All,

     The spacecraft was nominal. The inertial maneuver was successful.  Orbit 640 ATS was uplinked.

Tasks accomplished:

CAR #1186 Orbit#540 ATS uplink

   IBEX_2021_248_o0540a_v001 93cmds

Results from the Inertial maneuver:

Q1 -0.05612130 ActNor.EstInrToBdy[0]

Q2 -0.64456200 ActNor.EstInrToBdy[1]

Q3 -0.22859100 ActNor.EstInrToBdy[2]

Q4 0.72741800 ActNor.EstInrToBdy[3]

GPS sec 1314500505 ActNor.EstTime

UTC time 09/01/2021 03:01:31 output

MPS Diff 0.601 deg

MPS Cmd Vector X -0.913727000

MPS Cmd Vector Y 0.376667000

MPS Cmd Vector Z 0.152399000

CSS Angle TLM 0.521

CSS Sun-Pointing Angle 1.042

  27 Aug 21 @ 16:00:00

CSS Angle TLM 1.74125

CSS Sun-Pointing Angle 3.4825

  01 Sept 21 @ 03:00:00

Pre-Burn

Thruster 1 7264 27 Aug 21 @ 16:00:00

Thruster 2 7104

Thruster 3 8080

Thruster 4 8240

Post-Burn

Thruster 1 7536 01 Sept 21 @ 03:00:00

Thruster 2 7376

Thruster 3 8384

Thruster 4 8544

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 304

Thruster 4 304

Thruster Pairs  

Thruster 1 & 2 544

Thruster 3 & 4 608

Timothy E.Perry

CRS IBEX OCO-2

Mission Operations

timothy.perry@ngc.com

Office (703) 406-5976

Cell (301) 606-1430