#	Burn time	DV	Dt	a
R3P1	2020-02-25 17:00:00.000	1.0	18.698	0.05
R3D	2020-03-03 19:00:02.272	150.9	19.235	7.84
R3R	2020-03-04 00:04:45.393	72.8	9.495	7.66
TR1T1	2020-03-10 17:00:00.000	14.2	236.429	0.06
TR1T2	2020-03-12 23:07:19.786	13.0	1.890	6.88

The table shows the spacecraft maneuvers performed during the Reconnaissance C phase (the calculations and the graphs are based on NAIF's data files updated with tracking data through 06-APR-2020 17:31:03).

Here's the spacecraft trajectory from February 24 to April 6 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).