Position

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	0 of 232	100%	0 of 0	n/a	0	8	0	17	0	8
static {...}		100%		n/a	0	1	0	1	0	1
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[])		100%		n/a	0	1	0	4	0	1
Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite)		100%		n/a	0	1	0	2	0	1
Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite)		100%		n/a	0	1	0	2	0	1
Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite)		100%		n/a	0	1	0	2	0	1
theoreticalEvaluation(int, int, SpacecraftState[])		100%		n/a	0	1	0	3	0	1
Position(AbsoluteDate, Vector3D, MeasurementQuality, ObservableSatellite)		100%		n/a	0	1	0	2	0	1
getPosition()		100%		n/a	0	1	0	1	0	1