All,

   The apogee contact was nominal for CMD & TLM. The sun maneuver was successful. The sta_percent_valid was at 1, so I was unable to set the static z rate.

Results from the Sun Maneuver:

CSS Angle TLM-1.39241-

CSS Sun-Pointing Angle-2.78482-

--25 Dec 20 @ 00:30:00

CSS Angle TLM-0.568551-

CSS Sun-Pointing Angle-1.137102-

--29 Dec 20 @ 19:30:00

Pre-Burn- -

Thruster 1-2448-25 Dec 20 @ 00:30:00

Thruster 2-2400-

Thruster 3-2736-

Thruster 4-2784-

Post-Burn- -`

Thruster 1-2592-29 Dec 20 @ 19:30:00

Thruster 2-2496-

Thruster 3-3040-

Thruster 4-3136-

Number of Pulses- -

Thruster 1-144-

Thruster 2-96-

Thruster 3-304-

Thruster 4-352-

Thruster Pairs--

Thruster 1 & 2-240-

Thruster 3 & 4-656-

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430