Scenario: Vectors(J2000)

Used to report the selected vector and its derivative in J2000 axes. The vector must be defined in the Vector Geometry Tool.

Type: Time-varying data

Availability: Reports | Graphs | Dynamic Displays

Name Description
Earth Angular_Velocity Angular velocity vector of the body fixed axes with respect to the inertial axes.
Earth Cross_Product Default example of a cross product vector based on the Earth position vector with respect to the solar system barycenter and the north celestial pole vector.
Earth Earth(True) Vector that locates Earth center with respect to the object's center.
Earth EclipticNormal Unit vector normal to the Earth mean of J2000 epoch ecliptic plane or Z-axis of the Earth mean ecliptic of J2000 epoch axes.
Earth ICRF-X Unit vector along X-axis of the ICRF set of axes.
Earth ICRF-Z Unit vector along Z-axis of the ICRF set of axes.
Earth Moon Apparent position of the Moon center as seen from the object's center.
Earth Moon(True) True position of the Moon center as seen from the object's center.
Earth NorthPole Unit vector in the direction of the central body north pole which is Z-axis of the central body fixed axes.
Earth Orbit_AngMomentum Osculating orbit angular momentum which is a cross product of the instantaneous position and inertial velocity vectors
Earth Orbit_AngMomentum(Barycenter) Osculating orbit angular momentum with respect to the solar system barycenter which is a cross product of the instantaneous position and inertial velocity vectors with respect to the solar system barycenter.
Earth Orbit_Normal Unit vector in the direction of the osculating orbit angular momentum which is a cross product of the instantaneous position and inertial velocity vectors.
Earth Position True position of the object's center with respect to its central body center.
Earth Position(Barycenter) True position of the object's center with respect to the solar system barycenter.
Earth Sun Apparent position of the Sun center as seen from the object's center.
Earth Sun(True) True position of the Sun center as seen from the object's center.
Earth Velocity Inertial velocity of the object's center with respect to its central body center.
Earth Velocity(Barycenter) Inertial Velocity of the object's center with respect to the solar system barycenter.
Sun Angular_Velocity Angular velocity vector of the body fixed axes with respect to the inertial axes.
Sun Earth Apparent position of the Earth center as seen from the object's center.
Sun Earth(True) Vector that locates Earth center with respect to the object's center.
Sun EclipticNormal Unit vector normal to the Earth mean of J2000 epoch ecliptic plane or Z-axis of the Earth mean ecliptic of J2000 epoch axes.
Sun ICRF-X Unit vector along X-axis of the ICRF set of axes.
Sun ICRF-Z Unit vector along Z-axis of the ICRF set of axes.
Sun Moon Apparent position of the Moon center as seen from the object's center.
Sun Moon(True) True position of the Moon center as seen from the object's center.
Sun NorthPole Unit vector in the direction of the central body north pole which is Z-axis of the central body fixed axes.
Sun Position(Barycenter) True position of the object's center with respect to the solar system barycenter.
Sun Velocity(Barycenter) Inertial Velocity of the object's center with respect to the solar system barycenter.
Moon Angular_Velocity Angular velocity vector of the body fixed axes with respect to the inertial axes.
Moon Earth Apparent position of the Earth center as seen from the object's center.
Moon Earth(True) Vector that locates Earth center with respect to the object's center.
Moon EclipticNormal Unit vector normal to the Earth mean of J2000 epoch ecliptic plane or Z-axis of the Earth mean ecliptic of J2000 epoch axes.
Moon ICRF-X Unit vector along X-axis of the ICRF set of axes.
Moon ICRF-Z Unit vector along Z-axis of the ICRF set of axes.
Moon NorthPole Unit vector in the direction of the central body north pole which is Z-axis of the central body fixed axes.
Moon Orbit_AngMomentum Osculating orbit angular momentum which is a cross product of the instantaneous position and inertial velocity vectors
Moon Orbit_Normal Unit vector in the direction of the osculating orbit angular momentum which is a cross product of the instantaneous position and inertial velocity vectors.
Moon Position True position of the object's center with respect to its central body center.
Moon Position(Barycenter) True position of the object's center with respect to the solar system barycenter.
Moon Sun Apparent position of the Sun center as seen from the object's center.
Moon Sun(True) True position of the Sun center as seen from the object's center.
Moon Velocity Inertial velocity of the object's center with respect to its central body center.
Moon Velocity(Barycenter) Inertial Velocity of the object's center with respect to the solar system barycenter.

STK Programming Interface 11.0.1