I think the reduced detection horizon against ground based radar is really an incidental and largely peripheral benefit when modern and next gen early warning and tracking are increasingly going the space based route.
All of the space-based architecture network for hypersonic missile tracking will be in LEO, so an ICBMs that typically peaks at 1200 km will not be tracked by this array of space sensors, but will have a weakness due to altitude and radar based on land can track and discriminate and provide target designation for anti-ballistic missiles.
An ICBM with a depressed trajectory still maintains the advantage of a parabolic ICBM, at its apogee, because its maximum altitude will be 800 km, depending on the configuration of the trajectory of an ICBM and disregarding technical aspects in this assessment, an ICBM will hypothetically have an apogee of 400 km will be 3x stealthier because of its altitude compared to a parabolic ICBM that reaches a peak of 1200 km, the latter being much more easily tracked.
An ICBM with depressed trajectory still maintains the stealth of space-based radar (LEO) due to its apogee, and still takes advantage of land-based radar because of the same altitude advantage, making the ABM system more difficult to track, discriminate the target, and offer firing solution for anti-ballistic missiles.
Comparing:
An ICBM with a depressed trajectory that makes its flight in the atmosphere will be continuously tracked by sensors in space.
A depressed trajectory ICBM that travels out of space, maintaining a depressed altitude but making a space-based tracking solution impractical, will also offer the difficulty of detecting ground-based radar.
I'm even disregarding things like speed, an atmospheric trajectory "ICBM" will lose speed due to drag, but the flight time is shorter. An ICBM with a depressed trajectory in space will have more speed, but its flight time is longer.
Appropriate comparisons are restricted to:
ICBM parabolic trajectory: 10-20% of the trajectory in the atmosphere, more speed, more "flight" time, easier to be tracked both by sensors at sea and on land and to be shot down.
Atmospheric trajectory "ICBM": 80-100% flight in the atmosphere, it will be the vehicle with the lowest speed among those mentioned, it will be the missile with the shortest flight time, the most difficult to be tracked by sensors at sea and on land, it will be continuously tracked by sensors in space.
Depressed space trajectory ICBM: Will fly longer in the atmosphere than the parabolic trajectory missile but will be much shorter than the atmospheric trajectory ICBM, will have more speed than the atmospheric trajectory ICBM, but will have a slower speed than the parabolic trajectory ICBM, it will be much more difficult to track by space-based systems than the atmospheric trajectory ICBM and will maintain the same advantage as the parabolic trajectory ICBM over space sensors, but will have a shorter tracking interval per land- and sea-based systems than the parabolic trajectory ICBM but longer than the atmospheric trajectory ICBM.