Good morning team,
The apogee contact was nominal, and the inertial maneuver was successful. The ebno readings and agc were low, so we were unable to upload the ATS for orbit
653. We took the whole pass on Ibex-2.
Tasks accomplished:
Reset FDC totals.
Results from the inertial maneuver
Q1 -0.21690300
Q2 0.50313300
Q3 0.76885300
Q4 0.32966000
GPS sec 1403348552
UTC time 06/25/2024 11:02:18
MPS Diff 0.788
MPS Cmd Vector X -0.00884400
MPS Cmd Vector Y 0.92129900
MPS Cmd Vector Z 0.38875400
CSS Angle TLM 0.360994
CSS Sun-Pointing Angle 0.721988
19 Jun 24 @02:00:00
CSS Angle TLM 0.626826
CSS Sun-Pointing Angle 1.253652
25 Jun 24 @11:00:00
Pre-Burn
Thruster 1 544 19 Jun 24 @02:00:00
Thruster 2 544
Thruster 3 544
Thruster 4 544
Post-Burn
Thruster 1 816 25 Jun 24 @11:00:00
Thruster 2 816
Thruster 3 816
Thruster 4 816
Number of Pulses
Thruster 1 272
Thruster 2 272
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 544
Thruster 3 & 4 544
Kind regards,
Andrea Coca Gonzales | Associate
Engineer Satellite Systems | MEV | ICESat-2 | TESS | IBEX
Northrop Grumman Corporation | Space Systems