Semi Major Axis of Phasing Ellipse Solution

STEP 0: Pre-Calculation Summary
Formula Used
Semi Major Axis of Ellipse = ((Number of Period*Gravitational Parameter^0.5)/(2*pi))^(2/3)
a = ((n*μ^0.5)/(2*pi))^(2/3)
This formula uses 1 Constants, 3 Variables
Constants Used
pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288
Variables Used
Semi Major Axis of Ellipse - (Measured in Meter) - The Semi Major Axis of Ellipse value is denoted by the symbol a.
Number of Period - The Number of Periods is the periods on an annuity using the present value, periodic payment, and periodic rate.
Gravitational Parameter - 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
Number of Period: 2 --> No Conversion Required
Gravitational Parameter: 398600 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
a = ((n*μ^0.5)/(2*pi))^(2/3) --> ((2*398600^0.5)/(2*pi))^(2/3)
Evaluating ... ...
a = 34.3093520554891
STEP 3: Convert Result to Output's Unit
34.3093520554891 Meter -->0.0343093520554891 Kilometer (Check conversion ​here)
FINAL ANSWER
0.0343093520554891 0.034309 Kilometer <-- Semi Major Axis of Ellipse
(Calculation completed in 00.020 seconds)

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Mahatma Gandhi Institute of Technology (MGIT), Hyderabad
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Standard Gravitational Parameter
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Semi Major Axis of Phasing Ellipse Formula

​LaTeX ​Go
Semi Major Axis of Ellipse = ((Number of Period*Gravitational Parameter^0.5)/(2*pi))^(2/3)
a = ((n*μ^0.5)/(2*pi))^(2/3)

What is orbit phasing ?

Orbit phasing is the adjustment of the time-position of spacecraft along its orbit, usually described as adjusting the orbiting spacecraft's true anomaly.

How to Calculate Semi Major Axis of Phasing Ellipse?

Semi Major Axis of Phasing Ellipse calculator uses Semi Major Axis of Ellipse = ((Number of Period*Gravitational Parameter^0.5)/(2*pi))^(2/3) to calculate the Semi Major Axis of Ellipse, Semi Major Axis of Phasing Ellipse refers to the longest radius of the ellipse used to describe the relative positions of two objects in space during orbital maneuvers, particularly in the context of orbital rendezvous and docking maneuvers. Semi Major Axis of Ellipse is denoted by a symbol.

How to calculate Semi Major Axis of Phasing Ellipse using this online calculator? To use this online calculator for Semi Major Axis of Phasing Ellipse, enter Number of Period (n) & Gravitational Parameter (μ) and hit the calculate button. Here is how the Semi Major Axis of Phasing Ellipse calculation can be explained with given input values -> 3.4E-5 = ((2*398600^0.5)/(2*pi))^(2/3).

FAQ

What is Semi Major Axis of Phasing Ellipse?
Semi Major Axis of Phasing Ellipse refers to the longest radius of the ellipse used to describe the relative positions of two objects in space during orbital maneuvers, particularly in the context of orbital rendezvous and docking maneuvers and is represented as a = ((n*μ^0.5)/(2*pi))^(2/3) or Semi Major Axis of Ellipse = ((Number of Period*Gravitational Parameter^0.5)/(2*pi))^(2/3). The Number of Periods is the periods on an annuity using the present value, periodic payment, and periodic rate & Gravitational Parameter of a celestial body is the product of the gravitational constant G and the mass M of the bodies.
How to calculate Semi Major Axis of Phasing Ellipse?
Semi Major Axis of Phasing Ellipse refers to the longest radius of the ellipse used to describe the relative positions of two objects in space during orbital maneuvers, particularly in the context of orbital rendezvous and docking maneuvers is calculated using Semi Major Axis of Ellipse = ((Number of Period*Gravitational Parameter^0.5)/(2*pi))^(2/3). To calculate Semi Major Axis of Phasing Ellipse, you need Number of Period (n) & Gravitational Parameter (μ). With our tool, you need to enter the respective value for Number of Period & 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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