All,
The Perigee passes were nominal for CMD and TLM. The Inertial maneuver was successful.
The following was accomplished:
Reset the Master Timer
SSR Dump - Dump New
CAR # 1050 ATS upload – IBEX_2019_215_o0456a_V001 93 cmds
CAR # 1048 Dump Orbit 452 Missing blocks
CAR # 1051 Dump Orbit 452 Missing blocks
Results from the Inertial maneuver:
Q1 0.03999430
ActNor.EstInrToBdy[0]
Q2 -0.56989700
ActNor.EstInrToBdy[1]
Q3 -0.72820500
ActNor.EstInrToBdy[2]
Q4 0.37859600
ActNor.EstInrToBdy[3]
GPS sec 1248088134
ActNor.EstTime
UTC time
07/25/2019 11:08:40 output
MPS Cmd Vector X -0.493473000
MPS Cmd Vector Y 0.801565000
MPS Cmd Vector Z 0.337605000
CSS Angle TLM
0.530449
CSS Sun-Pointing Angle
1.060898
20 July 19 @ 13:00
CSS Angle TLM
1.46714
CSS Sun-Pointing Angle
2.93428
25 July 19 @ 11:00
Pre-Burn
Thruster 1
14944 20 July 19 @ 13:00
Thruster 2
14560
Thruster 3
17776
Thruster 4
18160
Post-Burn
Thruster 1
15184 25 July 19 @ 11:00
Thruster 2
14800
Thruster 3
18064
Thruster 4
18448
Number of Pulses
Thruster 1
240
Thruster 2
240
Thruster 3
288
Thruster 4
288
Thruster Pairs
Thruster 1 & 2
480
Thruster 3 & 4
576
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
Office (703) 406-5976
Cell (301) 606-1430