Deimos Calculator

Deimos Orbital Period Calculator body { font-family: 'Segoe UI', Tahoma, Geneva, Verdana, sans-serif; line-height: 1.6; margin: 0; padding: 20px; background-color: #f8f9fa; color: #333; } .loan-calc-container { max-width: 700px; margin: 30px auto; padding: 30px; background-color: #ffffff; border-radius: 8px; box-shadow: 0 4px 15px rgba(0, 74, 153, 0.1); border: 1px solid #e0e0e0; } h1, h2 { color: #004a99; text-align: center; margin-bottom: 25px; } .input-group { margin-bottom: 20px; display: flex; align-items: center; gap: 15px; flex-wrap: wrap; /* Allows wrapping on smaller screens */ } .input-group label { flex: 1; /* Takes available space */ min-width: 150px; /* Ensures labels don't get too small */ font-weight: 500; color: #004a99; } .input-group input[type="number"], .input-group input[type="text"] { flex: 2; /* Takes twice the space of the label */ padding: 10px 12px; border: 1px solid #ced4da; border-radius: 4px; font-size: 1rem; transition: border-color 0.2s ease-in-out, box-shadow 0.2s ease-in-out; box-sizing: border-box; /* Include padding and border in the element's total width and height */ } .input-group input[type="number"]:focus, .input-group input[type="text"]:focus { border-color: #004a99; outline: none; box-shadow: 0 0 0 0.2rem rgba(0, 74, 153, 0.25); } .input-group span { font-size: 0.9rem; color: #6c757d; margin-left: auto; /* Pushes the unit to the right */ min-width: 60px; /* Prevents units from shrinking too much */ } button { display: block; width: 100%; padding: 12px 20px; background-color: #28a745; color: white; border: none; border-radius: 5px; font-size: 1.1rem; font-weight: bold; cursor: pointer; transition: background-color 0.2s ease-in-out, transform 0.1s ease-in-out; margin-top: 20px; } button:hover { background-color: #218838; transform: translateY(-2px); } button:active { transform: translateY(0); } #result { margin-top: 30px; padding: 20px; background-color: #e9ecef; border: 1px solid #dee2e6; border-radius: 5px; text-align: center; } #result h3 { margin-top: 0; color: #004a99; font-size: 1.3rem; } #result-value { font-size: 2.5rem; font-weight: bold; color: #28a745; display: block; /* Ensures it takes its own line */ margin-top: 10px; } .article-content { margin-top: 40px; padding: 25px; background-color: #ffffff; border-radius: 8px; box-shadow: 0 4px 15px rgba(0, 74, 153, 0.1); border: 1px solid #e0e0e0; } .article-content h2 { color: #004a99; text-align: left; margin-bottom: 15px; } .article-content p, .article-content ul, .article-content li { margin-bottom: 15px; color: #555; } .article-content li { margin-left: 20px; } .article-content strong { color: #004a99; } /* Responsive adjustments */ @media (max-width: 768px) { .input-group { flex-direction: column; /* Stack input groups vertically */ align-items: stretch; /* Make items fill width */ gap: 10px; } .input-group label, .input-group input[type="number"], .input-group input[type="text"], .input-group span { flex: none; /* Reset flex properties for stacking */ width: 100%; /* Full width */ text-align: left; /* Align text left */ } .input-group span { margin-left: 0; /* Remove auto margin */ margin-top: 5px; /* Add some space above the unit */ } #result-value { font-size: 2rem; } }

Deimos Orbital Period Calculator

km
kg

Calculated Orbital Period

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:

  1. Converts the orbital radius from kilometers to meters ($a_{meters} = a_{km} \times 1000$).
  2. Calculates the cube of the orbital radius in meters ($a^3$).
  3. Calculates the product of the gravitational constant (G) and the central body's mass ($GM$).
  4. Divides the cubed orbital radius by the $GM$ product ($\frac{a^3}{GM}$).
  5. Takes the square root of the result.
  6. Multiplies the square root by $2\pi$. This gives the orbital period in seconds.
  7. 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

1. Convert radius to meters: $23460 \text{ km} \times 1000 \text{ m/km} = 23,460,000 \text{ m}$ 2. Calculate $a^3$: $(2.346 \times 10^7 \text{ m})^3 \approx 1.292 \times 10^{22} \text{ m}^3$ 3. Calculate $GM$: $(6.67430 \times 10^{-11} \text{ N} (\text{m/kg})^2) \times (5.972 \times 10^{24} \text{ kg}) \approx 3.986 \times 10^{14} \text{ m}^3/\text{s}^2$ 4. Calculate $\frac{a^3}{GM}$: $(1.292 \times 10^{22} \text{ m}^3) / (3.986 \times 10^{14} \text{ m}^3/\text{s}^2) \approx 32409 \text{ s}^2$ 5. Calculate $\sqrt{\frac{a^3}{GM}}$: $\sqrt{32409 \text{ s}^2} \approx 180.03 \text{ s}$ 6. Calculate T: $2\pi \times 180.03 \text{ s} \approx 1131.1 \text{ s}$ 7. Convert to hours: $1131.1 \text{ s} / (3600 \text{ s/hr}) \approx 0.314 \text{ hours}$. This is approximately 18.8 hours.

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. }

Leave a Comment