Quote from the BDS-3 sat chief designer: "In the past the launch vehicle makes the maneuver to get the IGSO sat from the usual GTO to 55 deg. incl. orbit; now the sat is optimized to maneuver by itself. This increases the sat's capacity and makes the IGSO and GEO sats similar."
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I realized that while not quite the same, this seems similar to the plan of launching GPS sats from the Space Shuttle in the 1980s, where the GPS sat & upper stage are released from a 28-ish deg. LEO (as they are almost always planned to be flown with run-of-the-mill comsats)?
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