All,

   The perigee contacts were nominal for CMD and TLM. The inertial maneuver was successful. 

The following was accomplished:

CAR #1085 ATS Upload IBEX_2020_060_o0479a_v001 88 cmds

SSR Dump -> Dump New

Reset Master Timer

Reset FDC Totals

Set Spacecraft Clock

Q1 0.74619100 ActNor.EstInrToBdy[0]

Q2 -0.19510700 ActNor.EstInrToBdy[1]

Q3 0.62388700 ActNor.EstInrToBdy[2]

Q4 0.12608700 ActNor.EstInrToBdy[3]

GPS sec 1266190307 ActNor.EstTime

UTC time 02/19/2020 23:31:33 output

MPS Diff 0.445 deg

MPS Cmd Vector X 0.881653000

MPS Cmd Vector Y -0.428831000

MPS Cmd Vector Z -0.196956000

CSS Angle TLM 1.137

CSS Sun-Pointing Angle 2.274

  16 Feb 20 @ 17:00

CSS Angle TLM 0.589171

CSS Sun-Pointing Angle 1.178342

  19 Feb 20 @ 23:30

Pre-Burn

Thruster 1 4272 16 Feb 20 @ 17:00

Thruster 2 4128

Thruster 3 5744

Thruster 4 5888

Post-Burn

Thruster 1 4528 19 Feb 20 @ 23:30

Thruster 2 4384

Thruster 3 6096

Thruster 4 6240

Number of Pulses

Thruster 1 256

Thruster 2 256

Thruster 3 352

Thruster 4 352

Thruster Pairs 

Thruster 1 & 2 512

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