[Isocops] IBEX Goat Herder 05 Nov 2022

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

The apogee tracking contact was nominal and the sun maneuver successful.

Results from the Sun  Maneuver:

Q1          -0.06173700        ActNor.EstInrToBdy[0]
Q2          -0.78924800        ActNor.EstInrToBdy[1]
Q3          0.40991700          ActNor.EstInrToBdy[2]
Q4          0.45303900          ActNor.EstInrToBdy[3]
GPS sec 1351654110         ActNor.EstTime
UTC time             11/05/2022 03:28:16       output

CSS Angle TLM   0.218503
CSS Sun-Pointing Angle 0.437006
                                28 Oct 22 @18:32:00
CSS Angle TLM   1.96394
CSS Sun-Pointing Angle 3.92788
                                05 Nov 22 at 03:30:00
Pre-Burn
Thruster 1            8064       28 Oct 22 @18:32:00
Thruster 2            7824
Thruster 3            10224
Thruster 4            10464
Post-Burn
Thruster 1            8400       05 Nov 22 at 03:30:00
Thruster 2            8160
Thruster 3            10864
Thruster 4            11104
Number of Pulses
Thruster 1            336
Thruster 2            336
Thruster 3            640
Thruster 4            640
Thruster Pairs
Thruster 1 & 2    672
Thruster 3 & 4    1280


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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