[Isocops] IBEX Goat Herder 08 August 2024

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

Hello team,

    The apogee contact was nominal, and the inertial maneuver was successful.

Results from the inertial maneuver:

Q1 -0.44672100
Q2 -0.39460000
Q3 0.05729290
Q4 0.80090500

GPS sec 1407118038
UTC time 08/08/2024 02:07:04
MPS Diff 0.586

MPS Cmd Vector X -0.68720300
MPS Cmd Vector Y 0.67033200
MPS Cmd Vector Z 0.28001300

CSS Angle TLM 0.189746
CSS Sun-Pointing Angle 0.379492
  03 Aug 24 @12:00:00
CSS Angle TLM 0.121947
CSS Sun-Pointing Angle 0.243894
  08 Aug 24 @02:00:00
Pre-Burn
Thruster 1 3280 03 Aug 24 @12:00:00
Thruster 2 3216
Thruster 3 3408
Thruster 4 3472
Post-Burn
Thruster 1 3552 08 Aug 24 @02:00:00
Thruster 2 3488
Thruster 3 3696
Thruster 4 3760
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 576

Kind regards,

Andrea Coca Gonzales | Associate Engineer Satellite Systems | MEV | ICESat-2 | TESS | IBEX
Northrop Grumman Corporation  |  Space Systems
Andrea.CocaGonzales at ngc.com<mailto:Andrea.CocaGonzales at ngc.com>

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