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) :             26/063 06:00:00.000
Semimajor Axis (km) :                         42205.80216
Eccentricity :                                0.000196
Inclination (deg) :                           1.428546
Right Ascension of Ascending Node (deg) :     85.442897
Argument of Perigee (deg) :                   290.760338
Mean Anomaly (deg) :                          77.743945
Apogee Ht (km):                               35835.92070
Perigee Ht (km):                              35819.40363

West Longitude (deg) :                        158.053
Longitude Drift Rate (deg/day) :              0.532000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 26/062 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) :                               3265.73719
Fuel Mass (kg) :                              367.242018
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/069 13:00:00.000
Semimajor Axis (km):                          42165.9399
Eccentricity :                                0.00023647
Inclination (deg) :                           0.13455389
Right Ascension of Ascending Node (deg) :     94.9601532
Argument of Perigee (deg) :                   211.496615
Mean Anomaly (deg) :                          312.069278
Apogee Ht (km) :                              35797.7670
Perigee Ht (km) :                             35777.8249

West Longitude (deg) :                        104.693819
Longitude Drift Rate (deg/day) :              0.00195314 EAST

Comments:
GOES-16 data propagated from orbit epoch 26/069 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/069.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3457.37144
Fuel Mass (kg) :                              535.484552
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/069 12:00:00.000
Semimajor Axis (km):                          42165.6557
Eccentricity :                                0.00017984
Inclination (deg) :                           0.68805774
Right Ascension of Ascending Node (deg) :     88.8958474
Argument of Perigee (deg) :                   218.327582
Mean Anomaly (deg) :                          311.436021
Apogee Ht (km) :                              35795.0949
Perigee Ht (km) :                             35779.9284

West Longitude (deg) :                        89.5193384
Longitude Drift Rate (deg/day) :              0.00563203 EAST

Comments:
GOES-17 data propagated from orbit epoch 26/069 12:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/068.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3655.93489
Fuel Mass (kg) :                              722.095588
Oxidizer Mass (kg) :                          34.2392986

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/069 11:00:00.000
Semimajor Axis (km):                          42166.0676
Eccentricity :                                0.00004523
Inclination (deg) :                           0.02174345
Right Ascension of Ascending Node (deg) :     93.2902763
Argument of Perigee (deg) :                   343.548331
Mean Anomaly (deg) :                          119.294210
Apogee Ht (km) :                              35789.8309
Perigee Ht (km) :                             35786.0163

West Longitude (deg) :                        137.006588
Longitude Drift Rate (deg/day) :              0.00070245 WEST

Comments:
GOES-18 data propagated from orbit epoch 26/069 11:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/069.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3864.35736
Fuel Mass (kg) :                              904.272881
Oxidizer Mass (kg) :                          29.4844801

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/069 13:00:00.000
Semimajor Axis (km):                          42165.3790
Eccentricity :                                0.00008765
Inclination (deg) :                           0.00314230
Right Ascension of Ascending Node (deg) :     313.550967
Argument of Perigee (deg) :                   74.5697941
Mean Anomaly (deg) :                          259.914611
Apogee Ht (km) :                              35790.9308
Perigee Ht (km) :                             35783.5392

West Longitude (deg) :                        75.1844357
Longitude Drift Rate (deg/day) :              0.00428705 EAST

Comments:
GOES-19 data propagated from orbit epoch 26/069 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/068.
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