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Calculators Created by Harsh Raj
Harsh Raj
Indian Institute of Technology, Kharagpur
(IIT KGP)
,
Kharagpur, West Bengal
44
Formulas Created
0
Formulas Verified
8
Across Categories
List of Calculators by Harsh Raj
Following is a combined list of all the calculators that have been created and verified by Harsh Raj. Harsh Raj has created 44 and verified 0 calculators across 8 different categories till date.
Angular Momentum
(4)
Created
Angular Momentum given Perigee Radius of Parabolic Orbit
Go
Created
Perigee Radius of Parabolic Orbit given Angular Momentum
Go
Created
Radial Position in Parabolic Orbit given Angular Momentum and True Anomaly
Go
Created
True Anomaly in Parabolic Orbit given Radial Position and Angular Momentum
Go
Circular Orbits
(1)
Created
Speed of Satellite in Circular LEO as Function of Altitude
Go
9 More Circular Orbits Calculators
Go
Elliptical Orbits
(11)
Created
Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity
Go
Created
Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity
Go
Created
Apogee Radius of Elliptic Orbit Given Angular Momentum and Eccentricity
Go
Created
Apogee Velocity in Elliptic Orbit Given Angular Momentum and Apogee Radius
Go
Created
Azimuth-Averaged Radius Given Apogee and Perigee Radii
Go
Created
Eccentricity of Elliptical Orbit given Apogee and Perigee
Go
Created
Elliptical Orbit Time Period given Angular Momentum and Eccentricity
Go
Created
Radial Velocity in Elliptic Orbit given Radial Position and Angular Momentum
Go
Created
Radial Velocity in Elliptic Orbit given True Anomaly, Eccentricity, and Angular Momentum
Go
Created
Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii
Go
Created
True Anomaly in Elliptic Orbit Given Radial Position, Eccentricity, and Angular Momentum
Go
5 More Elliptical Orbits Calculators
Go
Geostationary Earth Satellite
(7)
Created
Absolute Angular Velocity Given Geo Radius of Earth and Geo Speed
Go
Created
Absolute Angular Velocity of Earth Given Geo Radius
Go
Created
Geo Radius Given Absolute Angular Velocity of Earth
Go
Created
Geo Radius Given Absolute Angular Velocity of Earth and Geo Speed
Go
Created
Geo Radius Given Speed of Satellite in its Circular Geo Orbit
Go
Created
Geo Speed along its Circular Path Given Absolute Angular Velocity of Earth
Go
Created
Speed of Satellite in its Circular GEO of Radius
Go
Hyperbolic Orbits
(6)
Created
Aiming Radius in Hyperbolic Orbit given Semi-Major Axis and Eccentricity
Go
Created
Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity
Go
Created
Radial Position in Hyperbolic Orbit given Angular Momentum, True Anomaly, and Eccentricity
Go
Created
Semi-Major Axis of Hyperbolic Orbit given Angular Momentum and Eccentricity
Go
Created
True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity
Go
Created
Turn Angle given Eccentricity
Go
Orbital Position as Function of Time
(6)
Created
Eccentric Anomaly in Elliptic Orbit given True Anomaly and Eccentricity
Go
Created
Mean Anomaly in Elliptic Orbit given Eccentric Anomaly and Eccentricity
Go
Created
Mean Anomaly in Elliptic Orbit given Time since Periapsis
Go
Created
Time since Periapsis in Elliptic Orbit given Eccentric Anomaly and Time Period
Go
Created
Time since Periapsis in Elliptic Orbit given Mean Anomaly
Go
Created
True Anomaly in Elliptic Orbit given Eccentric Anomaly and Eccentricity
Go
Orbital Position as Function of Time
(4)
Created
Mean Anomaly in Parabolic Orbit given Time since Periapsis
Go
Created
Mean Anomaly in Parabolic Orbit given True Anomaly
Go
Created
Time since Periapsis in Parabolic Orbit given Mean Anomaly
Go
Created
True Anomaly in Parabolic Orbit given Mean Anomaly
Go
Orbital Position as Function of Time
(5)
Created
Hyperbolic Eccentric Anomaly given Eccentricity and True Anomaly
Go
Created
Mean Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly
Go
Created
Time since Periapsis in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly
Go
Created
Time since Periapsis in Hyperbolic Orbit given Mean Anomaly
Go
Created
True Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly and Eccentricity
Go
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