Guys,

The Perigee contacts on 16 Apr 19 were nominal for CMD and TLM. The inertial maneuver was nominal.

The following was accomplished::

Reset the Master Timer

Set_SC_Time.scr

Reset_FDC_Totals

@FMI_SetDownlink (320ksps)

@FTG_DumpBackorbit (from start,0,0,0,0)

Dumped SSR -> Dump New (VC2=31778/17)

CAR 1031 Orbit# 444 ATS upload

IBEX_2019_106_o0444a_v001.scr (13 - 105)

CAR 1032 Orbit# 444 HGC Cal Upload

IBEX_2019_106_o0444a_HGC_v001.scr (106 – 169)

CSS Angle TLM	0.437455
CSS Sun-Pointing Angle	0.87491
CSS Sun-Pointing Angle	0.87491	11 Apr 19 @ 14:00
CSS Angle TLM	0.350545
CSS Sun-Pointing Angle	0.70109
CSS Sun-Pointing Angle	0.70109	16 Apr 19 @ 09:00
Pre-Burn
Thruster 1	9088	11 Apr 19 @ 14:00
Thruster 2	8864
Thruster 3	11184
Thruster 4	11408
Post-Burn
Thruster 1	9360	16 Apr 19 @ 09:00
Thruster 2	9136
Thruster 3	11488
Thruster 4	11712
Number of Pulses
Thruster 1	272
Thruster 2	272
Thruster 3	304
Thruster 4	304
Thruster Pairs
Thruster 1 & 2	544
Thruster 3 & 4	608

Sheral R. Wesley

Principal Engr Satellite Systems

ICESat2, IBEX and OCO2 Mission OPS

CRS/CYGNUS Mission Planning

Northrop Grumman Innovation Systems

Bldg. 2 Room 1337

Cell (202) 236-0802

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