Good morning team,

    The apogee contact was nominal, and the inertial maneuver was successful. We took the contact on Ibex -1 and switched over to Ibex -2 about 15 minutes after AOS. All the data points looked about the same and we did not see any issues.

Tasks accomplished:

Reset FDC totals.

Results from the inertial maneuver:                 

Q1 -0.48710100

Q2 -0.26974300

Q3 -0.60882000

Q4 0.56507500

GPS sec 1401710616

UTC time 06/06/2024 12:03:22

MPS Diff 0.550

MPS Cmd Vector X 0.28454900

MPS Cmd Vector Y 0.88340600

MPS Cmd Vector Z 0.37232400

CSS Angle TLM 0.186626

CSS Sun-Pointing Angle 0.373252

  02 Jun 24 @10:00:00

CSS Angle TLM 0.217606

CSS Sun-Pointing Angle 0.435212

  06 Jun 24 @12:00:00

Pre-Burn

Thruster 1 25808 02 Jun 24 @10:00:00

Thruster 2 25056

Thruster 3 33616

Thruster 4 34368

Post-Burn

Thruster 1 26064 06 Jun 24 @12:00:00

Thruster 2 25312

Thruster 3 33920

Thruster 4 34672

Number of Pulses

Thruster 1 256

Thruster 2 256

Thruster 3 304

Thruster 4 304

Thruster Pairs  

Thruster 1 & 2 512

Thruster 3 & 4 608

Best,

Andrea Coca Gonzales | Associate Engineer Satellite Systems | MEV | ICESat-2 | TESS | IBEX

Northrop Grumman Corporation  |  Space Systems

C: 703-582-8233  |  Andrea.CocaGonzales@ngc.com