Below are the weekly GOES element sets:
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Spacecraft :                                  GOES-14

S/C Mass (kg) :                               1629.470
Fuel Mass (kg) :                               31.275
Oxidizer Mass (kg) :                           47.284

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/175 06:00:00.000
Semimajor Axis (km) :                         42166.53277
Eccentricity :                                0.000219
Inclination (deg) :                           0.755162
Right Ascension of Ascending Node (deg) :     85.795605
Argument of Perigee (deg) :                   93.166535
Mean Anomaly (deg) :                          75.453586
Apogee Ht (km):                               35797.63170
Perigee Ht (km):                              35779.15385

West Longitude (deg) :                        108.208
Longitude Drift Rate (deg/day) :              0.008000 EAST

Comments:
GOES-14 data propagated from OATS orbit epoch 25/169 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/044.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3293.81533
Fuel Mass (kg) :                              395.320164
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/175 10:00:00.000
Semimajor Axis (km):                          42165.3937
Eccentricity :                                0.00007658
Inclination (deg) :                           0.05047421
Right Ascension of Ascending Node (deg) :     278.597566
Argument of Perigee (deg) :                   272.830267
Mean Anomaly (deg) :                          126.653528
Apogee Ht (km) :                              35790.4788
Perigee Ht (km) :                             35784.0206

West Longitude (deg) :                        104.729362
Longitude Drift Rate (deg/day) :              0.00239385 EAST

Comments:
GOES-16 data propagated from orbit epoch 25/175 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/174.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3463.04692
Fuel Mass (kg) :                              541.160026
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/175 12:00:00.000
Semimajor Axis (km):                          42122.2934
Eccentricity :                                0.00010797
Inclination (deg) :                           0.02408961
Right Ascension of Ascending Node (deg) :     75.1842629
Argument of Perigee (deg) :                   140.664180
Mean Anomaly (deg) :                          138.350355
Apogee Ht (km) :                              35748.6973
Perigee Ht (km) :                             35739.6016

West Longitude (deg) :                        98.6959791
Longitude Drift Rate (deg/day) :              0.54528681 EAST

Comments:
GOES-17 data propagated from orbit epoch 25/175 12:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/175.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3689.50704
Fuel Mass (kg) :                              755.653013
Oxidizer Mass (kg) :                          34.2540284

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/175 10:00:00.000
Semimajor Axis (km):                          42166.9879
Eccentricity :                                0.00009707
Inclination (deg) :                           0.01683655
Right Ascension of Ascending Node (deg) :     64.6033278
Argument of Perigee (deg) :                   184.651107
Mean Anomaly (deg) :                          36.5532663
Apogee Ht (km) :                              35792.9370
Perigee Ht (km) :                             35784.7509

West Longitude (deg) :                        137.003797
Longitude Drift Rate (deg/day) :              0.00225785 WEST

Comments:
GOES-18 data propagated from orbit epoch 25/175 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/174.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3900.00903
Fuel Mass (kg) :                              939.910034
Oxidizer Mass (kg) :                          29.4989954

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/175 13:00:00.000
Semimajor Axis (km):                          42165.4861
Eccentricity :                                0.00003300
Inclination (deg) :                           0.01329501
Right Ascension of Ascending Node (deg) :     61.8395054
Argument of Perigee (deg) :                   82.8808657
Mean Anomaly (deg) :                          248.023065
Apogee Ht (km) :                              35788.7337
Perigee Ht (km) :                             35785.9506

West Longitude (deg) :                        75.1965763
Longitude Drift Rate (deg/day) :              0.00196896 EAST

Comments:
GOES-19 data propagated from orbit epoch 25/175 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/175.
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