
What is the lowest practical orbit of the Earth?
What do you mean by the lowest practical orbit of the Earth? Is it the closest point to the Earth's surface that a satellite or spacecraft can maintain without being dragged into the atmosphere and destroyed? Or is it a more nuanced concept, taking into account factors such as fuel efficiency, communication range, and the ability to perform specific scientific or commercial tasks? Could you elaborate on your understanding of the term and its relevance to space exploration and utilization?
