All,

    The Perigee passes were nominal for CMD and TLM. The Sun maneuver was successful.

The following was accomplished:

Reset Master Timer

Set Static Z rate from 4.182 -> 4.170

Reset FDC Totals

SSR Dump -> Dump New

Set Spacecraft Clock

CAR #1067 ATS upload – IBEX_2019_296_o0465a_v001 93 cmds

CAR #1069 ATS upload – IBEX_2019_305_o0466a_v001 88 cmds

Results from the Sun Maneuver:

CSS Angle TLM 0.829215

CSS Sun-Pointing Angle 1.65843

  19 Oct 19 @ 23:30

CSS Angle TLM 0.863208

CSS Sun-Pointing Angle 1.726416

  22 Oct 19 @ 23:05

Pre-Burn

Thruster 1 19392 19 Oct 19 @ 23:30

Thruster 2 18800

Thruster 3 24784

Thruster 4 25376

Post-Burn

Thruster 1 19520 22 Oct 19 @ 23:05

Thruster 2 18928

Thruster 3 25136

Thruster 4 25728

Number of Pulses

Thruster 1 128

Thruster 2 128

Thruster 3 352

Thruster 4 352

Thruster Pairs 

Thruster 1 & 2 256

Thruster 3 & 4 704

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430