[Isocops] IBEX Goat Herder 06 June 2024

[Coca Gonzales, Andrea [US] (SP)]

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 at ngc.com<mailto:Andrea.CocaGonzales at ngc.com>

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