Parameter of Orbit Solution

STEP 0: Pre-Calculation Summary
Formula Used
Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter
p = h^2/μstd
This formula uses 3 Variables
Variables Used
Parameter of Orbit - (Measured in Meter) - Parameter of Orbit is defined as the half of chord length through the center of attraction perpendicular to the apse line.
Angular Momentum of Orbit - (Measured in Squaer Meter per Second) - Angular Momentum of Orbit is a fundamental physical quantity that characterizes the rotational motion of an object in orbit around a celestial body, such as a planet or a star.
Standard Gravitational Parameter - (Measured in Cubic Meter per Square Second) - The Standard Gravitational Parameter of a celestial body is the product of the gravitational constant G and the mass M of the bodies.
STEP 1: Convert Input(s) to Base Unit
Angular Momentum of Orbit: 65611 Square Kilometer per Second --> 65611000000 Squaer Meter per Second (Check conversion ​here)
Standard Gravitational Parameter: 398000000000000 Cubic Meter per Square Second --> 398000000000000 Cubic Meter per Square Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
p = h^2/μstd --> 65611000000^2/398000000000000
Evaluating ... ...
p = 10816088.7462312
STEP 3: Convert Result to Output's Unit
10816088.7462312 Meter -->10816.0887462312 Kilometer (Check conversion ​here)
FINAL ANSWER
10816.0887462312 10816.09 Kilometer <-- Parameter of Orbit
(Calculation completed in 00.020 seconds)

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8 Fundamental Parameters Calculators

Tsiolkovsky Rocket Equation
​ Go Change in Rocket Velocity = Specific Impulse*[g]*ln(Wet Mass/Dry mass)
Radius of Sphere of Influence( Black Hole)
​ Go Sphere of Influence Radius = [G.]*(Black Hole Mass)/(Stellar Velocity Dispersion of the Host Bulge)^2
Semi Major Axis of Phasing Ellipse
​ Go Semi Major Axis of Ellipse = ((Number of Period*Gravitational Parameter^0.5)/(2*pi))^(2/3)
Radius of Sphere of Influence
​ Go Planet 2 radius = (Planet 1 radius/0.001)*(Planet 1 Mass/Planet 2 Mass)^(2/5)
Angular Momentum of Trajectory given Parameter of Orbit
​ Go Angular Momentum of Orbit = sqrt(Parameter of Orbit*[GM.Earth])
Parameter of Orbit
​ Go Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter
Rocket Mass Ratio
​ Go Rocket Mass Ratio = e^(Change in Rocket Velocity/Rocket Exhaust Velocity)
Standard Gravitational Parameter
​ Go Standard Gravitational Parameter = [G.]*(Mass of Orbital Body 1)

Parameter of Orbit Formula

Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter
p = h^2/μstd

What is Semi-latus rectum?

The semi-latus rectum is a parameter used to describe the size and shape of an ellipse in orbital mechanics. It is particularly important in the study of conic sections and Keplerian orbits.

How to Calculate Parameter of Orbit?

Parameter of Orbit calculator uses Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter to calculate the Parameter of Orbit, The Parameter of Orbit formula refers to a set of characteristics or properties that define the shape, size, orientation, and dynamics of an orbiting object's path around a central body. these parameters provide valuable information about the orbit and are essential for describing and analyzing the motion of objects in space. Parameter of Orbit is denoted by p symbol.

How to calculate Parameter of Orbit using this online calculator? To use this online calculator for Parameter of Orbit, enter Angular Momentum of Orbit (h) & Standard Gravitational Parameter std ) and hit the calculate button. Here is how the Parameter of Orbit calculation can be explained with given input values -> 10.81609 = 65611000000^2/398000000000000.

FAQ

What is Parameter of Orbit?
The Parameter of Orbit formula refers to a set of characteristics or properties that define the shape, size, orientation, and dynamics of an orbiting object's path around a central body. these parameters provide valuable information about the orbit and are essential for describing and analyzing the motion of objects in space and is represented as p = h^2/μstd or Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter. Angular Momentum of Orbit is a fundamental physical quantity that characterizes the rotational motion of an object in orbit around a celestial body, such as a planet or a star & The Standard Gravitational Parameter of a celestial body is the product of the gravitational constant G and the mass M of the bodies.
How to calculate Parameter of Orbit?
The Parameter of Orbit formula refers to a set of characteristics or properties that define the shape, size, orientation, and dynamics of an orbiting object's path around a central body. these parameters provide valuable information about the orbit and are essential for describing and analyzing the motion of objects in space is calculated using Parameter of Orbit = Angular Momentum of Orbit^2/Standard Gravitational Parameter. To calculate Parameter of Orbit, you need Angular Momentum of Orbit (h) & Standard Gravitational Parameter std ). With our tool, you need to enter the respective value for Angular Momentum of Orbit & Standard Gravitational Parameter 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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