All,
The perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful. The Instrument ATS for Orbit 491 was uplinked. At LOS there were 226 stored commands onboard. The Master Reset timer reset to zero thru stored command.
The following was accomplished:
CAR 2000 ATS upload – Ibex_2020_167_o0491a_INST_V001 46 CMDS
SSR Dump –Dump New
Set Spacecraft Clock
Reset FDC Counters
Q1 -0.27220500
ActNor.EstInrToBdy[0]
Q2 0.48259500
ActNor.EstInrToBdy[1]
Q3 0.56508900
ActNor.EstInrToBdy[2]
Q4 0.61129500
ActNor.EstInrToBdy[3]
MPS
Cmd Vector X 0.279738000
MPS
Cmd Vector Y 0.884416000
MPS
Cmd Vector Z 0.373571000
GPS sec 1275516331
ActNor.EstTime
UTC time 06/06/2020 22:05:17 output
MPS Diff 0.810
deg
CSS Angle TLM 1.45804
CSS Sun-Pointing Angle 2.91608
02 May 20 @07:00
CSS Angle TLM 0.958588
CSS Sun-Pointing Angle 1.917176
06 May 20 @22:00
Pre-Burn
Thruster 1 10240 02 May 20 @07:00
Thruster 2 9968
Thruster 3 12912
Thruster 4 13184
Post-Burn
Thruster 1 10544 06 May 20 @22:00
Thruster 2 10240
Thruster 3 13216
Thruster 4 13520
Number of Pulses
Thruster 1 304
Thruster 2 272
Thruster 3 304
Thruster 4 336
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 640
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2
Office (703) 406-5976
Cell (301) 606-1430
