All,

   The apogee contact was nominal for CMD and TLM. The sun maneuver  was successful. The static z rate was set from 4.1848 -> 4.1662.

Results from the sun maneuver:

CSS Angle TLM 1.69084

CSS Sun-Pointing Angle 3.38168

  17 Dec 19 @ 12:00

CSS Angle TLM 0.554966

CSS Sun-Pointing Angle 1.109932

  22 Dec 19 @ 20:00

Pre-Burn

Thruster 1 992 17 Dec 19 @ 12:00

Thruster 2 992

Thruster 3 1088

Thruster 4 1088

Post-Burn

Thruster 1 1136 22 Dec 19 @ 20:00

Thruster 2 1088

Thruster 3 1440

Thruster 4 1488

Number of Pulses

Thruster 1 144

Thruster 2 96

Thruster 3 352

Thruster 4 400

Thruster Pairs 

Thruster 1 & 2 240

Thruster 3 & 4 752

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430