All,

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

The following was completed:

CAR #1009 ISN Season and HI Background test sweep table uploads

Reset the Master timer

Cleared FDC Totals

CAR # 1036 Orbit #447 ATS uplinked 93 cmds

Dumped the SSR and set the pointers to 70000

 

 

Q1 -0.54777700 ActNor.EstInrToBdy[0]

Q2 -0.26260800 ActNor.EstInrToBdy[1]

Q3 -0.77388800 ActNor.EstInrToBdy[2]

Q4 0.17909500 ActNor.EstInrToBdy[3]

GPS sec 1241042468.000 ActNor.EstTime

MPS Diff 0.651 deg

MPS Cmd Vector X 0.749898000

MPS Cmd Vector Y 0.610535000

MPS Cmd Vector Z 0.254754000

CSS Angle TLM 0.355533

CSS Sun-Pointing Angle 0.711066

  29 Apr 19 @ 18:00

CSS Angle TLM 0.739134

CSS Sun-Pointing Angle 1.478268

  04 May 19 @ 22:00

Pre-Burn   

Thruster 1 10192 29 Apr 19 @ 18:00

Thruster 2 9936

Thruster 3 12384

Thruster 4 12640

Post-Burn  

Thruster 1 10464 04 May 19 @ 22:00

Thruster 2 10205

Thruster 3 12688

Thruster 4 12944

Number of Pulses  

Thruster 1 272

Thruster 2 269

Thruster 3 304

Thruster 4 304

Thruster Pairs 

Thruster 1 & 2 541

Thruster 3 & 4 608

 

 

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

tim.perry@orbitalatk.com

Office (703) 406-5976

Cell (301) 606-1430

cid:image001.jpg@01D04F4E.6B1BECE0

 

 
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