All,

    The apogee contacts was nominal for CMD and TLM. The inertial maneuver was successful. the contact was taken on string 1.

Results from the Inertial maneuver:

Q1 -0.18837900 ActNor.EstInrToBdy[0]

Q2 0.63514400 ActNor.EstInrToBdy[1]

Q3 -0.00190548 ActNor.EstInrToBdy[2]

Q4 0.74908700 ActNor.EstInrToBdy[3]

GPS sec 1270472518 ActNor.EstTime

MPS Diff 0.629 deg

MPS Cmd Vector X 0.952508000

MPS Cmd Vector Y 0.283249000

MPS Cmd Vector Z 0.111798000

CSS Angle TLM 0.260196

CSS Sun-Pointing Angle 0.520392

  5 Apr 20 @ 4:30

CSS Angle TLM 0.0625

CSS Sun-Pointing Angle 0.125

  9 Apr 20 @ 13:00

Pre-Burn

Thruster 1 6848 5 Apr 20 @ 4:30

Thruster 2 6656

Thruster 3 9056

Thruster 4 9248

Post-Burn

Thruster 1 7120 9 Apr 20 @ 13:00

Thruster 2 6928

Thruster 3 9376

Thruster 4 9568

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 320

Thruster 4 320

Thruster Pairs 

Thruster 1 & 2 544

Thruster 3 & 4 640

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430