RinexNavigationEphemeris Properties |
The RinexNavigationEphemeris type exposes the following members.
Properties| Name | Description | |
|---|---|---|
 | Accuracy |
Gets the Sv accuracy.
|
| ArgumentOfPerigee |
Gets the argument of perigee.
|
| AvailabilityIntervals |
Gets a TimeIntervalCollection over which data is available.
If the availability interval is infinite, this returns
Infinite.
|
| ClockBias |
Gets the clock bias.
|
| ClockDrift |
Gets the clock drift.
|
| ClockDriftRate |
Gets the clock drift rate.
|
| CosineCorrectionToArgumentOfLatitude |
Gets the amplitude of the cosine harmonic correction term to the Argument of Latitude.
|
| CosineCorrectionToInclination |
Gets the amplitude of the cosine harmonic correction term to the angle of inclination.
|
| CosineCorrectionToOrbitRadius |
Gets the amplitude of the sine harmonic correction term to the orbit radius.
|
| DefaultValuesUsed |
Gets a value indicating whether or not the default value is used for any parameter. This may result because of a parse failure for a particular item.
|
| Eccentricity |
Gets eccentricity.
|
| Epoch |
Gets the epoch at which these elements are specified.
|
| FitInterval |
Gets the fit interval representing the duration in hours for which this ephemeris is valid.
Note that, according to ICD-GPS-200D, if the fit interval in the RINEX file is zero (or absent) the default fit interval is set to 4 hours.
|
| GpsWeek |
Gets the GPS Week # (to go with TimeOfEphemeris).
|
| GroupDelayDifferential |
Gets the group delay differential (tgd) in seconds.
|
| Health |
Gets the Sv health (bits 17-22 w 3 sf 1).
|
| InclinationAngle |
Gets the inclination angle.
|
| IssueOfData |
Gets the issue of data ephemeris (IODE).
|
| IssueOfDataClock |
Gets the issue of data clock (IODC).
|
| L2Channel |
Gets the codes on L2 channel.
|
| L2PDataFlag |
Gets the L2 P data flag.
|
| LongitudeOfAscendingNode |
Gets the longitude of ascending node of orbit plane at weekly epoch.
|
| MeanAnomaly |
Gets the mean anomaly.
|
| MeanMotionDifference |
Gets the mean motion difference from computed value.
|
| PseudoRandomNumber |
Gets the Pseudo Random Number (PRN).
|
| RateOfInclinationAngle |
Gets the rate of inclination angle (IDOT).
|
| RateOfRightAscension |
Gets the rate of right ascension.
|
| SineCorrectionToArgumentOfLatitude |
Gets the amplitude of the sine harmonic correction term to the Argument of Latitude.
|
| SineCorrectionToInclination |
Gets the amplitude of the sine harmonic correction term to the angle of inclination.
|
| SineCorrectionToOrbitRadius |
Gets the amplitude of the sine harmonic correction term to the orbit radius.
|
| SquareRootOfSemimajorAxis |
Gets the square root of the semi-major axis (sqrt(meters)).
|
| TimeOfClock |
Gets GPS date of the time of clock of the message.
|
| TimeOfEphemeris |
Gets the time of ephemeris (TOE).
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| TimeOfEphemerisGpsDate |
Gets the GPS date of the time of ephemeris of the message.
|
| TransmissionTime |
Gets the transmission time of the message in seconds of the GpsWeek.
|
| TransmissionTimeGpsDate |
Gets the GPS date of the transmission time of the message.
|
See Also