In addition to orbital velocity (~1.7 km/s) and gravity losses (~0.2 km/s?) you should take into account all safety reserves - Eagle could hang a minute or more

In addition to orbital velocity (~1.7 km/s) and gravity losses (~0.2 km/s?) you should take into account all safety reserves - Eagle could hang a minute or more above the surface selecting the place to land. Given that we can't ignore safety, it's better to budget 2200-2500 m/s delta-V to get from the Moon orbit to the Moon surface. We need both Lagrange point stations and surface bases. It's arguable what should go first; an argument for Lagrange station is that it's easier to build.