[Isocops] IBEX Goat Herder for 9 Nov 24

[Wesley, Sheral R [US] (SP)]

All,
The apogee contact was nominal for command/telemetry and the sun maneuver successful

Results from the sun maneuver
Q1          0.64042700
Q2          -0.47794700
Q3          -0.09971680
Q4          0.59285500

GPS sec 1415221603
UTC time              11/09/2024 21:06:29

CSS Angle TLM   0.692386
CSS Sun-Pointing Angle  1.384772
                                03 Nov 24 @13:30:00
CSS Angle TLM   0.674056
CSS Sun-Pointing Angle  1.348112
                                09 Nov 24 @20:30:00
Pre-Burn
Thruster 1           8464     03 Nov 24 @13:30:00
Thruster 2           8256
Thruster 3           10000
Thruster 4           10208
Post-Burn
Thruster 1           8800     09 Nov 24 @20:30:00
Thruster 2           8592
Thruster 3           10592
Thruster 4           10800
Number of Pulses
Thruster 1           336
Thruster 2           336
Thruster 3           592
Thruster 4           592
Thruster Pairs
Thruster 1 & 2   672
Thruster 3 & 4   1184


Best Regards,

Sheral Wesley  |  Sr Principal Engineer, Satellite Systems
Northrop Grumman Corporation  |  Space Systems
O: 703-406-5641  |  C: 202-236-0802  |  sheral.wesley at ngc.com<mailto:sheral.wesley at ngc.com>
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