Re: [Orekit Users] Time of propagation DSSTPropagator

["Elisabet" <elisabet.cid-borobia@thalesaleniaspace.com>]

Paul,

The orbit tested has the following parameters:
sma=7040.956 km
e=0.00119932
w=90.0754744 deg
i=98.1256422 deg
raan=136.712926 deg
mean anomaly=-90 deg

As for the Earth’s perturbation I used  a degree of 15 and an order of 0:
FactoryManagedFrame GTOD =
FramesFactory.getGTOD(IERSConventions.IERS_2010,false);
UnnormalizedSphericalHarmonicsProvider provider =
GravityFieldFactory.getUnnormalizedProvider(degree, order);
dsst.addForceModel(new DSSTCentralBody(GTOD, wearth, provider, degree, degree,
order, degree, order));

Regards,

Elisabet