Hi,
Below is the code which I am using in order to create a satellite scenario. I have defined all the required parameters manually that are required to initialize a satellte, but I am not able to understand why are they getting changed after the satellite is initialized.
startTime = datetime(’27-Jun-2024 13:23:02′);
stopTime = startTime + seconds(60*100);
sampleTime = 10;
sc = satelliteScenario(startTime,stopTime,sampleTime);

mu = 3.986004418*1e14;
n = 15.06398680175205;

semiMajorAxis = nthroot(mu,3)/(((2*n*pi)/86400)^(2/3)) ;
trueAnomaly = 341.2089;
Eccentricity = 1.249e-04;
Inclination = 53.0534;
RightAscensionOfAscendingNode = 242.3386;
ArgumentOfPeriapsis = 94.5842;

sat = satellite(sc,semiMajorAxis,Eccentricity,Inclination,RightAscensionOfAscendingNode,ArgumentOfPeriapsis,trueAnomaly);
elements = orbitalElements(sat);

I would really appreciate if someone can help me figure out why are the values of RAAN and ArgumentOfPeriapsis getting changed after the satellite is initialized.
Thank youHi,
Below is the code which I am using in order to create a satellite scenario. I have defined all the required parameters manually that are required to initialize a satellte, but I am not able to understand why are they getting changed after the satellite is initialized.
startTime = datetime(’27-Jun-2024 13:23:02′);
stopTime = startTime + seconds(60*100);
sampleTime = 10;
sc = satelliteScenario(startTime,stopTime,sampleTime);

mu = 3.986004418*1e14;
n = 15.06398680175205;

semiMajorAxis = nthroot(mu,3)/(((2*n*pi)/86400)^(2/3)) ;
trueAnomaly = 341.2089;
Eccentricity = 1.249e-04;
Inclination = 53.0534;
RightAscensionOfAscendingNode = 242.3386;
ArgumentOfPeriapsis = 94.5842;

sat = satellite(sc,semiMajorAxis,Eccentricity,Inclination,RightAscensionOfAscendingNode,ArgumentOfPeriapsis,trueAnomaly);
elements = orbitalElements(sat);

I would really appreciate if someone can help me figure out why are the values of RAAN and ArgumentOfPeriapsis getting changed after the satellite is initialized.
Thank you Hi,
Below is the code which I am using in order to create a satellite scenario. I have defined all the required parameters manually that are required to initialize a satellte, but I am not able to understand why are they getting changed after the satellite is initialized.
startTime = datetime(’27-Jun-2024 13:23:02′);
stopTime = startTime + seconds(60*100);
sampleTime = 10;
sc = satelliteScenario(startTime,stopTime,sampleTime);

mu = 3.986004418*1e14;
n = 15.06398680175205;

semiMajorAxis = nthroot(mu,3)/(((2*n*pi)/86400)^(2/3)) ;
trueAnomaly = 341.2089;
Eccentricity = 1.249e-04;
Inclination = 53.0534;
RightAscensionOfAscendingNode = 242.3386;
ArgumentOfPeriapsis = 94.5842;

sat = satellite(sc,semiMajorAxis,Eccentricity,Inclination,RightAscensionOfAscendingNode,ArgumentOfPeriapsis,trueAnomaly);
elements = orbitalElements(sat);

I would really appreciate if someone can help me figure out why are the values of RAAN and ArgumentOfPeriapsis getting changed after the satellite is initialized.
Thank you communication, matlab MATLAB Answers — New Questions

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