All,
The Orbit# 490 Apogee Contact was nominal for command/telemetry.
Q1 -0.14920100 ActNor.EstInrToBdy[0]
Q2 0.53152300 ActNor.EstInrToBdy[1]
Q3 0.72831200 ActNor.EstInrToBdy[2]
Q4 0.40593700 ActNor.EstInrToBdy[3]
GPS sec 1275838559 ActNor.EstTime
MPS Cmd Vector X 0.208432000
MPS Cmd Vector Y 0.901311000
MPS Cmd Vector Z 0.379731000
GPS sec 1275838559 ActNor.EstTime
UTC time 06/10/2020 15:35:45 output
CSS Angle TLM 0.958588
CSS Sun-Pointing Angle 1.917176
06 June 20 @22:00
CSS Angle TLM 0.744936
CSS Sun-Pointing Angle 1.489872
10 June 20 @15:00
Pre-Burn
Thruster 1 10544 06 June 20 @22:00
Thruster 2 10240
Thruster 3 13216
Thruster 4 13520
Post-Burn
Thruster 1 10800 10 June 20 @15:00
Thruster 2 10496
Thruster 3 13488
Thruster 4 13792
Number of Pulses
Thruster 1 256
Thruster 2 256
Thruster 3 272
Thruster 4 272
Thruster Pairs
Thruster 1 & 2 512
Thruster 3 & 4 544
Sheral Wesley |
Principal Engineer, Satellite Systems
Northrop Grumman Corporation | Space Systems
O: 703-406-5641 | C: 202-236-0802 |
sheral.wesley@ngc.com