| column 1: SHOT_TIME | The UTC time of the laser transmission. |
| column 2: RANGE | The distance between spacecraft and asteroid surface calculated from the counter values of laser emission and reception. The accuracy is 0.5 m for AOCSM and 1.0 m for HK. The internal delay time in the LIDAR is taken into account. Unit is in m. |
| column 3: TOPO_LONGITUDE | The longitude of a laser footprint center position in the asteroid-fixed coordinates, converted from the inertial coordinates by using asteroid ephemeris, and axis and phase of the asteroid rotation. Unit is in degree. |
| column 4: TOPO_LATITUDE | The latitude of a laser footprint center position in the asteroid-fixed coordinates, converted from the inertial coordinates by using asteroid ephemeris, and axis and phase of the asteroid rotation. Unit is in degree. |
| column 5: TOPO_HEIGHT | The height of a laser footprint center position with respect to the center of the asteroid in the asteroid-fixed coordinates, converted from the inertial coordinates by using asteroid ephemeris, and axis and phase of the asteroid rotation. Unit is in meter. |
| column 6: TOPO_X | The X component of a laser footprint center position in the asteroid-fixed coordinates, converted from the inertial coordinates by using asteroid ephemeris, and axis and phase of the asteroid rotation. Unit is in meter. |
| column 7: TOPO_Y | The Y component of a laser footprint center position in the asteroid-fixed coordinates, converted from the inertial coordinates by using asteroid ephemeris, and axis and phase of the asteroid rotation. Unit is in meter. |
| column 8: TOPO_Z | The Z component of a laser footprint center position in the asteroid-fixed coordinates, converted from the inertial coordinates by using asteroid ephemeris, and axis and phase of the asteroid rotation. Unit is in meter. |
| column 9: SC_POS_X | The X component of the spacecraft position in the asteroid-fixed coordinates, converted from the inertial coordinates by using asteroid ephemeris, and axis and phase of the asteroid rotation. Unit is in meter. |
| column 10: SC_POS_Y | The Y component of the spacecraft position in the asteroid-fixed coordinates, converted from the inertial coordinates by using asteroid ephemeris, and axis and phase of the asteroid rotation. Unit is in meter. |
| column 11: SC_POS_Z | The Z component of the spacecraft position in the asteroid-fixed coordinates, converted from the inertial coordinates by using asteroid ephemeris, and axis and phase of the asteroid rotation. Unit is in meter. |