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

S/C Mass (kg) :                               1627.597
Fuel Mass (kg) :                               30.573
Oxidizer Mass (kg) :                           46.113

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/041 06:00:00.000
Semimajor Axis (km) :                         42210.18425
Eccentricity :                                0.000192
Inclination (deg) :                           1.378447
Right Ascension of Ascending Node (deg) :     84.936250
Argument of Perigee (deg) :                   300.313067
Mean Anomaly (deg) :                          59.094652
Apogee Ht (km):                               35840.14710
Perigee Ht (km):                              35823.94140

West Longitude (deg) :                        145.972
Longitude Drift Rate (deg/day) :              0.565000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 26/039 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/039.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3271.59770
Fuel Mass (kg) :                              373.102525
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/036 13:00:00.000
Semimajor Axis (km):                          42165.3148
Eccentricity :                                0.00025864
Inclination (deg) :                           0.16776983
Right Ascension of Ascending Node (deg) :     95.2674629
Argument of Perigee (deg) :                   193.984030
Mean Anomaly (deg) :                          296.739320
Apogee Ht (km) :                              35798.0765
Perigee Ht (km) :                             35776.2651

West Longitude (deg) :                        104.700781
Longitude Drift Rate (deg/day) :              0.00341627 WEST

Comments:
GOES-16 data propagated from orbit epoch 26/036 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/036.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3457.46021
Fuel Mass (kg) :                              535.573319
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/041 12:00:00.000
Semimajor Axis (km):                          42165.3984
Eccentricity :                                0.00025447
Inclination (deg) :                           0.62844020
Right Ascension of Ascending Node (deg) :     88.2844410
Argument of Perigee (deg) :                   201.906323
Mean Anomaly (deg) :                          300.869269
Apogee Ht (km) :                              35797.9844
Perigee Ht (km) :                             35776.5245

West Longitude (deg) :                        89.5219073
Longitude Drift Rate (deg/day) :              0.00973434 EAST

Comments:
GOES-17 data propagated from orbit epoch 26/041 12:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/040.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3658.84439
Fuel Mass (kg) :                              725.005091
Oxidizer Mass (kg) :                          34.2392986

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/041 11:00:00.000
Semimajor Axis (km):                          42165.7142
Eccentricity :                                0.00005694
Inclination (deg) :                           0.01436943
Right Ascension of Ascending Node (deg) :     96.2226022
Argument of Perigee (deg) :                   305.733673
Mean Anomaly (deg) :                          126.583654
Apogee Ht (km) :                              35789.9709
Perigee Ht (km) :                             35785.1695

West Longitude (deg) :                        137.000848
Longitude Drift Rate (deg/day) :              0.00116840 WEST

Comments:
GOES-18 data propagated from orbit epoch 26/041 11:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/041.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3867.45606
Fuel Mass (kg) :                              907.371585
Oxidizer Mass (kg) :                          29.4844801

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/041 13:00:00.000
Semimajor Axis (km):                          42165.9988
Eccentricity :                                0.00009477
Inclination (deg) :                           0.00595188
Right Ascension of Ascending Node (deg) :     315.299994
Argument of Perigee (deg) :                   34.2221588
Mean Anomaly (deg) :                          270.911565
Apogee Ht (km) :                              35791.8510
Perigee Ht (km) :                             35783.8586

West Longitude (deg) :                        75.1885174
Longitude Drift Rate (deg/day) :              0.00236526 EAST

Comments:
GOES-19 data propagated from orbit epoch 26/041 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/041.
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