#	Burn time	DV	Dt	a
IG11	2020-06-16 17:00:00.000	3.3	61.000	0.05
R2D2	2020-06-20 17:00:00.000	117.6	15.146	7.76
C3PO	2020-06-30 17:00:00.000	67.1	8.778	7.64
K2SO	2020-07-07 17:00:00.000	117.7	15.144	7.77
BB8	2020-07-09 22:27:25.099	64.6	8.496	7.60
TR2P1	2020-08-04 17:00:00.000	5.7	111.750	0.05

The table shows the maneuvers performed during this phase.
The calculations are based on NAIF's data files updated with tracking data through 07-AUG-2020 16:36:34.

Select a sub-phase: Parking orbit Departure Orbit re-insertion 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 (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).