Whatellites? 
Which ellites? Are our antennas fixed one point but catching them continuesly things on orbit? 
Google 'geostationary'.
Sorry i forgot that time when google sent a sattelite rocket to the orbit. Would you want to remind me?
OK, why try "using a web search engine of your choice, do some basic research into what a geostationary satellite is".
And just for fun, here's a British Pathe News article about a UK company building the receiving equipment for polar orbital weather satellites:
http://www.britishpathe.com/video/weather-satellite-station/query/weather+satellite
All about sattelites are lie. All lie. Some sources shows sattelites about 200-600 kilometres and more. Some sites showing less. But some sites showint their altitude about 35 000 kilometres. But we see the rocket goes about 2 minutes so it should be about 200-300 kilometres or low. But if we calculate it by angles and distances, finding tens on tousends kilometres, like this site show:
Turksat sattelite about on upper position to Tanzania and about 35.000 kilometres high. But take care, sattelites launches with rocket about 2 minutes and then reviewers saying the sattelite gone to the orbit! Where are they stays on? About 200-600 kilometres or 35.000-45.000 kilometres? There is no similarity between appears, calculated and said.
When you hear "But take care, sattelites launches with rocket about 2 minutes and then reviewers saying the sattelite gone to the orbit!" this is probably for satellites going (at least initially) into a Low Earth Orbit of 200 to 400 km. I don't know the details of insertion into Medium or High Earth Orbit.
You claim "There is no similarity between appears, calculated and said." That is not right at all, there is very good agreement - see my explanations below.
Satellites can orbit at any altitude from about 200 km above sea-level, biy those this low lose altitude from atmospheric drag.
The ISS orbits in what is called
Low
Earth
Orbit (or LEO). Being so low it avoids long-term crew exposure to the radiation of the first Van Allen Belt.
International Space Station
The ISS maintains an orbit with an altitude of between 330 and 435 km (205 and 270 mi) by means of reboost manoeuvres using the engines of the Zvezda module or visiting spacecraft. It completes 15.54 orbits per day.
GPS Satellites are in
Medium
Earth
Orbit
GPS satellites
GPS satellites fly in medium Earth orbit (MEO) at an altitude of approximately 20,200 km (12,550 miles). Each satellite circles the Earth twice a day.
The satellites in the GPS constellation are arranged into six equally-spaced orbital planes surrounding the Earth. Each plane contains four "slots" occupied by baseline satellites. This 24-slot arrangement ensures users can view at least four satellites from virtually any point on the planet.
From GPS.gov, Space Segment
Geosynchronous and Geostationary satellites have to circle the earth in one sidereal day or approximately 23 hours 56 minutes and 4 seconds and so are in
High
Earth
Orbit or
Geosynchronous
Earth
Orbit.
Geostationary orbit
A geostationary satellite above a marked spot on the Equator. An observer on the marked spot will see the satellite remain directly overhead unlike other celestial objects which sweep across the sky.
A geostationary equatorial orbit (GEO) is a circular geosynchronous orbit in the plane of the Earth's equator with a radius of approximately 42,164 km (26,199 mi) (measured from the center of the Earth). A satellite in such an orbit is at an altitude of approximately 35,786 km (22,236 mi) above mean sea level. It maintains the same position relative to the Earth's surface.
Usually the altitude of the satellite is given above sea-level simply because it's easier for us to picture ths for the lower satellites.
The
orbital radius is the distance of the satellite from the centre of the earth, so for satellites in an equatorial orbit it is
(the altitude + the equatorial radius of earth) = altitude + 6,384 km).
You had this information about the TURKSAT 2A
TURKSAT 2A
Geostationary
TV
NORAD ID: 26666
Int'l Code: 2001-002A
Perigee: 35,857.1 km
Apogee: 35,883.1 km
Inclination: 0.6 °
Period: 1,440.0 minutes
Semi major axis: 42241 km
RCS: 3.9 m2 (large)
Launch date: January 10, 2001
Source: Turkey (TURK)
Launch site: FRENCH GUIANA (FRGUI)
32 Ku-band transponders; direct-to-home voice, video, and data transmissions to countries between central Europe and the Indian subcontinent.
Meaning that the orbit is slightly elliptical with the lowest altitude or perigee = 35,857.1 km and the highes altitude or apogee = 35,883.1 km.
The "Semi major axis: 42,241 km" means that the average radius (from the centre of the earth) is 42,241 km and
the "Inclination: 0.6°" means that the orbit is inclined from the equator by 0.6°.
Maybe you won't bother reading this, but I have tried explaining it as well as I can.
And please don't call people liars, when it is you that do not understand what is going on. Just having an IQ of 160 does not help unless you have the knowledge to go with it.