All,
The perigee contacts were nominal. The SSR dump had 74 errors and will need to be redumped on the next high-rate perigee contact. The orbit 610 ATS was uplinked and the inertial
maneuver was successful.
Tasks Accomplished:
CAR#1319 Orbit# 610 ATS uplink
IBEX_2023_154_o0610a_v001 106 Cmds
Reset FDC Totals
Reset Master Timer
SSR Dump -> Dump New
Results from the Inertial Maneuver:
Q1 -0.46009000 ActNor.EstInrToBdy[0]
Q2 -0.33716400 ActNor.EstInrToBdy[1]
Q3 -0.75659000 ActNor.EstInrToBdy[2]
Q4 0.31970000 ActNor.EstInrToBdy[3]
GPS sec 1369116053 ActNor.EstTime
UTC time
05/26/2023 06:00:39 output
MPS Diff
0.693 deg
MPS Cmd Vector X 0.474042000
MPS Cmd Vector Y 0.811388000
MPS Cmd Vector Z 0.341955000
CSS Angle TLM 0.234902
CSS Sun-Pointing Angle 0.469804
21 May 23@11:00:00
CSS Angle TLM 0.0279765
CSS Sun-Pointing Angle 0.055953
25 May 23@17:00:00
Pre-Burn
Thruster 1 4816 21 May 23@11:00:00
Thruster 2 4704
Thruster 3 6288
Thruster 4 6400
Post-Burn
Thruster 1 5104 25 May 23@17:00:00
Thruster 2 4992
Thruster 3 6592
Thruster 4 6704
Number of Pulses
Thruster 1 288
Thruster 2 288
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 576
Thruster 3 & 4 608
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430