All,
The spacecraft is nominal. The inertial maneuver was successful. We commanded the Hi sweep table back to normal sweep. The ATS for Orbit 634 has been uplinked
and the SSR data for orbit 632 has been downlinked.
Tasks Accomplished:
CAR# 1335 – ISN Season and Hi background test Sweep table uplink
Pass #3 Upload Hi Normal Sweep Table (completed)
CAR# 1363 – Orbit # 634 ATS Upload
IBEX_2024_007_o0634a_v001 96 Commands
Set Spacecraft Clock
Reser FDC Totals
SSR Dump -> Dump New
Results from the Inertial Maneuver:
Q1 0.09790130 ActNor.EstInrToBdy[0]
Q2 0.82868400 ActNor.EstInrToBdy[1]
Q3 -0.53067400 ActNor.EstInrToBdy[2]
Q4 0.14860500 ActNor.EstInrToBdy[3]
GPS sec 1387927852 ActNor.EstTime
UTC time
12/29/2023 23:30:38 output
MPS Diff
0.720 deg
MPS Cmd Vector X 0.14807800
MPS Cmd Vector Y -0.903368000
MPS Cmd Vector Z -0.402491000
CSS Angle TLM 0.91564
CSS Sun-Pointing Angle 1.83128
24 Dec 23 @16:00:00
CSS Angle TLM 1.31
CSS Sun-Pointing Angle 2.62
29 Dec 23 @23:30:00
Pre-Burn
Thruster 1 16896 24 Dec 23 @16:00:00
Thruster 2 16384
Thruster 3 22368
Thruster 4 22880
Post-Burn
Thruster 1 17200 29 Dec 23 @23:30:00
Thruster 2 16688
Thruster 3 22672
Thruster 4 23184
Number of Pulses
Thruster 1 304
Thruster 2 304
Thruster 3 304
Thruster 4 304
Thruster Pairs
Thruster 1 & 2 608
Thruster 3 & 4 608
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430