#	Burn time	DV	Dt	a
R4P1	2020-05-19 17:00:00.000	1.5	29.301	0.05
R4P2	2020-05-23 17:00:00.000	3.5	69.407	0.05
R4D	2020-05-26 20:33:09.745	136.1	17.344	7.85
R4R	2020-05-27 01:39:30.415	100.8	12.943	7.79

The table shows the spacecraft maneuvers performed during this phase. The calculations and the graphs are based on NAIF's data files updated with tracking data through 08-JUN-2020 17:34:22.

Here's the spacecraft trajectory from May 15 to June 2 in the Bennu-centric mean ecliptic and equinox of J2000 reference frame.

The popup label shows the date, the radius vector (m), the altitude above Bennu (m), 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).