Math Problem Statement

A satellite orbits the sun with a period of 2.00 days. What is the radius of its orbit?

Solution

To find the radius of the orbit of the satellite, we will use Kepler's third law of planetary motion. Kepler's third law states that the square of the orbital period TT of a planet (or satellite) is proportional to the cube of the semi-major axis rr of its orbit:

T2=4π2GMr3T^2 = \frac{4\pi^2}{GM} r^3

Where:

  • TT is the orbital period (in seconds),
  • rr is the radius of the orbit,
  • GG is the gravitational constant (6.67430×1011m3/kgs2)(6.67430 \times 10^{-11} \, \text{m}^3/\text{kg}\cdot\text{s}^2),
  • MM is the mass of the Sun (1.989×1030kg)(1.989 \times 10^{30} \, \text{kg}).

Step 1: Convert the orbital period to seconds.

Given: T=2.00 daysT = 2.00 \text{ days} Convert days to seconds: T=2.00×24×3600=172,800 secondsT = 2.00 \times 24 \times 3600 = 172,800 \text{ seconds}

Step 2: Rearrange Kepler's third law to solve for rr.

Rearranging the formula: r3=GMT24π2r^3 = \frac{GMT^2}{4\pi^2}

Step 3: Substitute the values.

r3=(6.67430×1011)(1.989×1030)(172,800)24π2r^3 = \frac{(6.67430 \times 10^{-11})(1.989 \times 10^{30})(172,800)^2}{4\pi^2}

Calculating this expression:

  1. Calculate GMGM: GM=(6.67430×1011)(1.989×1030)=1.327×1020m3/s2GM = (6.67430 \times 10^{-11})(1.989 \times 10^{30}) = 1.327 \times 10^{20} \text{m}^3/\text{s}^2

  2. Calculate T2T^2: T2=(172,800)2=2.985×1010s2T^2 = (172,800)^2 = 2.985 \times 10^{10} \text{s}^2

  3. Compute r3r^3: r3=(1.327×1020)(2.985×1010)4π2=6.47×1020m3r^3 = \frac{(1.327 \times 10^{20})(2.985 \times 10^{10})}{4\pi^2} = 6.47 \times 10^{20} \text{m}^3

Step 4: Take the cube root to find rr.

r=6.47×102038.67×106kmr = \sqrt[3]{6.47 \times 10^{20}} \approx 8.67 \times 10^{6} \text{km}

Thus, the radius of the orbit is approximately 8.67×106km8.67 \times 10^{6} \text{km}.

Would you like further details or have questions about this calculation?

Related Questions

  1. How does Kepler's third law help in understanding satellite motion?
  2. What factors can influence the period of a satellite's orbit around the Sun?
  3. How do orbital radius and speed correlate for satellites orbiting the Sun?
  4. What is the relationship between gravitational force and orbital motion?
  5. How would the period change if the satellite were further from the Sun?

Tip

Remember, Kepler's laws apply to any two-body system where one body is much more massive than the other, such as a planet and a satellite.

Ask a new question for Free

By Image

Drop file here or Click Here to upload

Math Problem Analysis

Mathematical Concepts

Orbital Mechanics
Kepler's Laws
Gravitational Force

Formulas

T^2 = (4π^2 / GM) r^3
r^3 = (GMT^2) / 4π^2

Theorems

Kepler's Third Law of Planetary Motion

Suitable Grade Level

Undergraduate Physics or Advanced High School (Grades 11-12)