As the commenter states, e is indeed called the orbital eccentricity. If you add a radial scale length (e.g., semi-major axis) to both of those values the 1−e describes the periapsis (closest approach of orbit) and the 1+e apoapsis (furthest) of an elliptical orbit. They don't have a specific special name, as they are dimensionless measures, but can be quite useful in determining the orbit of planets and other Keplerian systems.
Periapsis:
rp=a(1−e)
Apoapsis:
ra=a(1+e)
Perhaps the could be named the maximum radial eccentricity and minimum radial eccentricity, if you needed to describe these parameters in a report or class homework etc.
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