This is the approximate trajectory of the SpaceX Falcon 9 booster during a “return to launch site” landing (i.e. landing on land).

This is the predicted trajectory of the engine block on a launch vehicle implementing ULA’s SMART Reuse technology, such as the ULA Vulcan.

This is the approximate trajectory of the SpaceX Falcon 9 booster during a downrange propulsive landing (i.e. ocean landing) on the ASDS.

Note that this profile includes a boostback burn; this profile was used during the launch of CRS-8, among others. It’s not used with heavy payloads, such as some of the larger GTO missions; instead, the booster does not perform a boostback burn and ends up much farther downrange, requiring the ASDS to position itself much farther from shore. The approximate trajectory of a Falcon 9 landing without a boostback burn can be seen here.

This is the approximate trajectory of the SpaceX Red Dragon capsule during its landing on Mars.