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

S/C Mass (kg) :                               1627.208
Fuel Mass (kg) :                               30.428
Oxidizer Mass (kg) :                           45.869

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/124 06:00:00.000
Semimajor Axis (km) :                         42208.66238
Eccentricity :                                0.000230
Inclination (deg) :                           1.554861
Right Ascension of Ascending Node (deg) :     83.342753
Argument of Perigee (deg) :                   330.756364
Mean Anomaly (deg) :                          64.483503
Apogee Ht (km):                               35840.24270
Perigee Ht (km):                              35820.80206

West Longitude (deg) :                        -166.453
Longitude Drift Rate (deg/day) :              0.553000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 26/118 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 23/313.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3262.84253
Fuel Mass (kg) :                              364.347357
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/125 05:00:00.000
Semimajor Axis (km):                          42165.3051
Eccentricity :                                0.00010945
Inclination (deg) :                           0.21084669
Right Ascension of Ascending Node (deg) :     84.5039154
Argument of Perigee (deg) :                   260.278597
Mean Anomaly (deg) :                          208.588131
Apogee Ht (km) :                              35791.7761
Perigee Ht (km) :                             35782.5461

West Longitude (deg) :                        104.719328
Longitude Drift Rate (deg/day) :              0.00451524 EAST

Comments:
GOES-16 data propagated from orbit epoch 26/125 05:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/124.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3457.13395
Fuel Mass (kg) :                              535.247062
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/125 12:00:00.000
Semimajor Axis (km):                          42165.2964
Eccentricity :                                0.00005495
Inclination (deg) :                           0.80796647
Right Ascension of Ascending Node (deg) :     85.9618640
Argument of Perigee (deg) :                   305.207642
Mean Anomaly (deg) :                          282.711828
Apogee Ht (km) :                              35789.4695
Perigee Ht (km) :                             35784.8353

West Longitude (deg) :                        89.4925020
Longitude Drift Rate (deg/day) :              0.00184660 EAST

Comments:
GOES-17 data propagated from orbit epoch 26/125 12:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/124.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3649.61800
Fuel Mass (kg) :                              715.778702
Oxidizer Mass (kg) :                          34.2392986

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/125 11:00:00.000
Semimajor Axis (km):                          42167.0284
Eccentricity :                                0.00002776
Inclination (deg) :                           0.01663243
Right Ascension of Ascending Node (deg) :     38.7210322
Argument of Perigee (deg) :                   145.622781
Mean Anomaly (deg) :                          66.9943456
Apogee Ht (km) :                              35790.0551
Perigee Ht (km) :                             35787.7137

West Longitude (deg) :                        136.996327
Longitude Drift Rate (deg/day) :              0.00239106 WEST

Comments:
GOES-18 data propagated from orbit epoch 26/125 11:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/124.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3857.94959
Fuel Mass (kg) :                              897.865108
Oxidizer Mass (kg) :                          29.4844801

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/125 13:00:00.000
Semimajor Axis (km):                          42164.9603
Eccentricity :                                0.00008951
Inclination (deg) :                           0.00376879
Right Ascension of Ascending Node (deg) :     305.977485
Argument of Perigee (deg) :                   152.899657
Mean Anomaly (deg) :                          244.350523
Apogee Ht (km) :                              35790.5906
Perigee Ht (km) :                             35783.0420

West Longitude (deg) :                        75.1891555
Longitude Drift Rate (deg/day) :              0.00225050 EAST

Comments:
GOES-19 data propagated from orbit epoch 26/125 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/125.
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