Styles by Object | Missile Report Styles | Missile Graph Styles

Report Style: Ephemeris-IFT

The position and velocity of the object with respect to Earth, as observed from its AlignmentAtEpoch coordinate system, expressed in Cartesian components as a function of time. The AlignmentAtEpoch system is the non-rotating coordinate system (i.e., a constant offset from ICRF) coincident with the Fixed system evaluated at the object's coordinate reference epoch (usually, the initial orbit epoch). Only available for objects whose central body is Earth.

Data Providers:Cartesian Position , Cartesian Velocity

Group: AlignmentAtEpoch

Availability: Reports | Dynamic Displays

Column Listing

Column	Column Name	Data Prv	Element	Type	Dimension	Description
1	Time	Cartesian Position	Time	Real Number or Text	Date	Time.
2	x	Cartesian Position	x	Real Number	Distance	The X component of the position vector.
3	y	Cartesian Position	y	Real Number	Distance	The Y component of the position vector.
4	z	Cartesian Position	z	Real Number	Distance	The Z component of the position vector.
5	vx	Cartesian Velocity	x	Real Number	Rate	The X component of the velocity vector.
6	vy	Cartesian Velocity	y	Real Number	Rate	The Y component of the velocity vector.
7	vz	Cartesian Velocity	z	Real Number	Rate	The Z component of the velocity vector.