Two Artificial Satellites Are Of Same Mass Moving Around The Earth

Two satellites a and b of the same mass are going around earth in concentric orbits.

Two artificial satellites are of same mass moving around the earth.

Geostationary orbit geo 36 000 km above the earth. Time period of artificial satellite is given as t 2π r gm where m is mass of the earth and r is the radius of path where satellite is orbiting. The distance of satellite b from earth s center is twice that of satellite a. This is to match the rotation of the earth so that the satellite appears to stay above the same point above the earth s surface.

As time period of different satellites are equal so r will be same for both satellites. The distance of satellite b from earth s center is twice that of satellite a. What is the ratio of the centripetal force acting on b compared to that acting on a. It s the same d.

Two satellites orbit the earth in circular orbits of the same radius. If the mass of the earth was quadrupled and nothing else was changed. Which is an accurate statement. C the one with smaller mass.

B cannot overtake a by increasing its speed. Which of the two will be moving more slowly in its orbit. Medium earth orbit meo most meo satellites are at an altitude of 20 000 km and time for one orbit is 12 hours. One satellite is twice as massive as the other.

Time for one orbit is 24 hours. Two artificial satellites are in circular orbits about the earth. Space debris at geostationary orbits typically has a lower collision speed than at leo since all geo satellites orbit in the same plane altitude and speed. The following statements refer to man made artificial satellites in orbit around earth.

It will then go into a different orbit. The centripetal force is whatever force is causing the centripetal acceleration. Two debris fields are shown. Two satellites a and b of the same mass are going around earth in concentric orbits.

What is the ratio of the centripetal force acting on b to that acting on a. Two satellites of mass m1 and m2 m1 m2 are revolving around the earth in orbits of radii r1 and r2 r1 r2 with velocities v1 and v2 respectively in this case 1 v1 v2. Around geostationary space and low earth orbit.