All,

    The contact was nominal for CMD and TLM. The Inertial maneuver was successful.

Results from the inertial maneuver:

Q1 0.12159300 ActNor.EstInrToBdy[0]

Q2 0.69543800 ActNor.EstInrToBdy[1]

Q3 0.11989200 ActNor.EstInrToBdy[2]

Q4 0.69800200 ActNor.EstInrToBdy[3]

GPS sec 1268920910 ActNor.EstTime

UTC time 03/22/2020 14:01:36 output

MPS Diff 0.820 deg

MPS Cmd Vector X 0.999949000

MPS Cmd Vector Y 0.004433000

MPS Cmd Vector Z -0.009076000

CSS Angle TLM 0.767958

CSS Sun-Pointing Angle 1.535916

  16 Mar 20 @ 19:00

CSS Angle TLM 0.148033

CSS Sun-Pointing Angle 0.296066

  22 Mar 20 @ 14:00

Pre-Burn

Thruster 1 5808 16 Mar 20 @ 19:00

Thruster 2 5816

Thruster 3 7872

Thruster 4 8064

Post-Burn

Thruster 1 6064 22 Mar 20 @ 14:00

Thruster 2 5872

Thruster 3 8160

Thruster 4 8352

Number of Pulses

Thruster 1 256

Thruster 2 56

Thruster 3 288

Thruster 4 288

Thruster Pairs 

Thruster 1 & 2 312

Thruster 3 & 4 576

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430