And it seems the "problem" is that the satellite is deliberately launched to the standard GTO trajectory, then apparently expected to make the 30+ degree inclination plane change to then target IGSO! I've never heard of something like that for a GSO sat!
https://twitter.com/Cosmic_Penguin/status/1119631197162708992 …
How much delta-V is need for a satellite to move from 28.5 to 55 degrees inclination assuming its orbit is 36500 km circular?
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It would be very close to the amount of delta-V to go from 28.5 to 0 degrees inclination as a standard GTO satellite
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Das Laden scheint etwas zu dauern.
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