original question: What are other functions supported by those rockets that support [Low Earth orbit]?
answer: launch vehicle, lunar launch vehicle, manned leo
answer type: Rocket Function.
auxiliary information: A low Earth orbit is an orbit around Earth with an altitude between 160 kilometers, and 2,000 kilometers. Objects below approximately 160 kilometers will experience very rapid orbital decay and altitude loss. The orbital velocity needed to maintain a stable low Earth orbit is about 7.8 km/s, but reduces with increased orbital altitude. With the exception of the manned lunar flights of the Apollo program, all human spaceflights have taken place in LEO. The altitude record for a human spaceflight in LEO was Gemini 11 with an apogee of 1,374.1 kilometers. All manned space stations to date, as well as the majority of satellites, have been in LEO.
When it comes to the rockets that support [Low Earth orbit] what are the functions supported?