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) :             25/117 06:00:00.000
Semimajor Axis (km) :                         42167.40137
Eccentricity :                                0.000125
Inclination (deg) :                           0.578690
Right Ascension of Ascending Node (deg) :     89.444252
Argument of Perigee (deg) :                   97.576967
Mean Anomaly (deg) :                          10.094909
Apogee Ht (km):                               35794.52506
Perigee Ht (km):                              35783.99769

West Longitude (deg) :                        108.362
Longitude Drift Rate (deg/day) :              0.005000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 25/113 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) :                               3304.78666
Fuel Mass (kg) :                              406.291490
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/119 10:00:00.000
Semimajor Axis (km):                          42205.6345
Eccentricity :                                0.00006674
Inclination (deg) :                           0.08046986
Right Ascension of Ascending Node (deg) :     271.098169
Argument of Perigee (deg) :                   246.995899
Mean Anomaly (deg) :                          124.700548
Apogee Ht (km) :                              35830.3075
Perigee Ht (km) :                             35824.6735

West Longitude (deg) :                        84.8198784
Longitude Drift Rate (deg/day) :              0.51297490 WEST

Comments:
GOES-16 data propagated from orbit epoch 25/119 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/118.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3472.32150
Fuel Mass (kg) :                              550.434610
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/119 12:00:00.000
Semimajor Axis (km):                          42165.4503
Eccentricity :                                0.00019189
Inclination (deg) :                           0.02311300
Right Ascension of Ascending Node (deg) :     273.579614
Argument of Perigee (deg) :                   188.046023
Mean Anomaly (deg) :                          191.696169
Apogee Ht (km) :                              35795.3975
Perigee Ht (km) :                             35779.2150

West Longitude (deg) :                        104.374247
Longitude Drift Rate (deg/day) :              0.00208103 WEST

Comments:
GOES-17 data propagated from orbit epoch 25/119 12:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/119.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3696.68947
Fuel Mass (kg) :                              762.820612
Oxidizer Mass (kg) :                          34.2688602

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/119 10:00:00.000
Semimajor Axis (km):                          42167.2272
Eccentricity :                                0.00008396
Inclination (deg) :                           0.00417380
Right Ascension of Ascending Node (deg) :     10.9835486
Argument of Perigee (deg) :                   225.130543
Mean Anomaly (deg) :                          354.496069
Apogee Ht (km) :                              35792.6234
Perigee Ht (km) :                             35785.5430

West Longitude (deg) :                        137.006788
Longitude Drift Rate (deg/day) :              0.00152863 WEST

Comments:
GOES-18 data propagated from orbit epoch 25/119 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/118.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3908.85968
Fuel Mass (kg) :                              948.760687
Oxidizer Mass (kg) :                          29.4989954

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/119 13:00:00.000
Semimajor Axis (km):                          42164.2356
Eccentricity :                                0.00002102
Inclination (deg) :                           0.01334043
Right Ascension of Ascending Node (deg) :     82.3881558
Argument of Perigee (deg) :                   7.62396566
Mean Anomaly (deg) :                          247.532777
Apogee Ht (km) :                              35786.9778
Perigee Ht (km) :                             35785.2055

West Longitude (deg) :                        75.1963235
Longitude Drift Rate (deg/day) :              0.00520491 EAST

Comments:
GOES-19 data propagated from orbit epoch 25/119 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/119.
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