shiftedBy(Orbit, double) |  | 100% |  | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, Frame, RealMatrix, OrbitType, PositionAngle) |  | 100% |  | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
changeFrameAndCreate(Orbit, AbsoluteDate, Frame, LOFType, RealMatrix, OrbitType, PositionAngle) |  | 100% |  | 100% | 0 | 2 | 0 | 14 | 0 | 1 |
changeTypeAndCreate(Orbit, AbsoluteDate, Frame, OrbitType, PositionAngle, OrbitType, PositionAngle, RealMatrix) |  | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
changeFrameAndCreate(Orbit, AbsoluteDate, LOFType, Frame, RealMatrix) |  | 100% |  | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
changeCovarianceType(Orbit, OrbitType, PositionAngle) |  | 100% |  | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
changeCovarianceFrame(Orbit, LOFType) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
changeCovarianceFrame(Orbit, Frame) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getStm(Orbit, double) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
checkInputConsistency(Frame, OrbitType) |  | 100% |  | 100% | 0 | 4 | 0 | 6 | 0 | 1 |
StateCovariance(RealMatrix, AbsoluteDate, Frame, LOFType, OrbitType, PositionAngle) |  | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
changeFrameAndCreate(Orbit, AbsoluteDate, LOFType, LOFType, RealMatrix) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
getJacobian(Transform) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
StateCovariance(RealMatrix, AbsoluteDate, LOFType) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
StateCovariance(RealMatrix, AbsoluteDate, Frame, OrbitType, PositionAngle) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDate() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMatrix() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOrbitType() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPositionAngle() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFrame() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLOFType() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
static {...} |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |