Styles by Object | SatelliteCollection Report Styles

Report Style: All Satellites Walker

A listing of automatically created Metadata for the satellites in the AllSatellites subset of a Satellite Collection of Walker type. When used with a different type of Satellite Collection, only the name, epoch, and ephemeris interval will be reported.

Data Provider:Subset Listing

Group:AllSatellites

Type: Fixed data.

Availability: Reports

Column Listing

Column	Column Name	Element	Type	Dimension	Description
1	RowNumber	RowNumber	Integer	Unitless	A counter indicating the row being reported.
2	Name	Name	Text	Unitless	The name of the satellite.
3	Epoch	Epoch	Real Number or Text	Date	The epoch associated with the satellite's ephemeris.
4	Ephemeris Start Time	Ephemeris Start Time	Real Number or Text	Date	The start time of the satellite's ephemeris.
5	Ephemeris Stop Time	Ephemeris Stop Time	Real Number or Text	Date	The stop time of the satellite's ephemeris.
6	ID	ID	Integer	Unitless	An integer identifier of the satellite.
7	Shell	Shell	Text	Unitless	The integer identifier of the orbital shell that the satellite entry lies within.
8	Plane	Plane	Text	Unitless	The integer identifier of the Walker constellation plane that the satellite entry lies in.
9	Slot	Slot	Text	Unitless	The integer identifier of the orbital slot that identifies the location of the satellite entry within the Walker constellation plane .
10	Altitude	Altitude	Real Number	Distance	The approximate altitude, computed from the satellite entry's initial orbit elements.
11	SemimajorAxis	SemimajorAxis	Real Number	Distance	The semimajor axis of the satellite entry's initial orbit elements.
12	Eccentricity	Eccentricity	Real Number	Unitless	The eccentricity of the satellite entry's initial orbit elements. For a Database type Satellite Collection, the eccentricity is obtained from the first element set if more than one exist.
13	Inclination	Inclination	Real Number or Text	Angle	The inclination of the satellite entry's initial orbit elements. For a Database type Satellite Collection, the inclination is obtained from the first element set if more than one exist.
14	ArgumentOfPerigee	ArgumentOfPerigee	Real Number or Text	Angle	The argument of perigee of the satellite entry's initial orbit elements.
15	RAAN	RAAN	Real Number or Text	Angle	The right ascension of the ascending node of the satellite entry's initial orbit elements.
16	TrueAnomaly	TrueAnomaly	Real Number or Text	Angle	The true anomaly of the satellite entry's initial orbit elements.