Good morning team,
The apogee contact was nominal, and the inertial maneuver was successful.
Results from the inertial maneuver:
Q1 -0.41111000
Q2 -0.36747500
Q3 -0.44579600
Q4 0.70513600
GPS sec 1404014774
UTC time 07/03/2024 04:06:00
MPS Diff 0.580
MPS Cmd Vector X -0.15736200
MPS Cmd Vector Y 0.90989100
MPS Cmd Vector Z 0.38384400
CSS Angle TLM 0.203672
CSS Sun-Pointing Angle 0.407344
28 Jun 24 @17:30:00
CSS Angle TLM 0.14671
CSS Sun-Pointing Angle 0.29342
03 Jul 24 @04:00:00
Pre-Burn
Thruster 1 1120 28 Jun 24 @17:30:00
Thruster 2 1088
Thruster 3 1088
Thruster 4 1120
Post-Burn
Thruster 1 1392 03 Jul 24 @04:00:00
Thruster 2 1360
Thruster 3 1392
Thruster 4 1424
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 608
Best,
Andrea Coca Gonzales | Associate
Engineer Satellite Systems | MEV | ICESat-2 | TESS | IBEX
Northrop Grumman Corporation | Space Systems