| Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |

Variables

# OrbitExtraChoiceEnum

Extra choice modes for getExtraData. More...

## Variables
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_NO_RESULTS = 0
| To calculate no extra results.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION = 1
| To calculate the geolocation data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_D = 2
| To calculate the geolocation rate data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_2D = 4
| To calculate the geolocation rate rate data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_EXTRA = 8
| To calculate the geolocation extra data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_EARTH_FIXED_D = 16
| To calculate the earth-fixed velocity data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_EARTH_FIXED_2D = 32
| To calculate the earth-fixed acceleration data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_SUN = 64
| To calculate the sun data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_MOON = 128
| To calculate the moon data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_OSCULATING_KEPLER = 256
| To calculate the osculating Kepler data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_INERTIAL_AUX = 512
| To calculate the inertial auxiliary data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_ANX_TIMING = 1024
| To calculate ANX timing data set.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPLER = 2048
| To calculate the mean keplerian elements.
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_ALL_RESULTS = 4095
| To calculate all extra results.

## Detailed Description

Extra choice modes for getExtraData.

## Variable Documentation

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_ALL_RESULTS = 4095`[static, inherited]`

To calculate all extra results.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_ANX_TIMING = 1024`[static, inherited]`

To calculate ANX timing data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPLER = 2048`[static, inherited]`

To calculate the mean keplerian elements.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_EARTH_FIXED_2D = 32`[static, inherited]`

To calculate the earth-fixed acceleration data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_EARTH_FIXED_D = 16`[static, inherited]`

To calculate the earth-fixed velocity data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION = 1`[static, inherited]`

To calculate the geolocation data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_2D = 4`[static, inherited]`

To calculate the geolocation rate rate data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_D = 2`[static, inherited]`

To calculate the geolocation rate data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_EXTRA = 8`[static, inherited]`

To calculate the geolocation extra data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_INERTIAL_AUX = 512`[static, inherited]`

To calculate the inertial auxiliary data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_MOON = 128`[static, inherited]`

To calculate the moon data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_NO_RESULTS = 0`[static, inherited]`

To calculate no extra results.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSCULATING_KEPLER = 256`[static, inherited]`

To calculate the osculating Kepler data set.

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_SUN = 64`[static, inherited]`

To calculate the sun data set.