[Isocops] IBEX Goat Herder 10 May 2024

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

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,

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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