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

S/C Mass (kg) :                               1627.785
Fuel Mass (kg) :                               30.643
Oxidizer Mass (kg) :                           46.231

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/357 06:00:00.000
Semimajor Axis (km) :                         42214.64554
Eccentricity :                                0.000027
Inclination (deg) :                           1.235285
Right Ascension of Ascending Node (deg) :     84.220949
Argument of Perigee (deg) :                   141.140825
Mean Anomaly (deg) :                          200.299548
Apogee Ht (km):                               35837.64023
Perigee Ht (km):                              35835.37085

West Longitude (deg) :                        116.374
Longitude Drift Rate (deg/day) :              0.628000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 25/352 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/351.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3274.12642
Fuel Mass (kg) :                              375.631250
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/357 13:00:00.000
Semimajor Axis (km):                          42165.2155
Eccentricity :                                0.00027867
Inclination (deg) :                           0.07129469
Right Ascension of Ascending Node (deg) :     83.4162384
Argument of Perigee (deg) :                   181.207168
Mean Anomaly (deg) :                          278.036522
Apogee Ht (km) :                              35798.8218
Perigee Ht (km) :                             35775.3213

West Longitude (deg) :                        104.663633
Longitude Drift Rate (deg/day) :              0.00225192 EAST

Comments:
GOES-16 data propagated from orbit epoch 25/357 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/357.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3457.71132
Fuel Mass (kg) :                              535.824422
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/357 12:00:00.000
Semimajor Axis (km):                          42165.0715
Eccentricity :                                0.00026732
Inclination (deg) :                           0.48800196
Right Ascension of Ascending Node (deg) :     86.3692471
Argument of Perigee (deg) :                   192.636743
Mean Anomaly (deg) :                          263.774513
Apogee Ht (km) :                              35798.1989
Perigee Ht (km) :                             35775.6562

West Longitude (deg) :                        89.5020000
Longitude Drift Rate (deg/day) :              0.00404966 EAST

Comments:
GOES-17 data propagated from orbit epoch 25/357 12:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/356.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3665.85272
Fuel Mass (kg) :                              731.998695
Oxidizer Mass (kg) :                          34.2540284

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/357 06:00:00.000
Semimajor Axis (km):                          42165.2425
Eccentricity :                                0.00001541
Inclination (deg) :                           0.00696544
Right Ascension of Ascending Node (deg) :     63.2478263
Argument of Perigee (deg) :                   290.793162
Mean Anomaly (deg) :                          50.9996371
Apogee Ht (km) :                              35787.7481
Perigee Ht (km) :                             35786.4489

West Longitude (deg) :                        136.998939
Longitude Drift Rate (deg/day) :              0.00214424 WEST

Comments:
GOES-18 data propagated from orbit epoch 25/357 06:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/356.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3874.82398
Fuel Mass (kg) :                              914.739504
Oxidizer Mass (kg) :                          29.4844801

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/357 13:00:00.000
Semimajor Axis (km):                          42164.8108
Eccentricity :                                0.00010099
Inclination (deg) :                           0.00302946
Right Ascension of Ascending Node (deg) :     329.547735
Argument of Perigee (deg) :                   4.68104450
Mean Anomaly (deg) :                          237.914350
Apogee Ht (km) :                              35790.9251
Perigee Ht (km) :                             35782.4084

West Longitude (deg) :                        75.1823989
Longitude Drift Rate (deg/day) :              0.00164921 EAST

Comments:
GOES-19 data propagated from orbit epoch 25/357 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/357.
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