Data Providers: Satellite: Astrogator Maneuver Ephemeris Block Initial: Other Orbit

Satellite: Astrogator Maneuver Ephemeris Block Initial: Other Orbit

Miscellaneous Calc Objects.

Name	Dimension	Type	Description
Time	DateFormat	Real Number	Time.
Apparent_Solar_Time	AngleUnit	Real Number	Apparent solar time expressed as an angle. The Calc Object allows a choice of a central body. The default is Earth.
Beta_Angle	AngleUnit	Real Number	Not defined for this class of object.
Earth_Mean_Solar_Time	AngleUnit	Real Number	Apparent solar time modified for earth's equation of time, expressed as an angle. The Calc Object allows a choice of a central body. The default is Earth.
Local_Apparent_Solar_Longitude	AngleUnit	Real Number	Apparent solar longitude minus vehicle longitude. The Calc Object allows a choice of a central body. The default is Earth.
Longitude_of_Periapsis	AngleUnit	Real Number	The sum of the right ascension of the ascending node and the argument of periapsis. The Calc Object allows a choice of element type (Osculating elements, Kozai-Izsak Mean elements, Brouwer-Lyddane Mean elements using only short period terms, and Brouwer-Lyddane Mean elements using both short and long period terms). The default is osculating. The Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
Orbit_State_Value	DateFormat	Real Number	Computes the value of the specified Calc Object given the specified input values of position and velocity
SignedEccentricity	Unitless	Real Number	The eccentricity multiplied by either 1.0 or -1.0. The value is positive if the mean anomaly is within pi/2 radians of the periapsis, else it is negative. The Calc Object allows a choice of element type (Osculating elements, Kozai-Izsak Mean elements, Brouwer-Lyddane Mean elements using only short period terms, and Brouwer-Lyddane Mean elements using both short and long period terms). The default is osculating.
SignedInclination	AngleUnit	Real Number	The inclination multiplied by either 1.0 or -1.0. The value is positive if the argument of latitude is within pi/2 radians of the ascending node, else it is negative. The Calc Object allows a choice of element type (Osculating elements, Kozai-Izsak Mean elements, Brouwer-Lyddane Mean elements using only short period terms, and Brouwer-Lyddane Mean elements using both short and long period terms). The default is osculating.
True_Longitude	AngleUnit	Real Number	The sum of the right ascension of the ascending node, the argument of periapsis, and the true anomaly. The Calc Object allows a choice of element type (Osculating elements, Kozai-Izsak Mean elements, Brouwer-Lyddane Mean elements using only short period terms, and Brouwer-Lyddane Mean elements using both short and long period terms). The default is osculating. The Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.