Good morning team,

The apogee contact was nominal, and the inertial maneuver was successful. We took the full contact on Ibex -1.

Tasks accomplished:

Reset FDC totals.

Results from the inertial maneuver:

Q1 -0.58946600

Q2 -0.08098700

Q3 -0.63893500

Q4 0.48757900

GPS sec 1399381289

UTC time 05/10/2024 13:01:15

MPS Diff 0.451

MPS Cmd Vector X 0.67437200

MPS Cmd Vector Y 0.681305000

MPS Cmd Vector Z 0.284685000

CSS Angle TLM 0.137056

CSS Sun-Pointing Angle 0.274112

05 May 24 @07:00:00

CSS Angle TLM 0.351102

CSS Sun-Pointing Angle 0.702204

10 May 24 @13:00:00

Pre-Burn

Thruster 1 24176 05 May 24 @07:00:00

Thruster 2 23488

Thruster 3 31840

Thruster 4 32528

Post-Burn

Thruster 1 24448 10 May 24 @13:00:00

Thruster 2 23760

Thruster 3 32176

Thruster 4 32864

Number of Pulses

Thruster 1 272

Thruster 2 272

Thruster 3 336

Thruster 4 336

Thruster Pairs

Thruster 1 & 2 544

Thruster 3 & 4 672

Best,

Northrop Grumman Corporation | Space Systems