Acceleration along the body-fixed Y axis of the satellite. Input is unitless but is multiplied by 1.0e-12 m/s2 to yield an acceleration perpendicular to the sun-to-satellite line. Also known as K2, the nominally value is in the range of -1 < YBias < 1.
Read-write property
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Public Property YBias() As Double |
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public: __property double get_YBias(); |
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