Name
|
Description
|
ArgumentOfPerigee
|
Argument of perigee
|
Bstar
|
B* term of the two-line-element
|
Classification
|
The classification of the element set
|
DeclaredName
|
The name of the object as declared.
|
DisplayName
|
The name displayed for this object in output windows such as views, plots, and reports.
|
Eccentricity
|
Eccentricity
|
ElementSetNumber
|
The element set number. Normally, this number is incremented each time a new element set is generated. However, recent practice has this number set to 999 at all times, to avoid confusion after rollovers.
|
EphemerisType
|
Ephemeris type (ie. orbital model) used to generate the data
|
Epoch
|
The day of year of the epoch of the element set include the fractional portion of the day.
|
Inclination
|
Orbit Inclination
|
InternationalDesignator
|
The year of the launch, the launch of that year, and the piece of that launch for each object
|
MeanAnomaly
|
Mean Anomaly
|
MeanMotion
|
Mean motion
|
MeanMotionDDot
|
The second derivative of the mean motion divided by six, in units of revolutions per day^3, decimal point assumed, as a string. Note, since this parameter is not used, it is read directly from the TLE, or output directly to it.
|
MeanMotionDot
|
The first derivative of the mean motion divided by two, in units of revolutions per day^2 as a string. Note, since this parameter is not used, it is read directly from the TLE, or output directly to it.
|
ObjectId
|
The unique identifier for the object.
|
ObjectType
|
The type of the object.
|
RAAN
|
Right ascension of the ascending node
|
RevolutionNumber
|
The revolution number at epoch
|
SatelliteNumber
|
The catalog number assigned to the object by the US Air Force
|
SpacecraftName
|
The name of spacecraft as read or written as the header line in a three-line-element.
|