Two satellites orbit the earth in circular orbits of the same radius.
Two artificial satellites are of same mass moving around the earth.
Time for one orbit is 24 hours.
B cannot overtake a by increasing its speed.
Geostationary orbit geo 36 000 km above the earth.
It s the same d.
The centripetal force is whatever force is causing the centripetal acceleration.
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.
D the one with the large mass.
C the one with smaller mass.
Which is an accurate statement.
If the mass of the earth was quadrupled and nothing else was changed.
Two satellites a and b of the same mass are going around earth in concentric orbits.
The distance of satellite b from earth s center is twice that of satellite 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.
However the presence of satellites in eccentric orbits allows for collisions at up to 4 km s.
It will then go into a different orbit.
Which of the two will be moving more slowly in its orbit.
As time period of different satellites are equal so r will be same for both satellites.
Two satellites a b are in the same orbit around the earth b being behind a.
The following statements refer to man made artificial satellites in orbit around earth.
What is the ratio of the centripetal force acting on b compared to that acting on a.
Two debris fields are shown.
Around geostationary space and low earth orbit.
Two artificial satellites are in circular orbits about the earth.
The distance of satellite b from earth s center is twice that of satellite a.
One satellite is twice as massive as the other.
Medium earth orbit meo most meo satellites are at an altitude of 20 000 km and time for one orbit is 12 hours.
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.