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TwoLineElementSet Constructor (Sgp4Elements, String, String, String, String, Double, Double, Int32, Int32)

Initializes a new Two Line Element Set (TLE) from a set of Sgp4Elements and additional meta-data contained in the TLE format.

Namespace:  AGI.Foundation.Propagators
Assembly:  AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.3.420.0 (24.3.420.0)
Syntax
public TwoLineElementSet(
	Sgp4Elements elements,
	string name,
	string satelliteNumber,
	string classification,
	string internationalDesignator,
	double meanMotionDot,
	double meanMotionDotDot,
	int elementNumber,
	int revolutions
)

Parameters

elements
Type: AGI.Foundation.PropagatorsSgp4Elements
The elements specifying the essential orbit ephemeris data.
name
Type: SystemString
The name of the satellite to appear on the line just prior to the TLE.
satelliteNumber
Type: SystemString
The NORAD satellite catalog number, as a string.
classification
Type: SystemString
The single character classification for the satellite. All civilian space objects are classified with 'U' for 'Unclassified'.
internationalDesignator
Type: SystemString
The international catalog number assigned by the World Data Center-A for Rockets and Satellites.
meanMotionDot
Type: SystemDouble
The first time derivative of the mean motion at epoch.
meanMotionDotDot
Type: SystemDouble
The second time derivative of the mean motion at epoch.
elementNumber
Type: SystemInt32
A number assigned to indicate the number of times this ephemeris has been regenerated.
revolutions
Type: SystemInt32
The number of times the spacecraft has passed through its ascending node (since launch).
Exceptions
ExceptionCondition
ArgumentNullException Thrown when elements is .
See Also