Good morning team,

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

Tasks accomplished : Reset FDC totals.

Results from the inertial maneuver:

Q1 0.07771270

Q2 0.62725500

Q3 0.44047700

Q4 0.63756700

GPS sec 1397830218

UTC time 04/22/2024 14:10:04

MPS Diff 0.876

MPS Cmd Vector X 0.86502700

MPS Cmd Vector Y 0.464154000

MPS Cmd Vector Z 0.190501000

CSS Angle TLM 0.3456

CSS Sun-Pointing Angle 0.6912

17 Apr 24 @18:00:00

CSS Angle TLM 0.244694

CSS Sun-Pointing Angle 0.489388

22 Apr 24 @13:00:00

Pre-Burn

Thruster 1 23040 17 Apr 24 @18:00:00

Thruster 2 22384

Thruster 3 30672

Thruster 4 31328

Post-Burn

Thruster 1 23344 22 Apr 24 @13:00:00

Thruster 2 22656

Thruster 3 30960

Thruster 4 31648

Number of Pulses

Thruster 1 304

Thruster 2 272

Thruster 3 288

Thruster 4 320

Thruster Pairs

Thruster 1 & 2 576

Thruster 3 & 4 608

Kind regards,

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

Northrop Grumman Corporation | Space Systems