All,

The Apogee pass was nominal for CMD and TLM. The Inertial maneuver was successful.

Results from the Inertial Maneuver:

Q1 -0.63168700 ActNor.EstInrToBdy[0]

Q2 0.45750000  ActNor.EstInrToBdy[1]

Q3 -0.62315400 ActNor.EstInrToBdy[2]

Q4 0.05782350  ActNor.EstInrToBdy[3]

GPS sec 1265907562 ActNor.EstTime

UTC time 02/16/2020 16:59:08  

MPS Diff 0.480 deg

MPS Cmd Vector X 0.841256000

MPS Cmd Vector Y -0.492320000

MPS Cmd Vector Z -0.223403000

CSS Angle TLM   1.378    

CSS Sun-Pointing Angle   2.756    

10 Feb 20 @ 23:30

CSS Angle TLM   1.137    

CSS Sun-Pointing Angle   2.274    

16 Feb 20 @ 17:00

Pre-Burn

Thruster 1 4016  10 Feb 20 @ 23:30

Thruster 2 3872 

Thruster 3 5440 

Thruster 4 5584 

Post-Burn

Thruster 1 4272  16 Feb 20 @ 17:00

Thruster 2 4128 

Thruster 3 5744 

Thruster 4 5888 

Number of Pulses

Thruster 1 256   

Thruster 2 256   

Thruster 3 304   

Thruster 4 304   

Thruster Pairs   

Thruster 1 & 2    512       

Thruster 3 & 4    608       

Eric Chubin  | Engineer Systems

Northrop Grumman Corporation  |  Space Systems

O: 703-429-7015  |  C: 240-328-2098  |  eric.chubin@ngc.com