A satellite in an equatorial orbit flies along the plane of the Earth's equator. If an orbit does not lie at an equatorial orbit, then it will not remain at a fixed state.
satellite is satellite
the speed of light = 299792458 m / sGEO (Geostationary Earth Orbit) = 35863000 m above the Earth's surfaceround trip time = 2*(35863000)/299792458 =0.239 sthe time needed for an RF signal to reach a GEO satellite and gets retransmitted back to a ground station on earth is approximately 240 milliseconds(assuming zero signal propagation/processing time in the satellite and equatorial ground station location with the same longitude as the satellite slot)
Answer: 1.communication satellite 2.navigational satellite 3.weather satellite 4.millitary satellite 5.scientific satellite 6.satellite launches. It composed of 6 satellites...........i hope.....my answer can help you.....
A "geo-synchronous" orbit is one in which a satellite orbits in exactly 23 hours 56 minutes, the same rate at which the Earth spins. So while the satellite is moving and the Earth is moving, they are moving together at the same angular speed. This only works for equatorial orbits.
It is 71492 kilometres.
It is polar orbiting.
equatorial orbit
Geo-stationary communication satellites are 35,768 Km far from earth surface at an equatorial latitiude.
The satellite inclination angle in satellite communication refers to the angle between the satellite's orbital plane and the equatorial plane of the Earth. This angle is crucial for determining the satellite's coverage area and the type of services it can provide. A geostationary satellite, for example, has an inclination angle of 0 degrees, allowing it to remain fixed over a specific point on the equator, while polar satellites typically have an inclination of 90 degrees, enabling them to pass over the poles and cover the entire Earth.
The range of orbit inclinations for artificial satellites can vary from 0 degrees (equatorial orbit) to 90 degrees (polar orbit). The inclination determines how tilted the satellite's orbital plane is relative to the Earth's equatorial plane. Different types of orbits have specific inclination ranges based on their intended purpose and requirements.
And here ... the way you were going ... we thought you were going to ask somethingreally astronomical, like "What is the satellite's altitude above the earth's surface ?"OK. To answer the question you actually did ask, we think we have to assume that yoursatellite is in an equatorial orbit. If its orbit is inclined to the equator, then the componentof its velocity along the equator could be sinusoidal ... we're not sure, and don't feel likeputting that much effort into it right now. (It won't make any difference anyway.)If it makes 5.0 complete revolutions in 24 hours, then . . .-- if the earth is rotating in the same direction, then the satellite's "ground speed" is4 x (equatorial circumference) / 24 = 4,150 miles per hour.-- if the earth is rotating in the opposite direction, then the satellite's "ground speed" is6 x (equatorial circumference) / 24 = 6,225 miles per hour.
There are equatorial lines of latitude.
North Equatorial flow clockwise and southern counter-clockwise.
Guinea Ecuatorial =Equatorial Guinea
The population of Equatorial Guinea is 633,441.
For a satellite to stay in one place over the earth, the satellite must be going in orbit in the same direction that the earth spins. The satellite must also travel at the same pace/speed as the earth spins to give us the 24-hour day that we as people witness. To apparently stay in one place it must be in a synchronous orbit. For the earth this is about 24,000 miles altitude. It must also be an equatorial satellite.
the equatorial inclination is an inclined plane on the earth..