Good morning team,

The apogee contact was nominal, and the inertial maneuver was successful.

Tasks accomplished:

Re-enabled flight computer back orbit data

Executed CAR #1335 - 2024 ISN Season and Hi Background Test sweep table uploads

Pass 7 – Upload Lo Normal Sweep table and normal star sensor telemetry cadence (beginning of orbit 646b)

USHI01, 05/01/24, DOY 122, 07:00 – 08:00 UTC

Results from the inertial maneuver:

Q1 0.38910600 ActNor.EstInrToBdy[0]

Q2 0.47365600 ActNor.EstInrToBdy[1]

Q3 0.76436800 ActNor.EstInrToBdy[2]

Q4 0.19996900 ActNor.EstInrToBdy[3]

GPS sec 1398582080

UTC time 05/01/2024 07:01:06

MPS Diff 0.834

MPS Cmd Vector X 0.77882000

MPS Cmd Vector Y 0.579331000

MPS Cmd Vector Z 0.240448000

CSS Angle TLM 0.137056

CSS Sun-Pointing Angle 0.274112

26 Apr 24 @19:00:00

CSS Angle TLM 0.24866

CSS Sun-Pointing Angle 0.49732

01 May 24 @07:00:00

Pre-Burn

Thruster 1 23632 26 Apr 24 @19:00:00

Thruster 2 22944

Thruster 3 31264

Thruster 4 31952

Post-Burn

Thruster 1 23904 01 May 24 @07:00:00

Thruster 2 23216

Thruster 3 31536

Thruster 4 32224

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

Best,

Andrea Coca Gonzales | Associate Engineer Satellite Systems | MEV | ICESat-2 | TESS

Northrop Grumman Corporation | Space Systems