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Question: A satellite GeoSAT is in a circular geostationary orbit of radius \(R_{G}\), above a point P on the ...

A satellite GeoSAT is in a circular geostationary orbit of radius RGR_{G}, above a point P on the equator. Another satellite ComSAT is in a lower circular orbit of radius 0.81RG0.81 R_{G} At 77PM on January 11 ComSAT is sighted directly above P. On which day among
the following can ComSAT be sighted directly above P between 77 PM and 88 PM
A) January 3 3
B) January 99
C) January 1515
D) January 2121

Explanation

Solution

Time period of Geostationary satellite is 2424 hours. In the question,
radius and time period are given. So, we will use Kepler’s third Law which gives relation
between time period and radius.
Formula Used:
T is directly related to the orbit semi-major axis through the formula: -
T2R3T^{2} \propto R^{3}
Where, T is the time period of satellite
R is the radius.

Complete answer:
Given-
Radius of geostationary satellite = RGR_{G},
Radius of ComSAT =0.81RG0.81 R_{G},
Time period of geostationary satellite, TGT_{G}= 2424 hours
We have to find the time period of ComSAT. So, we will use Kepler’s third law given by-
T2R3T^{2} \propto R^{3}
Where, T is the time period of satellite
R is the radius.
So, arrange this formula for geostationary satellites and ComSAT.
RG3TG2=Rc3Tc2\dfrac{R_{G}^{3}}{ T_{G}^{2}}= \dfrac{ R_{c}^{3}}{ T_{c}^{2}}
Tc=242×0.81RG3RG3T_{c} = \sqrt{\dfrac{ {24^{2} \times 0.81 R_{G}^{3}}}{{ R_{G}^{3}}}}
Tc=17.496T_{c} =17.496 hours
So, we need to find the day at which ComSAT be sighted directly above P between 77PM
and 88PM
Hours=17.496×11=192.456Hours = 17.496 \times 11 = 192.456 hours
Now we will find days by dividing the hours with 2424.
Days=192.45624=8.019Days = \dfrac {192.456}{24} = 8.019 days
Now, the day from Jan 1+8.01=91+ 8.01 =9January

So, B is the right answer.

Additional Information:
Geostationary satellites possess the unique quality of remaining
fixed in the same state in the sky as seen from any arranged location on Earth, meaning that
ground-based wires do not need to track them but can continue fixed in one direction.

Note:
The time period of the geostationary satellite is not given. so, we will take same time
period as earth has a time period of one day. Noted that square of time period is directly
proportional to the cube of radius. Time period will increase as the radius. T
should be in hours and for days T should be divided by 2424.