are
The maximum and minimum velocities of a satellite
Vmax and Vmin respectively. Pore that the
eccentricity of the orbit of the satellite is
e= (Vmax - Vmin)/(Vmax+Vmin)
Answers
Answered by
4
Answer:
It's maximum and minimum velocities of satellites are 3×10 4m/s and 1×103 m/s respectively
Similar questions
Math,
3 months ago
Computer Science,
3 months ago
English,
3 months ago
Math,
7 months ago
Math,
1 year ago