The table shows the maneuvers contained in the NAIF's data files (PTO1 is a 2-step maneuver).
The calculations are based on NAIF's data files updated with tracking data through 05-APR-2021 20:35:36.
Select a sub-phase:
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Here's the spacecraft trajectory in the Bennu-centric mean ecliptic and equinox of J2000 reference frame.
The popup label shows the date, the radius vector (km), the altitude above Bennu (km), the spacecraft inertial speed (Vi, mm/s) and the speed relative to the surface of Bennu (Vs, mm/s).
Here's the same graph as above, but in the Bennu-centric Sun-North reference frame.
Instead of the inertial speed, the popup label shows the spacecraft speed in the Bennu-fixed rotating frame (Vbfr, mm/s).
The following graph shows the s/c radius vector, altitude, inertial speed and the speed relative to the surface of Bennu (click a graph legend to hide/show the related plot).