in the same place relative to earth. imagine a circle of radius 42250km+radius of earth(6,356km). it's perimeter is 2 x pi x 48606km = satellite's journey. then think of a really fast speed, which is the speed the satellite is moving at. divide the distance by speed and you have the time of one orbit However, by the height being 42250 , it makes me think the satellite is a geostationary satellite and so it would take 24 hours moving at approximately 12725 kmph does that answer your question?
The period of revolution or orbital revolution. For Earth, this is one year.
The time it takes for something to go completely around a fixed point.
The rotation period of a geostationary satellite is equal to one sidereal day, which is approximately 23 hours, 56 minutes, and 4 seconds. This period matches the time it takes for the satellite to orbit the Earth once and remain fixed relative to a specific point on the Earth's surface.
If a satellite is in geosynchronous orbit, it will take the satellite 24 hours, a day, to orbit the Earth once. This is so because geosynchronous orbit is when a satellite orbit the Earth at such a time, that is is over the Earth at all times.
The time it takes for a satellite to complete one full orbit around the Earth, known as its orbital period, can vary depending on the altitude of the satellite. On average, a satellite in low Earth orbit (LEO) typically takes about 90 minutes to complete one orbit, while a geostationary satellite orbits the Earth every 24 hours.
Watch the satellite, with either a telescope or a very highly directional radio antenna. An observation period of twelve hours will be long enough to answer the question. If the satellite appears to move in the sky by more than a few tenths of a degree during that time, then it is not in geostationary orbit.
A geostationary satellite takes approximately 24 hours to complete one revolution around the Earth. This period matches the Earth's rotation period, allowing the satellite to remain fixed over a specific point on the equator. As a result, it appears stationary relative to the surface of the Earth.
A geostationary satellite is an earth-orbiting satellite, placed at an altitude of approximately 35,800 kilometers (22,300 miles) directly over the equator, that revolves in the same direction the earth rotates (west to east). A geosynchronous satellite is a satellite whose orbital track on the Earth repeats regularly over points on the Earth over time.
The period of a satellite is the time it takes for the satellite to complete one orbit around its parent body, such as a planet or a star. It is typically measured in hours, days, or years depending on the size and speed of the satellite's orbit. The period is determined by the satellite's orbital velocity and the mass of the parent body it is orbiting.
Artificial satellites orbit the Earth. Some are geostationary - means that their orbital period matches the revolutions of the Earth, keeping them in the same spot over the surface all the time. Other travels roughly pole-to-pole, allowing them to cover the whole Earth as the Earth rotates beneath them.
The time it takes a planet or satellite to revolve once is called its day.
Synchronous orbitThis is where an orbiting body (moon) has a period equal to the average rotational period of the body being orbited (planet), and in the same direction of rotation as that body.
Because the geostationary orbit round the Earth is perturbed by gravity from the Sun and Moon. The biggest effect is to change the orbital plane of the geostationary satellite so that, after a while on station, in 24 hours it appears to move up and down slightly. For that reason communications satellites need motors and fuel to correct the orbit from time to time.
The time for one (stable) orbit is directly linked to the orbital radius. At one particular radius (geostationary), the resultant stable orbit velocity is exactly enough to match the rotation of the earth, keeping the satellite overhead at all times. This geostationary radius is approximately 42 000 km from earths centre and most geostationary satellites are roughly in the equatorial plane.