X Coordinate of Parabolic Trajectory given Parameter of Orbit Solution

STEP 0: Pre-Calculation Summary
Formula Used
X Coordinate Value = Parameter of Parabolic Orbit*(cos(True Anomaly in Parabolic Orbit)/(1+cos(True Anomaly in Parabolic Orbit)))
x = pp*(cos(θp)/(1+cos(θp)))
This formula uses 1 Functions, 3 Variables
Functions Used
cos - Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle., cos(Angle)
Variables Used
X Coordinate Value - (Measured in Meter) - X Coordinate Value is the distance of the object in horizontal direction from the origin.
Parameter of Parabolic Orbit - (Measured in Meter) - Parameter of Parabolic Orbit is defined as the half of chord length through the center of attraction perpendicular to the apse line.
True Anomaly in Parabolic Orbit - (Measured in Radian) - True Anomaly in Parabolic Orbit measures the angle between the object's current position and the perigee (the point of closest approach to the central body) when viewed from the focus of the orbit.
STEP 1: Convert Input(s) to Base Unit
Parameter of Parabolic Orbit: 10800 Kilometer --> 10800000 Meter (Check conversion ​here)
True Anomaly in Parabolic Orbit: 115 Degree --> 2.0071286397931 Radian (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
x = pp*(cos(θp)/(1+cos(θp))) --> 10800000*(cos(2.0071286397931)/(1+cos(2.0071286397931)))
Evaluating ... ...
x = -7905129.17944648
STEP 3: Convert Result to Output's Unit
-7905129.17944648 Meter -->-7905.12917944649 Kilometer (Check conversion ​here)
FINAL ANSWER
-7905.12917944649 -7905.129179 Kilometer <-- X Coordinate Value
(Calculation completed in 00.020 seconds)

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Parabolic Orbit Parameters Calculators

X Coordinate of Parabolic Trajectory given Parameter of Orbit
​ LaTeX ​ Go X Coordinate Value = Parameter of Parabolic Orbit*(cos(True Anomaly in Parabolic Orbit)/(1+cos(True Anomaly in Parabolic Orbit)))
Y Coordinate of Parabolic Trajectory given Parameter of Orbit
​ LaTeX ​ Go Y Coordinate Value = Parameter of Parabolic Orbit*sin(True Anomaly in Parabolic Orbit)/(1+cos(True Anomaly in Parabolic Orbit))
Escape Velocity given Radius of Parabolic Trajectory
​ LaTeX ​ Go Escape Velocity in Parabolic Orbit = sqrt((2*[GM.Earth])/Radial Position in Parabolic Orbit)
Radial Position in Parabolic Orbit given Escape Velocity
​ LaTeX ​ Go Radial Position in Parabolic Orbit = (2*[GM.Earth])/Escape Velocity in Parabolic Orbit^2

X Coordinate of Parabolic Trajectory given Parameter of Orbit Formula

​LaTeX ​Go
X Coordinate Value = Parameter of Parabolic Orbit*(cos(True Anomaly in Parabolic Orbit)/(1+cos(True Anomaly in Parabolic Orbit)))
x = pp*(cos(θp)/(1+cos(θp)))

What causes a parabolic trajectory ?

Projectiles travel with a parabolic trajectory due to the fact that the downward force of gravity accelerates them downward from their otherwise straight-line, gravity-free trajectory.

How to Calculate X Coordinate of Parabolic Trajectory given Parameter of Orbit?

X Coordinate of Parabolic Trajectory given Parameter of Orbit calculator uses X Coordinate Value = Parameter of Parabolic Orbit*(cos(True Anomaly in Parabolic Orbit)/(1+cos(True Anomaly in Parabolic Orbit))) to calculate the X Coordinate Value, The X Coordinate of Parabolic Trajectory given Parameter of Orbit formula is defined as distance of the object in horizontal direction from the origin. X Coordinate Value is denoted by x symbol.

How to calculate X Coordinate of Parabolic Trajectory given Parameter of Orbit using this online calculator? To use this online calculator for X Coordinate of Parabolic Trajectory given Parameter of Orbit, enter Parameter of Parabolic Orbit (pp) & True Anomaly in Parabolic Orbit p) and hit the calculate button. Here is how the X Coordinate of Parabolic Trajectory given Parameter of Orbit calculation can be explained with given input values -> -7.905129 = 10800000*(cos(2.0071286397931)/(1+cos(2.0071286397931))).

FAQ

What is X Coordinate of Parabolic Trajectory given Parameter of Orbit?
The X Coordinate of Parabolic Trajectory given Parameter of Orbit formula is defined as distance of the object in horizontal direction from the origin and is represented as x = pp*(cos(θp)/(1+cos(θp))) or X Coordinate Value = Parameter of Parabolic Orbit*(cos(True Anomaly in Parabolic Orbit)/(1+cos(True Anomaly in Parabolic Orbit))). Parameter of Parabolic Orbit is defined as the half of chord length through the center of attraction perpendicular to the apse line & True Anomaly in Parabolic Orbit measures the angle between the object's current position and the perigee (the point of closest approach to the central body) when viewed from the focus of the orbit.
How to calculate X Coordinate of Parabolic Trajectory given Parameter of Orbit?
The X Coordinate of Parabolic Trajectory given Parameter of Orbit formula is defined as distance of the object in horizontal direction from the origin is calculated using X Coordinate Value = Parameter of Parabolic Orbit*(cos(True Anomaly in Parabolic Orbit)/(1+cos(True Anomaly in Parabolic Orbit))). To calculate X Coordinate of Parabolic Trajectory given Parameter of Orbit, you need Parameter of Parabolic Orbit (pp) & True Anomaly in Parabolic Orbit p). With our tool, you need to enter the respective value for Parameter of Parabolic Orbit & True Anomaly in Parabolic Orbit 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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