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

S/C Mass (kg) :                               1629.275
Fuel Mass (kg) :                               31.202
Oxidizer Mass (kg) :                           47.161

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/308 06:00:00.000
Semimajor Axis (km) :                         42167.48613
Eccentricity :                                0.000337
Inclination (deg) :                           1.069627
Right Ascension of Ascending Node (deg) :     86.063970
Argument of Perigee (deg) :                   138.415795
Mean Anomaly (deg) :                          160.797406
Apogee Ht (km):                               35803.56467
Perigee Ht (km):                              35775.12760

West Longitude (deg) :                        108.447
Longitude Drift Rate (deg/day) :              0.000000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 25/302 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/212.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3281.17845
Fuel Mass (kg) :                              382.683275
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/308 13:00:00.000
Semimajor Axis (km):                          42164.3618
Eccentricity :                                0.00035857
Inclination (deg) :                           0.04928335
Right Ascension of Ascending Node (deg) :     80.0399408
Argument of Perigee (deg) :                   164.887675
Mean Anomaly (deg) :                          249.415600
Apogee Ht (km) :                              35801.3366
Perigee Ht (km) :                             35771.0990

West Longitude (deg) :                        104.686859
Longitude Drift Rate (deg/day) :              0.00015134 EAST

Comments:
GOES-16 data propagated from orbit epoch 25/308 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/307.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3458.23249
Fuel Mass (kg) :                              536.345600
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/308 12:00:00.000
Semimajor Axis (km):                          42164.2022
Eccentricity :                                0.00036799
Inclination (deg) :                           0.33125992
Right Ascension of Ascending Node (deg) :     91.0826725
Argument of Perigee (deg) :                   168.239777
Mean Anomaly (deg) :                          235.157360
Apogee Ht (km) :                              35801.5743
Perigee Ht (km) :                             35770.5422

West Longitude (deg) :                        89.5092652
Longitude Drift Rate (deg/day) :              0.00269685 EAST

Comments:
GOES-17 data propagated from orbit epoch 25/308 12:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/307.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3674.11198
Fuel Mass (kg) :                              740.257948
Oxidizer Mass (kg) :                          34.2540284

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/308 06:00:00.000
Semimajor Axis (km):                          42166.7951
Eccentricity :                                0.00007520
Inclination (deg) :                           0.01747240
Right Ascension of Ascending Node (deg) :     101.066117
Argument of Perigee (deg) :                   227.934837
Mean Anomaly (deg) :                          27.7317837
Apogee Ht (km) :                              35791.8219
Perigee Ht (km) :                             35785.4802

West Longitude (deg) :                        137.011643
Longitude Drift Rate (deg/day) :              0.00475782 WEST

Comments:
GOES-18 data propagated from orbit epoch 25/308 06:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/307.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3882.62738
Fuel Mass (kg) :                              922.528385
Oxidizer Mass (kg) :                          29.4989954

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/308 13:00:00.000
Semimajor Axis (km):                          42166.1538
Eccentricity :                                0.00017185
Inclination (deg) :                           0.00634284
Right Ascension of Ascending Node (deg) :     234.762724
Argument of Perigee (deg) :                   28.6587907
Mean Anomaly (deg) :                          260.417300
Apogee Ht (km) :                              35795.2562
Perigee Ht (km) :                             35780.7633

West Longitude (deg) :                        75.1929758
Longitude Drift Rate (deg/day) :              0.00581974 WEST

Comments:
GOES-19 data propagated from orbit epoch 25/308 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/308.
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