A satellite of mass 2230 kg is in a geosynchronous orbit (meaning that is orbits in a circle once for ever 24 hr. revolution of the Earth, remaining over the same point on Earth's surface). The satellite orbits at a constant speed and at a distance of 35786 km from Earth's center.
Determine the tangential speed of the satellite.
2.60 m/s
9.37 $\cdot$ 10$^6$ m/s
1491.1 m/s
2602.4 m/s