I ask you for one reference which proves your point of view that geo satellites do not move. Every reliable reference on satellites and orbits says that a geo satellite is in a geo orbit. All satellites work the same it makes no difference whether its high or low altitude
No they are not the same as I just previously described, from a position on earth LOS move, HOS do not.
- they orbit by their own momentum and any fuel on large satellites is not enough to sustain them for such a long period of time, but it's used to correct or change the orbit when required.
They have to use their own momentum via fuel otherwise they fall to earth at LO.
Yes calculations may be done w.r.t a stationary earth because it is more convenient.
OK so you admit that the calculation are done with a geostatic model, that's good, kind of difficult to deny that, not that it's merely convient, it just because the earth is not moving therefor your calculations need to be based on a non-moving earth otherwise you wouldnt be able to calculate with moving earth model because the calculations would be wrong.
But the fact remains that every GEO satellite is designed to go into a geo orbit, not a geo stationary.
But it is geostationary.
The power is not to maintain speed , momentum does that, in orbit it it's to make corrections if it goes out of orbit. If low level satellitse need fuel to propel them, then how come LEO satellites as small as 50 kg or less and 1 foot cubed satellites can fly at 7.5 km/s in orbit for years with no rockets or fuel? Read some websites about how satellitse work and if you can find one that proves your view please post it. I doubt you can though, because it's pretty much a no brainer that all satellitse orbit around the earth and there's no such thing as a non-moving satellite, except when viewed from an observer on the ground in the case of geostationary satellites.
This is the alleged gravity enabled geosynchronous model: consider what is required to make this particular satellite move after it is placed in its position:
a) It must attain and maintain an exact epeed of 6865 MPH, to be off by even 1 MPH would throw it out by over 700 miles in one month. off 10 MPH = 7000 miles out of position per month, this is a serious problem. No other satellites retain an unassisted, unvarying speed!!! That is a fact.
b) It must perform a perfectly circular orbit with absolutely no apogee or perigee. This is something that no satellite has ever achieved.
c) any varience from 4-way confinement withing given flight path affects the speed and direction, this would result in failure as there is no way to readjust direction, and of course you would have to constantly change the postion of the the recieving dish points.
d) The ring of geostationary satellites now over the equator has very nearly reached maximum, i.e. 180 at 2 degrees apart, so the current need for virtual geostationary satellites ...One of the characteristics of the new orbits of new "virtual geostationary satellite" contain the proof that geosynchronous concept os utterly false! And indeed that the present geostationary satelites are in fact geostationary and do not move. What is this characteristic? I will tell you; there orbits can be either clockwise or anticlockwise... while all geostat orbits must be counterclockwise obviously to match the alleged counterclockwise rotation of the earth.
http://www.patentstorm.us/patents/6701126/description.html
The satellite in a high-altitude, geostationary orbit circles the earth once every 24 hours, the same amount of time it takes for the Earth to spin on its axis. The satellite turns eastward (like our Earth) along the Equator. It stays above the same point on Earth all the time. To maintain the same rotational period as the Earth, a satellite in geostationary orbit must be 22,237 miles above the Earth. At this distance, the satellite can view a huge portion of the Earth's surface. Because the high-altitude satellite appears to remain fixed in one position (it's really orbiting at the same rate as the Earth turns), it requires no tracking to receive its downlink signal. That is why when we turn our home satellite dish on to receive the TV signal from a particular geostationary satellite, we don't have to keep jumping up to adjust its position.
For reasons I just expained, no satellite can maintain the same postion at the same speed and direction, that why all calculations are done based on the earth not moving, if the earth was rotating the satelites that are in geosationary positions could not keep that position, if the satelites were moving in geosynchronous speed, in relation to a rotating earth than such calculation would exist and could be proved by physics seeming no calculation exist that actually works based on a rotating earth, then it is proven by the same given method that they are indeed stationary. LOS that move need propulsion to do so;
http://gltrs.grc.nasa.gov/cgi-bin/GLTRS/browse.pl?1994/TM-106701.html