How do i find geosynch orbit for an imaginary planet?
The question is: i have a planet with:
Radius 4935.8
... and want to have a satellite in a proper geostationary orbit around it. How do i find the semimajoraxis for the satellite?
-rthorvald
World-building question: how to...
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rthorvald,
I don't know if this link that uses the planet Earth as the example will also help you ?
http://www.satcom.co.uk/print.asp?article=11
I don't know if this link that uses the planet Earth as the example will also help you ?
http://www.satcom.co.uk/print.asp?article=11
1.6.0:AMDAth1.2GHz 1GbDDR266:Ge6200 256mbDDR250:WinXP-SP3:1280x1024x32FS:v196.21@AA4x:AF16x:IS=HQ:T.Buff=ON Earth16Kdds@15KkmArctic2000AD:FOV1:SPEC L5dds:NORM L5dxt5:CLOUD L5dds:
NIGHT L5dds:MOON L4dds:GALXY ON:MAG 15.2-SAP:TIME 1000x:RP=OGL2:10.3FPS
NIGHT L5dds:MOON L4dds:GALXY ON:MAG 15.2-SAP:TIME 1000x:RP=OGL2:10.3FPS
granthutchison wrote:you need to know the rotation period (P) and the mass (M).
Then the required semimajor axis (a) is given by:
a^3 = G*M*P^2/(4*pi^2)
Thanks. Though i can?t read that formula; regrettably, i haven?t learned the language
I can read and use it if you tell me what the symbol ^ means... (Sorry for stupid questions).
I got this off stargen.
The mass is 2.7E+24Kg
Rotationperiod (lenght of day) is 23.10 hours
-rthorvald
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rthorvald wrote:I can read and use it if you tell me what the symbol ^ means... (Sorry for stupid questions).
It means "to the power" (but you could type it into a spreadsheet and get the answer even if you didn't know what it meant).
So:
a cubed = 6.67E-11*2.7E+24*(23.10*3600)*(23.10*3600)/(4*pi*pi)
a cubed = 3.155E+22m
a ~ 31600km
You can get the same result more easily if you use Earth-units: the rotation period is 0.965 Earth rotation periods; the mass is 0.452 Earth masses. So the synchronous radius for your planet (in multiples of Earth's synchronous radius) is:
a cubed = 0.965*0.965*0.452
a cubed = 0.421
a = 0.749
Since Earth's synchronous radius is 42164km, a = 42164*0.749 ~ 31600km.
Same result, different route.
Grant
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The radius is irrelevant: you need to know the rotation period (P) and the mass (M).
Well, since Celestia planets don't have mass, how do I create a sinchronous orbit? I tried using the formula, but the math just didn't work, specially because my fake planet lacks a precise mass number.
I'm not trying to be precise or anything, so I thought: wouldn't it work like a big disk does? If the satelite has an orbital period equal to the rotation of the planet, wouldn't it make it circle around the same point?
I'm just asking coz I spent this whole afternoon over a papersheet covered with 11 digit numbers and a lot of mistakes, and yet it does not work.
thanks anyway
Tanketai wrote: If the satelite has an orbital period equal to the rotation of the planet, wouldn't it make it circle around the same point?
Yes, it will. The RotationPeriod of the planet should be equal to the Period of the satellite.
But the RotationPeriod of both planets and satellites are noted in hours, while the Period of Planets are noted in years, and the Period of Satellites are noted in DAYS.
So, to set the satellite in geosynch, you will have convert the planet??s RotationPeriod (hours) into days for the satellite Period.
-rthorvald