Ansy Mearth 5.9 8 X 1024 8x1024 kg G = 6.67X10 Nm Nm2/kg 2 6.38 X10m + 1.6x106m 7.98 X10 ra 6 T= za 83 GM 2x 3.14 X (7.9881063 6,67 X10-1) X 5.98 X 1024 6.28 x 12.74 X 105 T= 6,28 x 508.1696X 1018 39.887 X 1013 6.28 X 10PX 11.2872 T 11 7.09 X103 seconds T = 4. 18. X103 minute
For the answer please have the correct number of signifcant figures What is the orbital period...
What speed must a satellite have if it is to move in a circular orbit of 610 km above the surface of the Earth? (The Earth's radius is 6400 km and the Earth's mass is 5.98*1024 kg.)
A particular satellite was placed in a circular orbit about 163 mi above Earth. (a) Determine the orbital speed of the satellite. m/s (b) Determine the time required for one complete revolution. min 1024 kg.) An artificial satellite circling the Earth completes each orbit in 119 minutes. (The radius of the Earth is 6.38 x 106 m. The mass of the Earth is 5.98 (a) Find the altitude of the satellite. m (b) What is the value of g at...
A satellite circles the earth in an orbit whose radius is 2.84 times the earth's radius. The earth's mass is 5.98 x 1024 kg, and its radius is 6.38 x 10m. What is the period of the satellite? Number 187.01 Units 5
Find the height H of a geosynchronous satellite above the surface of the earth. You may well want to find the radius of the orbit R first. You may use the following constants: The universal gravitational constant G is 6.67×10−11Nm2/kg2. The mass of the earth is 5.98×1024kg. The mass of the satellite is 2.10×102kg. The radius of the earth is 6.38×106m. Give the height of the orbit above the surface in km to three significant digits.
10-3. A 639-kg satellite is in a circular orbit about Earth at a height h = 1.16 x 10^7 m above the Earth’s surface. Find (a) the gravitational force (N) acting on the satellite, (b) the satellite’s speed (m/s) (magnitude of its velocity, not its angular velocity), and (c) the period (h) of its revolution. Caution: The radius of the satellite’s orbit is not just its height above the Earth’s surface. It also includes the radius of the Earth. The...
A satellite is in a circular orbit about the Earth at a distance of four (4) Earth radii above the surface of the Earth. What is the velocity of the satellite? (Earth's mass: ME = 5.98 x 1024 kg; the radius of the Earth: 6.4 x 106m ; G = 6.67 x 10-11 Nm2/kg2 ). A) 4,072.5 m/s B)3,530.5 m/s C)5,582.2 m/s D)7,465.9 m/s
What is the orbital speed of a satelite in a circular orbit at 8, 129 kilometers above the Earth surface? Express your answer in km/s and round it to two decimals. Earth's mean radius is RE = 6.37 x100 m; Earth's mass is ME = 5.97x104kg. A What is the orbital period of a satelite in a circular orbit at 5,384 kilometers above the Earth surface? Express your answer in minutes (enter "min" for minutes) and round it to the...
A satellite in low Earth orbit is 225km above the surface. What is its orbital velocity. Mass of earth= 6 x 10^24 kg. Radius of earth = 6.38 x 10^6m
help with this please ASAP a satelite with mass 500 kg is placed in a circular orbit about Earth ( Mass= 5.98 x 10^24 kg) radius =6.4 x 10^6. a distance of 1500 km above the surface a) what is the force gravity acting on satellite? b) what is the satellite’s acceleration? c) what is the satellite’s orbital speed?
Derive the "Clarke radius", the altitude above the surface of the Earth where a satellite in a circular orbit has an orbital period of exactly one day. Assume a spherical Earth, and use the following constants (taken from Vallado, David A., Fundamentals of Astrodynamics and Applications, 2nd ed. 2001) Gravitational constant: G 6.673 x 10-20 km Radius of the Earth: Re = 6378.137 km 1024 kg Mass of the Earth: Me = 5.9733328 x Round your final answer to four...