CelestrakGeneralPerturbationElements Properties |
The CelestrakGeneralPerturbationElements type exposes the following members.
Name | Description | |
---|---|---|
ArgumentOfPerigee |
Gets or sets the argument of perigee, in degrees.
(Inherited from Sgp4Elements.) | |
BStar |
Gets or sets the BSTAR drag term, in units of 1 / EarthRadii.
This term represents a modification of the ballistic coefficient
(Coefficient of drag times area over mass). The value is modified
by one half atmospheric density and expressed in units of inverse
Earth radii. Source: https://celestrak.com/ (Inherited from Sgp4Elements.) | |
Classification |
Gets or sets the classification.
| |
Eccentricity |
Gets or sets the eccentricity
(Inherited from Sgp4Elements.) | |
ElementNumber |
Gets or sets the element number.
| |
EphemerisType |
Gets or sets the ephemeris type. Ephemeris Type 0 is the correct type for Sgp4Propagator.
Ephemeris type 4 is not supported by Sgp4Propagator, and it will throw an argument exception
if a CelestrakGeneralPerturbationElements has ephemeris type 4.
| |
Epoch |
Gets or sets the epoch at which these initial conditions are defined.
(Inherited from Sgp4Elements.) | |
Inclination |
Gets or sets the inclination, in degrees
(Inherited from Sgp4Elements.) | |
InternationalDesignator |
Gets or sets the international designator.
| |
MeanAnomaly |
Gets or sets the mean anomaly, in degrees.
(Inherited from Sgp4Elements.) | |
MeanMotion |
Gets or sets the mean motion, in revolutions per day.
(Inherited from Sgp4Elements.) | |
MeanMotionDot |
Gets or sets the first derivative of mean motion divided by two, in revolutions per day squared.
| |
MeanMotionDotDot |
Gets or sets the second derivative of mean motion divided by six, in revolutions per day cubed.
| |
Name |
Gets or sets the spacecraft name.
| |
RawEpoch |
Gets or sets the epoch at which these initial conditions are defined,
represented in the standard form: YYDDD.DDDD. Note: this will
be represented to as much precision as possible and will not reflect
the RawEpoch taken from a
TwoLineElementSet format. To represent the correct
precision for a TLE, use the TwoLineElementSet type instead.
(Inherited from Sgp4Elements.) | |
RevolutionNumber |
Gets or sets the revolution number at epoch.
| |
RightAscensionOfAscendingNode |
Gets or sets the right ascension of the ascending node, in degrees
(Inherited from Sgp4Elements.) | |
SatelliteNumber |
Gets or sets the satellite number.
| |
SwitchingMethod |
Gets or sets the method to use when switching between this element set and the following element set.
By default, this is Sgp4ElementsSwitchByEpoch.
(Inherited from Sgp4Elements.) |