Good morning team,
The apogee contact was nominal, and the inertial maneuver was successful.
Results from the inertial maneuver:
Q1 -0.16342800
Q2 -0.53247400
Q3 -0.67520100
Q4 0.48359800
GPS sec 1404814117
UTC time 07/12/2024 10:08:23
MPS Diff 0.719
MPS Cmd Vector X -0.30254900
MPS Cmd Vector Y 0.87831600
MPS Cmd Vector Z 0.37016800
CSS Angle TLM 0.279765
CSS Sun-Pointing Angle 0.55953
07 Jul 24 @13:00:00
CSS Angle TLM 0
CSS Sun-Pointing Angle 0
12 Jul 24 @10:00:00
Pre-Burn
Thruster 1 1664 07 Jul 24 @13:00:00
Thruster 2 1632
Thruster 3 1696
Thruster 4 1728
Post-Burn
Thruster 1 1904 12 Jul 24 @10:00:00
Thruster 2 1872
Thruster 3 1968
Thruster 4 2000
Number of Pulses
Thruster 1 240
Thruster 2 240
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 480
Thruster 3 & 4 544
Best,
Andrea Coca Gonzales | Associate
Engineer Satellite Systems | MEV | ICESat-2 | TESS | IBEX
Northrop Grumman Corporation | Space Systems