[Isocops] IBEX Goat Herder 03 July 2024

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

Good morning team,

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

Results from the inertial maneuver:

Q1 -0.41111000
Q2 -0.36747500
Q3 -0.44579600
Q4 0.70513600

GPS sec 1404014774
UTC time 07/03/2024 04:06:00
MPS Diff 0.580

MPS Cmd Vector X -0.15736200
MPS Cmd Vector Y 0.90989100
MPS Cmd Vector Z 0.38384400

CSS Angle TLM 0.203672
CSS Sun-Pointing Angle 0.407344
  28 Jun 24 @17:30:00
CSS Angle TLM 0.14671
CSS Sun-Pointing Angle 0.29342
  03 Jul 24 @04:00:00
Pre-Burn
Thruster 1 1120 28 Jun 24 @17:30:00
Thruster 2 1088
Thruster 3 1088
Thruster 4 1120
Post-Burn
Thruster 1 1392 03 Jul 24 @04:00:00
Thruster 2 1360
Thruster 3 1392
Thruster 4 1424
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 608

Best,
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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