Hello team,
The apogee contact was nominal, and the maneuver was successful.
Tasks Accomplished:
Reset FDC Totals
Results from the Inertial Maneuver:
Q1 0.76113700
Q2 -0.17595800
Q3 -0.44215100
Q4 0.44069500
GPS sec 1414354033
UTC time 10/30/2024 20:06:59
MPS Diff 0.885
MPS Cmd Vector X -0.82280800
MPS Cmd Vector Y -0.51750800
MPS Cmd Vector Z -0.23488800
CSS Angle TLM 0.817571
CSS Sun-Pointing Angle 1.635142
25 Oct 24 @02:30:00
CSS Angle TLM 0.300296
CSS Sun-Pointing Angle 0.600592
30 Oct 24 @20:00:00
Pre-Burn
Thruster 1 7856 25 Oct 24 @02:30:00
Thruster 2 7648
Thruster 3 9408
Thruster 4 9616
Post-Burn
Thruster 1 8160 30 Oct 24 @20:00:00
Thruster 2 7952
Thruster 3 9696
Thruster 4 9904
Number of Pulses
Thruster 1 304
Thruster 2 304
Thruster 3 288
Thruster 4 288
Thruster Pairs
Thruster 1 & 2 608
Thruster 3 & 4 576
Best,
Andrea Coca Gonzales | Associate
Engineer Satellite Systems | MEV | ICESat-2 | TESS | IBEX
Northrop Grumman Corporation | Dulles Chapter Adelante Member Engagement Lead | Space Systems