Not LEO but just above the Karman line
The alternative, actual LEO (orbit):
I don't think anyone is going to be deploying cubesats at 100 km, MECO (main engine cutoff) is below that, looks like roughly 70 km and you'll be passing Karman during the middle of 2nd stage burn, not a time when anyone will want to be deploying cubesats.
The lowest altitude regular deployments would be the Starlinks at roughly 250 km, you can check if they do concurrent cubesat deployments.
Certainly there are from time to time missions launched at very low altitude, and some might have concurrent secondary payload programs for cubesats.
Atomic oxygen and space weathering (erosion) - beware!
note: Become very familiar with the effects of atomic oxygen (O rather than O2) on the materials on the outside and the inside of your spacecraft!
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- What are the long term effects of Space Weathering on man-made materials?
Also related to VLEO (Very Low Earth Orbit):
- What technologies enable or at least help satellite operation in Very Low Earth Orbit (VLEO)?
- How to calculate the lowest possible altitude a satellite can orbit at due to aerodynamic heating if provided with a sufficient propulsion system?
- What is Direct Simulation Monte Carlo and why is it a good method for simulating spacecraft drag in VLEO?
- How low is VLEO? (FCC's newest approval for SpaceX)
- Why is ~280 km one month before reentry the lowest altitude that the final ISS crew may see? Isn't that cutting it kinda close?
- What is the lowest altitude that an ion thruster can be used for station keeping?
- What's the lowest altitude that an ion engine has been used for a significant orbital maneuver?