Hubble Space Telescope Orbital Period

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SUMMARY

The orbital period of the Hubble Space Telescope, which orbits at an altitude of 610 km, can be calculated using Kepler’s laws. The correct formula is T^2 = (4π²/GM) * r³, where G is 6.67 x 10^-11 and M is the mass of the Earth, 5.98 x 10^24 kg. The radius (r) must include the Earth's radius, resulting in a total radius of approximately 6,990,000 meters. The final calculated orbital period is approximately 96.9 minutes, which aligns with external sources such as Wikipedia.

PREREQUISITES
  • Understanding of Kepler’s laws of planetary motion
  • Familiarity with gravitational constant (G) and Earth's mass (M)
  • Basic algebra for manipulating equations
  • Knowledge of orbital mechanics and satellite motion
NEXT STEPS
  • Study the derivation of Kepler’s laws in detail
  • Learn about the implications of orbital radius in satellite calculations
  • Explore the relationship between velocity and orbital period in circular orbits
  • Investigate the effects of altitude on satellite orbital periods
USEFUL FOR

Astronomy students, aerospace engineers, and anyone interested in satellite dynamics and orbital mechanics will benefit from this discussion.

warmfire540
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Use Kepler’s laws to determine the period of the Hubble Space Telescope which orbits the Earth at an altitude of 610 km.

I'm using the equation i know to find the period of an object revolving around another object

T^2=Kr^3
T^2=(4pi^2/GM)*r^3
G=6.67 x 10^-11
M=5.98× 10^24 (Mass of Earth)
r=610,000

T^2=(39.48/3.99 x 10^14)*2.27 x 10^17
T^2=9.898 x 10^-14*2.27 x 10^17
T^2=22465.81736
T=149.88

I don't know what this means...
but i have another equation for the period of a satelite given by
T=2pi*r/v

mv^2/R+h = GMm/(R+h)^2
v^2/R+h = GM/(R+h)^2
v^2/6.99 x 10^6 = 3.989 x 10^14/4.886 x 10^13
v^2= 8.16 * 6.99 x 10^6
v=7554.3

back to original eqation:
T=2pi*r/v
T=5813.84 seconds
T=96.9 minutes

wikipedia agrees with that number
 
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Hi warmfire540,

warmfire540 said:
Use Kepler’s laws to determine the period of the Hubble Space Telescope which orbits the Earth at an altitude of 610 km.

I'm using the equation i know to find the period of an object revolving around another object

T^2=Kr^3
T^2=(4pi^2/GM)*r^3
G=6.67 x 10^-11
M=5.98× 10^24 (Mass of Earth)
r=610,000

I believe this number is your error; this r is supposed to be the radius of the orbit, so r is the altitude of 610 km plus the radius of the earth.
 

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