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

Variables

# OrbitExtraModelMKODependantEnum

Extra data model independent result vector. More...

## Variables
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_NODAL_PERIOD = 0
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_UTC_CURRENT_ANX = 1
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_ORBIT_NUMBER = 2
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_SEC_SINCE_ANX = 3
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_A = 4
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_E = 5
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_I = 6
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_RA = 7
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_W = 8
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_M = 9
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_NUM_DEP_ELEMENTS = 10

## Detailed Description

Extra data model independent result vector.

## Variable Documentation

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

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_E = 5`[static, inherited]`

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_I = 6`[static, inherited]`

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_M = 9`[static, inherited]`

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPL_RA = 7`[static, inherited]`

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

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

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

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_SEC_SINCE_ANX = 3`[static, inherited]`

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

long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_NUM_DEP_ELEMENTS = 10`[static, inherited]`