public interface SBASOrbitalElements extends TimeStamped
SBASPropagator
.Modifier and Type | Field and Description |
---|---|
static double |
SBAS_MU
WGS 84 value of the Earth's universal gravitational parameter for SBAS user in m³/s².
|
Modifier and Type | Method and Description |
---|---|
default double |
getAGf0()
Gets the Zeroth Order Clock Correction.
|
default double |
getAGf1()
Gets the First Order Clock Correction.
|
default int |
getIODN()
Gets the Issue Of Data Navigation (IODN).
|
int |
getPRN()
Gets the PRN number of the SBAS satellite.
|
double |
getTime()
Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
|
default double |
getToc()
Gets the clock correction reference time toc.
|
int |
getWeek()
Gets the Reference Week of the SBAS orbit.
|
double |
getX()
Get the ECEF-X component of satellite coordinates.
|
double |
getXDot()
Get the ECEF-X component of satellite velocity vector.
|
double |
getXDotDot()
Get the ECEF-X component of satellite acceleration vector.
|
double |
getY()
Get the ECEF-Y component of satellite coordinates.
|
double |
getYDot()
Get the ECEF-Y component of satellite velocity vector.
|
double |
getYDotDot()
Get the ECEF-Y component of satellite acceleration vector.
|
double |
getZ()
Get the ECEF-Z component of satellite coordinates.
|
double |
getZDot()
Get the ECEF-Z component of satellite velocity vector.
|
double |
getZDotDot()
Get the ECEF-Z component of satellite acceleration vector.
|
getDate
static final double SBAS_MU
int getPRN()
int getWeek()
double getTime()
double getX()
double getXDot()
double getXDotDot()
double getY()
double getYDot()
double getYDotDot()
double getZ()
double getZDot()
double getZDotDot()
default int getIODN()
default double getAGf0()
default double getAGf1()
default double getToc()
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