If ve is the escape velocity and vo is the orbital velocity of a satellite for orbit close to the earth's surface, then these  are related by:

1. \(v_o=v_e\) 2. \(v_e=\sqrt{2v_o}\)
3. \(v_e=\sqrt{2}~v_o\) 4. \(v_o=\sqrt{2}~v_e\)
Subtopic:  Orbital velocity |
 76%
From NCERT
AIPMT - 2012
To view explanation, please take trial in the course.
NEET 2021 - Achiever Batch - Aryan Raj Singh
Hints
Links
To view explanation, please take trial in the course.
NEET 2021 - Achiever Batch - Aryan Raj Singh