All,

   The Apogee pass was nominal for CMD and TLM.  The Inertial maneuver was successful.

The following tasks were accomplished:

CAR # 1063 “ISN Season and Hi Background Test sweep table uploads”  Pass # 6

Sweep Table “Table_Lo_11223678_ISN2” was uplinked

Reset FDC Totals

Results from the Inertial Maneuver:

Q1 0.74585600

Q2 -0.31525400

Q3 0.52527200

Q4 0.26154000

MPS Cmd Vector X 0.622298000

MPS Cmd Vector Y -0.714510000

MPS Cmd Vector Z -0.319720000

GPS sec 1264176012 ActNor.EstTime

UTC time 01/27/2020 15:59:58 output

MPS Diff 0.651 deg

CSS Angle TLM 0.716005

CSS Sun-Pointing Angle 1.43201

  23 Jan 20 @ 19:00

CSS Angle TLM 0.714637

CSS Sun-Pointing Angle 1.429274

  27 Jan 20 @ 16:00

Pre-Burn  

Thruster 1 2864 23 Jan 20 @ 19:00

Thruster 2 2768

Thruster 3 4128

Thruster 4 4224

Post-Burn  

Thruster 1 3136 27 Jan 20 @ 16:00

Thruster 2 3040

Thruster 3 4432

Thruster 4 4528

Number of Pulses  

Thruster 1 272

Thruster 2 272

Thruster 3 304

Thruster 4 304

Thruster Pairs 

Thruster 1 & 2 544

Thruster 3 & 4 608

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430