How much delta-v does a typical geostationary satellite carry? I'm wondering - how much delta-v do typical geostationary satellites carry with them once they get into the orbit for things like orbital adjustment or movement to the graveyard orbit?
There's a mountain of readily available information, of which the following is one example.  From   GOES page
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There is more information there about the thrust produced, so I suspect you can calculate the total delta-kinetic energy available.

A2100 has been used for over 40 missions and is available in different versions catered to specific mission needs in terms of
dimensions and power availability with satellite mass varying between
2,000 and 6,740 Kilograms.
Each GOES-R-class satellite is 6.1 by 5.6 by 3.9 meters in size and has a dry mass of 2,857 Kilograms. At liftoff, the satellite
weighs 5,192 Kilograms, loaded with propellants to support a mission
of at least 14 years.
GOES-R, S, T, U launches with a propellant and pressurant load of
2,335 Kilograms with Mixed Oxides of Nitrogen and Hydrazine acting as
main propellant components and Helium gas used for the pressurization
of tanks.