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Table 4 Properties of the Swarm panel model used for aerodynamic and radiation pressure modeling

From: Swarm accelerometer data processing from raw accelerations to thermospheric neutral densities

Panel Area X Y Z
Nadir 1 1.540 0.0 0.0 1.0
Nadir 2 1.400 −0.19766 0.0 0.98027
Nadir 3 1.600 −0.13808 0.0 0.99042
Solar array +Y 3.450 0.0 0.58779 −0.80902
Solar array −Y 3.450 0.0 −0.58779 −0.80902
Zenith 0.500 0.0 0.0 −1.0
Front 0.560 1.0 0.0 0.0
Side wall +Y 0.753 0.0 1.0 0.0
Side wall −Y 0.753 0.0 −1.0 0.0
Shear panel nadir front 0.800 1.0 0.0 0.0
Shear panel nadir back 0.800 −1.0 0.0 0.0
Boom +Y 0.600 0.0 1.0 0.0
Boom −Y 0.600 0.0 −1.0 0.0
Boom zenith 0.600 −0.23924 0.0 −0.97096
Boom nadir 0.600 0.22765 0.0 0.97374