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PCADGRATE
Static Version: Mean --- One Week

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
ai1ax1xon8.819e-050.104-0.94 +/- 1.59(1.94+/-1.92)e2DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off3.295e-051.972e-04-3.88 +/- 0.020.61 +/- 1.18No Violation Check
ai1ax1yon0.0080.105-0.95 +/- 1.61(1.99+/-1.94)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-2.368e-051.670e-04-3.92 +/- 0.01-0.06 +/- 1.00No Violation Check
ai1ax2xon-0.0020.105-0.93 +/- 1.60(1.93+/-1.93)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off1.333e-051.841e-04-3.89 +/- 0.020.69 +/- 1.08No Violation Check
ai1ax2yon0.0040.105-0.94 +/- 1.61(1.94+/-1.94)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-2.286e-051.799e-04-3.92 +/- 0.02-0.53 +/- 1.01No Violation Check
ai2ax1xon-4.242e-051.712e-04-0.00 +/- 0.02-0.33 +/- 1.82DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4310.063-1.51 +/- 1.79-62.92 +/- 93.73No Violation Check
ai2ax1yon4.099e-051.072e-04-0.00 +/- 0.010.46 +/- 0.94DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5240.066-1.55 +/- 1.86-69.43 +/- 96.95No Violation Check
ai2ax2xon3.032e-051.758e-04-0.00 +/- 0.02-0.36 +/- 1.87DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.4980.065-1.53 +/- 1.84-62.83 +/- 95.68No Violation Check
ai2ax2yon-5.034e-058.280e-05-0.00 +/- 0.010.15 +/- 0.68DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5150.066-1.54 +/- 1.85-68.07 +/- 96.66No Violation Check
aoalpang 1.3790.257-14.77 +/- 23.86(2.66+/-25.70)e2DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 -0.0630.006-0.12 +/- 0.55-48.29 +/- 26.86naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0050.0030.26 +/- 0.29-9.78 +/- 23.82naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0570.0050.03 +/- 0.5024.39 +/- 28.07naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0340.0030.47 +/- 0.24-6.25 +/- 15.65naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -0.5380.380-9.83 +/- 35.11(4.64+/-38.41)e2DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 -0.0630.006-0.12 +/- 0.55-48.31 +/- 26.86naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0050.0030.26 +/- 0.29-9.82 +/- 23.82naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0570.0050.03 +/- 0.5024.42 +/- 28.07naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -198.636257.943-(9.44+/-23.34)e3-(1.71+/-0.40)e6KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 3.698e+03469.013-(6.88+/-4.31)e4(3.76+/-7.29)e5KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -2.039e+03410.603(5.69+/-3.74)e4(2.16+/-0.66)e6KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0620.010-0.03 +/- 0.9414.82 +/- 30.69KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.0180.0170.14 +/- 1.56-47.96 +/- 36.93KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.0790.016-0.04 +/- 1.423.87 +/- 34.16KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 0.0073.239e-05-0.92 +/- 0.010.01 +/- 0.06naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0153.170e-05-0.37 +/- 0.030.23 +/- 0.17naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0063.076e-05-0.16 +/- 0.010.02 +/- 0.04naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 3.454e-041.138e-04-0.01 +/- 0.010.79 +/- 0.93naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 4.964e-042.982e-040.01 +/- 0.03-1.12 +/- 1.66naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 5.154e-051.799e-05-1.00 +/- 0.00-0.03 +/- 0.03naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 -0.0610.006-0.12 +/- 0.55-43.55 +/- 27.30naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0050.0030.26 +/- 0.29-4.73 +/- 24.27naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0570.0050.03 +/- 0.5025.35 +/- 28.74naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Oct 22, 2026
Last Site Modification: Sep 30, 2021