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Orbital Period of Satellite in Minutes Calculator

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Satellite Orbital Characteristics Geostationary Orbit Radio Wave Propagation

✖Mean Motion is angular speed required for a body to complete an orbit, assuming constant speed in circular orbit that takes same time as variable speed elliptical orbit of actual body.ⓘ Mean Motion [n]

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✖Orbital Period in Minutes is the number of minutes a given astronomical object takes to complete one orbit around another object.ⓘ Orbital Period of Satellite in Minutes [P_min]

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Orbital Period of Satellite in Minutes Solution

STEP 0: Pre-Calculation Summary

Formula Used

Orbital Period in Minutes = 2*pi/Mean Motion
P_min = 2*pi/n
This formula uses 1 Constants, 2 Variables

Constants Used

pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288

Variables Used

Orbital Period in Minutes - (Measured in Second) - Orbital Period in Minutes is the number of minutes a given astronomical object takes to complete one orbit around another object.
Mean Motion - (Measured in Radian per Second) - Mean Motion is angular speed required for a body to complete an orbit, assuming constant speed in circular orbit that takes same time as variable speed elliptical orbit of actual body.

STEP 1: Convert Input(s) to Base Unit

Mean Motion: 0.045 Radian per Second --> 0.045 Radian per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

P_min = 2*pi/n --> 2*pi/0.045

Evaluating ... ...

P_min = 139.626340159546

STEP 3: Convert Result to Output's Unit

139.626340159546 Second -->2.32710566932577 Minute (Check conversion here)

FINAL ANSWER

2.32710566932577 ≈ 2.327106 Minute <-- Orbital Period in Minutes

(Calculation completed in 00.004 seconds)

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Created by Shobhit Dimri

Bipin Tripathi Kumaon Institute of Technology (BTKIT), Dwarahat

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< Satellite Orbital Characteristics Calculators

Mean Anomaly

LaTeX Go Mean Anomaly = Eccentric Anomaly-Eccentricity*sin(Eccentric Anomaly)

Mean Motion of Satellite

LaTeX Go Mean Motion = sqrt([GM.Earth]/Semi Major Axis^3)

Local Sidereal Time

LaTeX Go Local Sidereal Time = Greenwich Sidereal Time+East Longitude

Anomalistic Period

LaTeX Go Anomalistic Period = (2*pi)/Mean Motion

Orbital Period of Satellite in Minutes Formula

LaTeX Go

Orbital Period in Minutes = 2*pi/Mean Motion
P_min = 2*pi/n

What is Earth's Orbital Period?

Earth orbits the Sun at an average distance of 149.60 million km (92.96 million mi), and one complete orbit takes 365.256 days (1 sidereal year), during which time Earth has traveled 940 million km (584 million mi).

How to Calculate Orbital Period of Satellite in Minutes?

Orbital Period of Satellite in Minutes calculator uses Orbital Period in Minutes = 2*pi/Mean Motion to calculate the Orbital Period in Minutes, The Orbital Period of Satellite in Minutes formula is defined as the time a given astronomical object takes to complete one orbit around another object, and applies in astronomy usually to planets or asteroids orbiting the Sun, moons orbiting planets, exoplanets orbiting other stars, or binary stars. Orbital Period in Minutes is denoted by P_min symbol.

How to calculate Orbital Period of Satellite in Minutes using this online calculator? To use this online calculator for Orbital Period of Satellite in Minutes, enter Mean Motion (n) and hit the calculate button. Here is how the Orbital Period of Satellite in Minutes calculation can be explained with given input values -> 0.038785 = 2*pi/0.045.

FAQ

What is Orbital Period of Satellite in Minutes?

The Orbital Period of Satellite in Minutes formula is defined as the time a given astronomical object takes to complete one orbit around another object, and applies in astronomy usually to planets or asteroids orbiting the Sun, moons orbiting planets, exoplanets orbiting other stars, or binary stars and is represented as P_min = 2*pi/n or Orbital Period in Minutes = 2*pi/Mean Motion. Mean Motion is angular speed required for a body to complete an orbit, assuming constant speed in circular orbit that takes same time as variable speed elliptical orbit of actual body.

How to calculate Orbital Period of Satellite in Minutes?

The Orbital Period of Satellite in Minutes formula is defined as the time a given astronomical object takes to complete one orbit around another object, and applies in astronomy usually to planets or asteroids orbiting the Sun, moons orbiting planets, exoplanets orbiting other stars, or binary stars is calculated using Orbital Period in Minutes = 2*pi/Mean Motion. To calculate Orbital Period of Satellite in Minutes, you need Mean Motion (n). With our tool, you need to enter the respective value for Mean Motion and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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