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) :             26/083 06:00:00.000
Semimajor Axis (km) :                         42212.00560
Eccentricity :                                0.000182
Inclination (deg) :                           1.464239
Right Ascension of Ascending Node (deg) :     84.813869
Argument of Perigee (deg) :                   278.914598
Mean Anomaly (deg) :                          97.820063
Apogee Ht (km):                               35841.55135
Perigee Ht (km):                              35826.17985

West Longitude (deg) :                        170.168
Longitude Drift Rate (deg/day) :              0.591000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 26/078 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/071.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3264.28441
Fuel Mass (kg) :                              365.789236
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/083 05:00:00.000
Semimajor Axis (km):                          42165.0445
Eccentricity :                                0.00023572
Inclination (deg) :                           0.14060445
Right Ascension of Ascending Node (deg) :     93.7591469
Argument of Perigee (deg) :                   218.386365
Mean Anomaly (deg) :                          199.854072
Apogee Ht (km) :                              35796.8398
Perigee Ht (km) :                             35776.9612

West Longitude (deg) :                        104.692024
Longitude Drift Rate (deg/day) :              0.00203931 EAST

Comments:
GOES-16 data propagated from orbit epoch 26/083 05:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/083.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3457.30688
Fuel Mass (kg) :                              535.419991
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/083 12:00:00.000
Semimajor Axis (km):                          42165.8949
Eccentricity :                                0.00018794
Inclination (deg) :                           0.71511415
Right Ascension of Ascending Node (deg) :     88.5296261
Argument of Perigee (deg) :                   214.529901
Mean Anomaly (deg) :                          329.422199
Apogee Ht (km) :                              35795.6756
Perigee Ht (km) :                             35779.8262

West Longitude (deg) :                        89.4955994
Longitude Drift Rate (deg/day) :              0.00202173 EAST

Comments:
GOES-17 data propagated from orbit epoch 26/083 12:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/082.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3654.24905
Fuel Mass (kg) :                              720.409752
Oxidizer Mass (kg) :                          34.2392986

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/083 11:00:00.000
Semimajor Axis (km):                          42166.3388
Eccentricity :                                0.00002634
Inclination (deg) :                           0.01468789
Right Ascension of Ascending Node (deg) :     93.7249750
Argument of Perigee (deg) :                   162.083447
Mean Anomaly (deg) :                          314.128401
Apogee Ht (km) :                              35789.3054
Perigee Ht (km) :                             35787.0841

West Longitude (deg) :                        137.001897
Longitude Drift Rate (deg/day) :              0.00142875 WEST

Comments:
GOES-18 data propagated from orbit epoch 26/083 11:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/083.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3863.03323
Fuel Mass (kg) :                              902.948747
Oxidizer Mass (kg) :                          29.4844801

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             26/083 13:00:00.000
Semimajor Axis (km):                          42165.5673
Eccentricity :                                0.00005440
Inclination (deg) :                           0.00268828
Right Ascension of Ascending Node (deg) :     8.78033097
Argument of Perigee (deg) :                   355.393802
Mean Anomaly (deg) :                          297.651782
Apogee Ht (km) :                              35789.7172
Perigee Ht (km) :                             35785.1294

West Longitude (deg) :                        75.1925064
Longitude Drift Rate (deg/day) :              0.00061511 EAST

Comments:
GOES-19 data propagated from orbit epoch 26/083 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 26/083.
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