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The vehicle will be able to launch satellites of up to 750 kg into geostationary orbit.
As said in the earlier answer, a simple combination of these launchers could not put a satellite into geostationary orbit.
A perfectly stable geostationary orbit is an ideal that can only be approximated.
Launched in 1982, it was operated in geostationary orbit at a longitude of 74 east.
The launch successfully placed the satellite into geostationary orbit.
Examples are any and all particular geographical locations, mineral deposits, and even geostationary orbit locations and portions of the electromagnetic spectrum.
We note that the mass of the satellite "m" appears on both sides geostationary orbit is independent of the mass of the satellite.
Launched in 1967 it was operated in geostationary orbit, spending most of its operational life at a longitude of 15 degrees west.
It would have been capable of moving up to 100 tonnes of mass to a geostationary orbit, but was never flown.
The upper stage of the rocket underperformed, but the satellite used its significant stationkeeping fuel margin to achieve its operational geostationary orbit.
Spacecraft carrying instruments for which an altitude of 36000 km is suitable sometimes use a geostationary orbit.
For satellites in geostationary orbit and geosynchronous orbits, the graveyard orbit is a few hundred kilometers above the operational orbit.
The transfer to a graveyard orbit above geostationary orbit requires the same amount of fuel that a satellite needs for approximately three months of stationkeeping.
To broadcast to these latitudes from a geostationary orbit would require considerable power due to the low elevation angles.
At launch, the satellite was carrying of fuel, for raising itself into geostationary orbit, and subsequently operateing there for a planned twelve years.
