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PCADGRATE
Static Version: Min --- Full Range

One Week Three Month One Year Five Year Full Range Min Mean Max

Delta/Yr below is a slope of the linear fitting over the data of the period. Delta/Yr/Yr is a slope of the liner fitting over the devivative data of the period. Slope listed on a linked plot is the slope computed on the last few periods of the data to show the direction of the trend, and different from that of Delta/Yr.

MSID MeanRMSDelta/YrDelta/Yr/YrUnitDescriptionLimit Violation
ai1ax1xon0.0016.737e-04-0.05 +/- 0.28(2.12+/-15.16)e-4DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off-0.0043.296e-04-3.94 +/- 0.210.00 +/- 0.00No Violation Check
ai1ax1yon0.0026.549e-04-0.05 +/- 0.270.00 +/- 0.00DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-0.0043.282e-04-3.96 +/- 0.210.00 +/- 0.00No Violation Check
ai1ax2xon-2.160e-046.962e-04-0.07 +/- 0.29(1.11+/-18.26)e-4DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-0.0043.279e-04-3.95 +/- 0.210.00 +/- 0.00No Violation Check
ai1ax2yon7.895e-046.708e-04-0.06 +/- 0.280.00 +/- 0.00DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-0.0043.297e-04-3.96 +/- 0.210.00 +/- 0.00No Violation Check
ai2ax1xon0.0013.018e-04-0.05 +/- 0.200.00 +/- 0.00DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-0.0110.002-3.75 +/- 0.15-0.01 +/- 0.04No Violation Check
ai2ax1yon0.0023.081e-04-0.05 +/- 0.200.00 +/- 0.00DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-0.0130.002-3.76 +/- 0.150.01 +/- 0.03No Violation Check
ai2ax2xon0.0013.062e-04-0.06 +/- 0.200.00 +/- 0.00DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-0.0110.002-3.74 +/- 0.15-(1.10+/-289.70)e-4No Violation Check
ai2ax2yon0.0023.068e-04-0.04 +/- 0.200.00 +/- 0.00DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-0.0130.003-3.75 +/- 0.16-0.01 +/- 0.04No Violation Check
aoalpang -0.8920.023-36.80 +/- 20.150.50 +/- 0.46DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0025.208e-04-0.39 +/- 0.420.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 -0.0025.345e-04-0.43 +/- 0.440.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0024.955e-04-0.48 +/- 0.410.02 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0600.044-0.18 +/- 35.890.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -0.3190.021-44.10 +/- 16.950.36 +/- 0.40DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0025.211e-04-0.39 +/- 0.430.02 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 -0.0025.346e-04-0.43 +/- 0.440.01 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0024.954e-04-0.48 +/- 0.410.01 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 2.097e+0332.289-(2.05+/-3.11)e4(8.93+/-2.53)e2KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -1.058e+044.140e+04-(3.95+/-338.00)e5(8.62+/-2.87)e2KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 1.263e+0353.330(2.77+/-4.47)e4(2.22+/-0.38)e3KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 0.0030.003-1.19 +/- 2.060.11 +/- 0.03KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0120.002-1.36 +/- 1.770.09 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0080.002-1.41 +/- 1.450.10 +/- 0.02KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -3.594e-058.857e-04-0.02 +/- 0.72-(3.31+/-77.36)e-4naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 1.389e-067.953e-040.00 +/- 0.65-0.00 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 5.739e-043.428e-04-0.00 +/- 0.28-(6.43+/-31.04)e-4naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 -9.210e-041.887e-05-0.02 +/- 0.020.00 +/- 0.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0025.999e-05-0.04 +/- 0.050.00 +/- 0.00naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 4.416e-069.683e-07-1.00 +/- 0.00(2.10+/-2.04)e-7naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0025.112e-04-0.35 +/- 0.420.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 -0.0025.302e-04-0.40 +/- 0.430.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0024.837e-04-0.45 +/- 0.400.02 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

If you have any questions, please contact swolk@cfa.harvard.edu.

Data Updated: Feb 05, 2026
Last Site Modification: Sep 30, 2021