[Isocops] IBEX Goat Herder 30 July 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 -0.06813790
Q2 -0.57560500
Q3 -0.59274000
Q4 0.55919200

GPS sec 1406340155
UTC time 07/30/2024 02:02:21
MPS Diff 0.698

MPS Cmd Vector X -0.56968600
MPS Cmd Vector Y 0.75786900
MPS Cmd Vector Z 0.31795000

CSS Angle TLM 0.714911
CSS Sun-Pointing Angle 1.429822
  25 Jul 24 @22:00:000
CSS Angle TLM 0.190774
CSS Sun-Pointing Angle 0.381548
  30 Jul 24 @02:00:00

Pre-Burn
Thruster 1 2736 25 Jul 24 @22:00:000
Thruster 2 2672
Thruster 3 2848
Thruster 4 2912
Post-Burn
Thruster 1 3008 30 Jul 24 @02:00:00
Thruster 2 2944
Thruster 3 3120
Thruster 4 3184
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 544

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>

-------------- next part --------------
An HTML attachment was scrubbed...
URL: <https://lists.sr.unh.edu/pipermail/isocops/attachments/20240730/e7b176e9/attachment.htm>