All,

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

The following was accomplished:

SSR Dump -> Dump new & reset pointers

Reset Master Timer

Set Spacecraft Clock

CAR #1086 ATS upload -> IBEX_2020_069_o0480a_V001 93 Cmds

Reset FDC Totals

Results from the Inertial Maneuver:

Q1 0.32760500 ActNor.EstInrToBdy[0]

Q2 0.67537000 ActNor.EstInrToBdy[1]

Q3 0.09292420 ActNor.EstInrToBdy[2]

Q4 0.65415200 ActNor.EstInrToBdy[3]

MPS Cmd Vector X 0.945157000

MPS Cmd Vector Y -0.295488000

MPS Cmd Vector Z -0.139156000

GPS sec 1266970192 ActNor.EstTime

UTC time 02/29/2020 00:09:38 output

MPS Diff 0.829 deg

CSS Angle TLM 0.625263

CSS Sun-Pointing Angle 1.250526

  26 Feb 20 @ 18:00

CSS Angle TLM 0.696893

CSS Sun-Pointing Angle 1.393786

  29 Feb 20 @ 00:05

Pre-Burn  

Thruster 1 4768 26 Feb 20 @ 18:00

Thruster 2 4624

Thruster 3 6384

Thruster 4 6528

Post-Burn  

Thruster 1 5040 29 Feb 20 @ 00:05

Thruster 2 4896

Thruster 3 6704

Thruster 4 6848

Number of Pulses  

Thruster 1 272

Thruster 2 272

Thruster 3 320

Thruster 4 320

Thruster Pairs 

Thruster 1 & 2 544

Thruster 3 & 4 640

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430