#	Burn time	DV	Dt	a
R1P1	2020-01-14 17:00:00.000	3.7	67.738	0.05
R1D	2020-01-21 20:31:56.608	128.3	16.378	7.83
R1R	2020-01-22 06:12:13.585	132.5	16.924	7.83
R2P1	2020-02-04 17:00:00.000	2.6	47.367	0.05
R2D	2020-02-11 17:17:03.007	102.8	13.222	7.77
R2R	2020-02-12 04:14:22.138	110.6	14.243	7.76

The table shows the spacecraft maneuvers performed during the Reconnaissance B phase (the calculations are based on NAIF's data file updated with tracking data through 02-MAR-2020 16:34:21).

Here's the spacecraft trajectory from January 10 to February 29 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).