Good morning team,

The perigee contacts were nominal, and the inertial maneuver was successful. We performed the following, dump SSR (VCid2) and reset master timer.

Tasks Accomplished:

Reset Master Timer

Reset FDC Totals

SSR Dump (VCid2)

CAR #1389 Orbit 648 ATS upload

IBEX_2024_136_o0648a_v001 - 103 commands

Results from the inertial maneuver:

Q1 -0.56964300

Q2 0.20075200

Q3 -0.39981200

Q4 0.68946100

GPS sec 1399011471

UTC time 05/06/2024 06:17:37

MPS Diff 0.588

MPS Cmd Vector X 0.72839500

MPS Cmd Vector Y 0.632159000

MPS Cmd Vector Z 0.264227000

CSS Angle TLM 0.137056

CSS Sun-Pointing Angle 0.274112

01 May 24 @07:00:00

CSS Angle TLM 0.14537

CSS Sun-Pointing Angle 0.29074

05 May 24 @18:00:00

Pre-Burn

Thruster 1 23904 01 May 24 @07:00:00

Thruster 2 23216

Thruster 3 31536

Thruster 4 32224

Post-Burn

Thruster 1 24176 05 May 24 @18:00:00

Thruster 2 23488

Thruster 3 31840

Thruster 4 32528

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

Kind regards,

Northrop Grumman Corporation | Space Systems