#	UTC burn time	DV	Dt	a
PTO1	2021-01-14 19:44:21.000	743.8	10.760	69.12
PTO1	2021-01-14 20:14:57.000	732.5	10.763	68.06
PTO2	2021-03-06 20:00:00.000	342.1	43.020	7.95
PTO3	2021-03-20 20:00:00.000	391.7	49.201	7.96
PTO4	2021-03-27 20:00:00.000	257.8	32.522	7.93
PTO5	2021-04-04 20:00:00.000	105.3	13.523	7.79

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: PTO1 App + flyby Flyby Loading...

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).