Geostationary Height Solution

STEP 0: Pre-Calculation Summary
Formula Used
Geostationary Height = Geostationary Radius-[Earth-R]
Hgso = Rgso-[Earth-R]
This formula uses 1 Constants, 2 Variables
Constants Used
[Earth-R] - Earth mean radius Value Taken As 6371.0088
Variables Used
Geostationary Height - (Measured in Meter) - Geostationary Height refers to the altitude at which a geostationary satellite is positioned above the Earth's equator.
Geostationary Radius - (Measured in Meter) - Geostationary Radius refers to the distance between the Earth's surface and a geostationary satellite in orbit around the Earth.
STEP 1: Convert Input(s) to Base Unit
Geostationary Radius: 6752.8 Kilometer --> 6752800 Meter (Check conversion here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Hgso = Rgso-[Earth-R] --> 6752800-[Earth-R]
Evaluating ... ...
Hgso = 381791.2
STEP 3: Convert Result to Output's Unit
381791.2 Meter -->381.7912 Kilometer (Check conversion here)
FINAL ANSWER
381.7912 Kilometer <-- Geostationary Height
(Calculation completed in 00.004 seconds)

Credits

Created by Shobhit Dimri
Bipin Tripathi Kumaon Institute of Technology (BTKIT), Dwarahat
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Vishwakarma Government Engineering College (VGEC), Ahmedabad
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14 Geostationary Orbit Calculators

Power Density at Satellite Station
Go Power Density at Satellite Station = Effective Isotropic Radiated Power-Path Loss-Total Loss-(10*log10(4*pi))-(20*log10(Range of Satellite))
Earth Station Latitude
Go Earth Station Latitude = Right Angle-Angle of Elevation-Tilt Angle
Angle of Elevation
Go Angle of Elevation = Right Angle-Tilt Angle-Earth Station Latitude
Angle of Tilt
Go Tilt Angle = Right Angle-Angle of Elevation-Earth Station Latitude
Time of Perigee Passage
Go Perigee Passage = Time in Minutes-(Mean Anomaly/Mean Motion)
Satellite Geostationary Radius
Go Geostationary Radius = (([GM.Earth]*Orbital Period in Days)/(4*pi^2))^(1/3)
Geostationary Radius
Go Geostationary Radius = Geostationary Height+[Earth-R]
Geostationary Height
Go Geostationary Height = Geostationary Radius-[Earth-R]
Length of Radius Vectors at Perigee
Go Perigee Radius = Major Orbital Axis*(1-Eccentricity)
Length of Radius Vectors at Apogee
Go Apogee Radius = Major Orbital Axis*(1+Eccentricity)
Acute Value
Go Acute Angle = Straight Angle-Azimuth Angle
Perigee Heights
Go Perigee Height = Perigee Radius-[Earth-R]
Azimuth Angle
Go Azimuth Angle = Straight Angle-Acute Angle
Apogee Heights
Go Apogee Height = Apogee Radius-[Earth-R]

Geostationary Height Formula

Geostationary Height = Geostationary Radius-[Earth-R]
Hgso = Rgso-[Earth-R]

What is difference between geostationary and geosynchronous orbit?

Geosynchronous satellites can have any inclination, the key difference to geostationary orbit is the fact that they lie on the same plane as the equator. Geostationary orbits fall in the same category as geosynchronous orbits, but it's parked over the equator.

How to Calculate Geostationary Height?

Geostationary Height calculator uses Geostationary Height = Geostationary Radius-[Earth-R] to calculate the Geostationary Height, The Geostationary Height formula is the orbital distance above the Earth's equator where a satellite orbits at the same speed as Earth's rotation, maintaining a fixed position relative to the ground. Geostationary Height is denoted by Hgso symbol.

How to calculate Geostationary Height using this online calculator? To use this online calculator for Geostationary Height, enter Geostationary Radius (Rgso) and hit the calculate button. Here is how the Geostationary Height calculation can be explained with given input values -> 0.381791 = 6752800-[Earth-R].

FAQ

What is Geostationary Height?
The Geostationary Height formula is the orbital distance above the Earth's equator where a satellite orbits at the same speed as Earth's rotation, maintaining a fixed position relative to the ground and is represented as Hgso = Rgso-[Earth-R] or Geostationary Height = Geostationary Radius-[Earth-R]. Geostationary Radius refers to the distance between the Earth's surface and a geostationary satellite in orbit around the Earth.
How to calculate Geostationary Height?
The Geostationary Height formula is the orbital distance above the Earth's equator where a satellite orbits at the same speed as Earth's rotation, maintaining a fixed position relative to the ground is calculated using Geostationary Height = Geostationary Radius-[Earth-R]. To calculate Geostationary Height, you need Geostationary Radius (Rgso). With our tool, you need to enter the respective value for Geostationary Radius 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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