All,
The perigee contacts were nominal. The inertial maneuver was successful. We were able to redump the missing data from Orbit 666. The orbit 667 SSR Dump
took a hit at the end of the dump. We were able to recover the missing data on the following contact. The Orbit 669 ATS was successfully uplinked.
Tasks Accomplished:
SSR Dump -> Dump New
Reset FDC Totals
Reset Master Timer
CAR # 1424 Redump Orbit 666 Missing Blocks
CAR # 1425 Orbit 669 ATS Uplink
IBEX_2024_327_o0669a_v001
CAR #1427 Redump Orbit 667 Missing Blocks
Results from the Inertial Maneuver:
Q1 0.74118800 ActNor.EstInrToBdy[0]
Q2 -0.31223000 ActNor.EstInrToBdy[1]
Q3 -0.21993100 ActNor.EstInrToBdy[2]
Q4 0.55207100 ActNor.EstInrToBdy[3]
GPS sec 1415463075 ActNor.EstTime
UTC time
11/12/2024 16:11:01 output
MPS Diff
0.768 deg
MPS Cmd Vector X -0.66444600
MPS Cmd Vector Y -0.68207300
MPS Cmd Vector Z -0.30542900
CSS Angle TLM 0.674056
CSS Sun-Pointing Angle 1.348112
09 Nov 24 @20:30:00
CSS Angle TLM 0.181794
CSS Sun-Pointing Angle 0.363588
12 Nov 24 @17:00:00
Pre-Burn
Thruster 1 8800 09 Nov 24 @20:30:00
Thruster 2 8592
Thruster 3 10592
Thruster 4 10800
Post-Burn
Thruster 1 8912 12 Nov 24 @17:00:00
Thruster 2 8704
Thruster 3 10736
Thruster 4 10944
Number of Pulses
Thruster 1 112
Thruster 2 112
Thruster 3 144
Thruster 4 144
Thruster Pairs
Thruster 1 & 2 224
Thruster 3 & 4 288
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
IBEX MOC (703)404-7470
Cell (301) 606-1430