All,

   The apogee contact was nominal. The inertial maneuver was successful. The FDC totals were reset during the contact.

Results from the Inertial Maneuver.

Q1 0.37421400 ActNor.EstInrToBdy[0]

Q2 0.67736800 ActNor.EstInrToBdy[1]

Q3 0.00813852 ActNor.EstInrToBdy[2]

Q4 0.63330100 ActNor.EstInrToBdy[3]

GPS sec 1392300213 ActNor.EstTime

UTC time 02/18/2024 14:03:19 output

MPS Diff 0.690 deg

MPS Cmd Vector X 0.86529600

MPS Cmd Vector Y -0.456219000

MPS Cmd Vector Z -0.207673000

CSS Angle TLM 0.977187

CSS Sun-Pointing Angle 1.954374

  13 Feb 24 @21:00:00

CSS Angle TLM 1.23035

CSS Sun-Pointing Angle 2.4607

  18 Feb 24 @14:00:00

Pre-Burn

Thruster 1 19568 13 Feb 24 @21:00:00

Thruster 2 18960

Thruster 3 26352

Thruster 4 26960

Post-Burn

Thruster 1 19856 18 Feb 24 @14:00:00

Thruster 2 19248

Thruster 3 26672

Thruster 4 27280

Number of Pulses

Thruster 1 288

Thruster 2 288

Thruster 3 320

Thruster 4 320

Thruster Pairs  

Thruster 1 & 2 576

Thruster 3 & 4 640

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