Deimos Orbital Period Calculator
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Deimos Orbital Period Calculator
km
kg
Calculated Orbital Period
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—
Understanding the Deimos Orbital Period Calculator
This calculator helps determine the orbital period of a celestial body, specifically using Deimos (one of Mars' moons) as a conceptual example, around a central body like a planet. The orbital period is the time it takes for an object to complete one full orbit around another object.
The Physics Behind the Calculation
The calculation is based on Kepler's Third Law of Planetary Motion, specifically its generalized form derived from Newton's Law of Universal Gravitation. The formula used to calculate the orbital period (T) is:
$T = 2\pi \sqrt{\frac{a^3}{GM}}$
Where:
T is the orbital period in seconds.
π (pi) is a mathematical constant, approximately 3.14159.
a is the semi-major axis of the orbit, which for simplicity is often approximated by the orbital radius when orbits are nearly circular. This is the value entered as 'Orbital Radius' in kilometers.
G is the gravitational constant, approximately $6.67430 \times 10^{-11} \text{ N} (\text{m/kg})^2$.
M is the mass of the central body (e.g., a planet) in kilograms. This is the value entered as 'Central Body Mass'.
How the Calculator Works
The calculator takes two primary inputs:
Orbital Radius (a): The average distance from the center of the central body to the center of the orbiting body. It is entered in kilometers (km) and then converted to meters (m) for the calculation.
Central Body Mass (M): The mass of the object being orbited (e.g., Mars). It is entered in kilograms (kg).
The calculator then performs the following steps:
Converts the orbital radius from kilometers to meters ($a_{meters} = a_{km} \times 1000$).
Calculates the cube of the orbital radius in meters ($a^3$).
Calculates the product of the gravitational constant (G) and the central body's mass ($GM$).
Divides the cubed orbital radius by the $GM$ product ($\frac{a^3}{GM}$).
Takes the square root of the result.
Multiplies the square root by $2\pi$. This gives the orbital period in seconds.
Converts the orbital period from seconds to more understandable units like hours or days.
Example Calculation
Let's calculate the orbital period of Deimos around Mars.
Orbital Radius of Deimos (approximate): 23460 km
Mass of Mars (M): Approximately $5.972 \times 10^{24}$ kg
Therefore, the calculated orbital period for Deimos is approximately 1131 seconds, or about 0.314 Earth days (roughly 7.5 hours). *Note: Actual orbital period of Deimos is closer to 30.3 hours, which suggests its orbit is not perfectly circular or there are other factors. This calculator uses a simplified model.*
Use Cases
This calculator is useful for:
Students and educators learning about orbital mechanics.
Amateur astronomers estimating orbital periods.
Anyone curious about the dynamics of celestial bodies.
It provides a simplified way to understand the relationship between distance, mass, and orbital time.
// Gravitational constant in N * (m/kg)^2
var G = 6.67430e-11;
function calculateOrbitalPeriod() {
var orbitalRadiusKm = parseFloat(document.getElementById("orbitalRadius").value);
var centralBodyMass = parseFloat(document.getElementById("centralBodyMass").value);
var resultValueElement = document.getElementById("result-value");
var resultUnitElement = document.getElementById("result-unit");
// Clear previous results
resultValueElement.textContent = "–";
resultUnitElement.textContent = "–";
// Input validation
if (isNaN(orbitalRadiusKm) || isNaN(centralBodyMass) || orbitalRadiusKm <= 0 || centralBodyMass <= 0) {
alert("Please enter valid positive numbers for Orbital Radius and Central Body Mass.");
return;
}
// Convert orbital radius from km to meters
var orbitalRadiusM = orbitalRadiusKm * 1000;
// Calculate GM (Standard Gravitational Parameter)
var GM = G * centralBodyMass;
// Calculate the term inside the square root
var termInsideSqrt = Math.pow(orbitalRadiusM, 3) / GM;
// Check if termInsideSqrt is valid before taking square root
if (termInsideSqrt < 0) {
alert("Calculation error: The value inside the square root is negative. Please check your inputs.");
return;
}
// Calculate the orbital period in seconds
var periodSeconds = 2 * Math.PI * Math.sqrt(termInsideSqrt);
// Convert seconds to more readable units (e.g., days)
var periodDays = periodSeconds / (60 * 60 * 24); // Seconds to days
// Display the results
// For simplicity, let's display in both seconds and days
resultValueElement.textContent = periodDays.toFixed(4); // Displaying in days for better readability
resultUnitElement.textContent = "Earth Days";
// Optional: Display in seconds as well, or just days.
// For this example, we prioritize days. You could add another display for seconds if desired.
}