All,
The perigee contacts were nominal. The sun maneuver was successful. The current star percent valid is at 79%.
The following contact was extended to successfully re-dump Orbit 624 VC2 data
IBEX,AUWA01,ADD,10/26/23,299,20:00:00,10/26/23,299,21:30:00,LAHO 64K IBEX-3 Orbit# 625 Tracking Contact 11re Perigee
Tasks Accomplished:
Reset Master Timer
SSR Dump -> Dump New (4136 est. remaining blocks)
Set Static Z rate
CAR# 1349 Upload Orbit# 626 (26 Oct – 4 Nov 23)
IBEX_2023_299_o0626a_v001.scr (753-855)
CAR# 1350 Upload Orbit# 627 (4 Nov – 13 Nov 23)
IBEX_2023_308_o0627a_v002.scr (856-953)
CAR# 1348 Redump orbit# 624 Blocks (SSR Dump.scr, Start 123010, Numblks, 29740)
Results from the Sun Maneuver:
CSS Angle TLM 0.976787
CSS Sun-Pointing Angle 1.953574
25 Oct 23@01:00:00
CSS Angle TLM 1.64746
CSS Sun-Pointing Angle 3.29492
26 Oct 23@11:15:00
Pre-Burn
Thruster 1 13440 25 Oct 23@01:00:00
Thruster 2 13072
Thruster 3 17328
Thruster 4 17696
Post-Burn
Thruster 1 13632 26 Oct 23@11:15:00
Thruster 2 13216
Thruster 3 17760
Thruster 4 18176
Number of Pulses
Thruster 1 192
Thruster 2 144
Thruster 3 432
Thruster 4 480
Thruster Pairs
Thruster 1 & 2 336
Thruster 3 & 4 912
Best Regards,
Sheral Wesley |
Sr
Principal Engineer, Satellite Systems
Northrop Grumman Corporation | Space Systems
O: 703-406-5641 | C: 202-236-0802 |
sheral.wesley@ngc.com