All,
The apogee contact was nominal and the sun maneuver was successful. The star percent valid was at 21, so we were unable to set the static Z rate. The Orbit 590 ATS was successfully uplinked.
Tasks Accomplished:
CAR # 1279 Orbit #590 ATS uplink
IBEX_2022_338_o0590a_v001 98 cmds
Results from the Sun Maneuver:
CSS Angle TLM 0.228957
CSS Sun-Pointing Angle 0.457914
25 Nov
22@07:30:00
CSS Angle TLM 0.901789
CSS Sun-Pointing Angle 1.803578
30 Nov
22@19:00:00
Pre-Burn
Thruster 1 736 25 Nov 22@07:30:00
Thruster 2 736
Thruster 3 1040
Thruster 4 1040
Post-Burn
Thruster 1 1120 30 Nov 22@19:00:00
Thruster 2 1072
Thruster 3 1616
Thruster 4 1664
Number of Pulses
Thruster 1 384
Thruster 2 336
Thruster 3 576
Thruster 4 624
Thruster Pairs
Thruster 1 & 2 720
Thruster 3 & 4 1200