[Isocops] IBEX Goat Herder for 8 March 2023

[Perry, Timothy E [US] (SP)]

All,

   The apogee contact was nominal for CMD and TLM. The inertial maneuver was successful.



Results from the Inertial Maneuver:
Q1 0.72325800 ActNor.EstInrToBdy[0]
Q2 0.12936800 ActNor.EstInrToBdy[1]
Q3 0.63363100 ActNor.EstInrToBdy[2]
Q4 0.24222700 ActNor.EstInrToBdy[3]

GPS sec 1362322923 ActNor.EstTime
UTC time 03/08/2023 15:01:49 output

MPS Diff 0.725 deg

MPS Cmd Vector X 0.980670000
MPS Cmd Vector Y -0.175691000
MPS Cmd Vector Z -0.086130000

CSS Angle TLM 0.990316
CSS Sun-Pointing Angle 1.980632
  04 Mar 23 at 06:30:00

CSS Angle TLM 1.13453
CSS Sun-Pointing Angle 2.26906
  08 Mar 23 at 15:00:00

Pre-Burn
Thruster 1 752 04 Mar 23 at 06:30:00
Thruster 2 752
Thruster 3 928
Thruster 4 928
Post-Burn
Thruster 1 1040 08 Mar 23 at 15:00:00
Thruster 2 1040
Thruster 3 1232
Thruster 4 1232
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 608



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