All,
The spacecraft is nominal. The inertial maneuver was successful. I was unable to dump the SSR or uplink the Orbit 629 ATS. The first contact USHI02 was
canceled due to an issue at the tracking station. The second contact USAK01, we had a very low receiver signal strength. The data kept dropping out during the contact. The AGC stayed between -122 & -121. I was able to extend the contact on Nov 23 to 2 hours.
The contact is scheduled for a 320k downlink.
Tasks Accomplished:
Reset Master Timer
Results from the Inertial Maneuver:
Q1 0.66999100 ActNor.EstInrToBdy[0]
Q2 -0.44629600 ActNor.EstInrToBdy[1]
Q3 -0.10764100 ActNor.EstInrToBdy[2]
Q4 0.58339100 ActNor.EstInrToBdy[3]
GPS sec 138398438 ActNor.EstTime
UTC time
05/25/1984 20:00:24 output
MPS Diff
0.608 deg
MPS Cmd Vector X -0.66229300
MPS Cmd Vector Y -0.683815000
MPS Cmd Vector Z -0.306210000
CSS Angle TLM 0.932722
CSS Sun-Pointing Angle 1.865444
9 Nov 23 @20:00:00
CSS Angle TLM 0.238211
CSS Sun-Pointing Angle 0.476422
14 Nov 23 @07:30:00
Pre-Burn
Thruster 1 14368 9 Nov 23 @20:00:00
Thruster 2 13952
Thruster 3 18752
Thruster 4 19168
Post-Burn
Thruster 1 14496 14 Nov 23 @07:30:00
Thruster 2 14080
Thruster 3 18928
Thruster 4 19344
Number of Pulses
Thruster 1 128
Thruster 2 128
Thruster 3 176
Thruster 4 176
Thruster Pairs
Thruster 1 & 2 256
Thruster 3 & 4 352
Timothy E.Perry
CRS IBEX OCO-2
Mission Operations
Office (703) 406-5976
Cell (301) 606-1430