All,

   The perigee contacts were nominal. We took the first contact on maestro03. During the contact we were able to uplink both ATS’s for orbits 664 & 665. The SSR was dumped during that contact also.

 

Tasks Accomplished:

SSR Dump -> Dump New

Reset FDC totals

Reset Master Timer

CAR #1415 Orbit 664 ATS upload

   IBEX_2024_280_o0664a_v001 91 commands

CAR #1417Orbit #665 ATS upload

   IBEX_2024_290_o0665a_v001 103 Commands

CAR #1428 Redump Missing Blocks from Orbit 663

 

Results from the Inertial Maneuver:

Q1 -0.23879100 ActNor.EstInrToBdy[0]

Q2 -0.69484500 ActNor.EstInrToBdy[1]

Q3 0.33408700 ActNor.EstInrToBdy[2]

Q4 0.59038600 ActNor.EstInrToBdy[3]

     

GPS sec 1412274864 ActNor.EstTime

UTC time 10/06/2024 18:34:10 output

 

MPS Diff 0.486 deg

 

MPS Cmd Vector X -0.98027200

MPS Cmd Vector Y -0.17759800

MPS Cmd Vector Z -0.08675600

 

CSS Angle TLM 1.32663

CSS Sun-Pointing Angle 2.65326

  05 Oct 24 @14:00:00

 

CSS Angle TLM 0.819961

CSS Sun-Pointing Angle 1.639922

  06 Oct 24 @18:30:00

 

Pre-Burn   

Thruster 1 6768 05 Oct 24 @14:00:00

Thruster 2 6608

Thruster 3 7792

Thruster 4 7952

Post-Burn  

Thruster 1 6912 06 Oct 24 @18:30:00

Thruster 2 6752

Thruster 3 7968

Thruster 4 8128

Number of Pulses  

Thruster 1 144

Thruster 2 144

Thruster 3 176

Thruster 4 176

Thruster Pairs 

Thruster 1 & 2 288

Thruster 3 & 4 352

 

 

 

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

IBEX MOC (703)404-7470

Cell (301) 606-1430