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

S/C Mass (kg) :                               1776.816
Fuel Mass (kg) :                               86.249
Oxidizer Mass (kg) :                          139.655

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             21/056 06:00:00.000
Semimajor Axis (km) :                         42167.37707
Eccentricity :                                0.001111
Inclination (deg) :                           0.083322
Right Ascension of Ascending Node (deg) :     157.292078
Argument of Perigee (deg) :                   66.746458
Mean Anomaly (deg) :                          276.992025
Apogee Ht (km):                               35836.08966
Perigee Ht (km):                              35742.38449

West Longitude (deg) :                        104.417
Longitude Drift Rate (deg/day) :              0.002000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 21/043 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 20/233.
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Spacecraft :                                  GOES-15

S/C Mass (kg) :                               1821.981
Fuel Mass (kg) :                               97.682
Oxidizer Mass (kg) :                          165.117

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             21/056 06:00:00.000
Semimajor Axis (km) :                         42168.49381
Eccentricity :                                0.000323
Inclination (deg) :                           0.177135
Right Ascension of Ascending Node (deg) :     249.747702
Argument of Perigee (deg) :                   142.477736
Mean Anomaly (deg) :                          84.950689
Apogee Ht (km):                               35803.95935
Perigee Ht (km):                              35776.74826

West Longitude (deg) :                        128.108
Longitude Drift Rate (deg/day) :              0.023000 WEST

Comments:
GOES-15 data propagated from OATS orbit epoch 21/050 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 21/049.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3563.74751
Fuel Mass (kg) :                              658.402342
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             21/056 08:00:00.000
Semimajor Axis (km):                          42164.9370
Eccentricity :                                0.00014516
Inclination (deg) :                           0.02197482
Right Ascension of Ascending Node (deg) :     272.360448
Argument of Perigee (deg) :                   90.8903629
Mean Anomaly (deg) :                          196.958545
Apogee Ht (km) :                              35792.9209
Perigee Ht (km) :                             35780.6791

West Longitude (deg) :                        75.2034060
Longitude Drift Rate (deg/day) :              0.00294131 EAST

Comments:
GOES-16 data propagated from orbit epoch 21/056 08:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 21/056.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3668.86926
Fuel Mass (kg) :                              746.982368
Oxidizer Mass (kg) :                          29.1868926

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             21/056 09:00:00.000
Semimajor Axis (km):                          42166.8899
Eccentricity :                                3.3900e-05
Inclination (deg) :                           0.04412106
Right Ascension of Ascending Node (deg) :     265.995182
Argument of Perigee (deg) :                   176.269385
Mean Anomaly (deg) :                          70.9806629
Apogee Ht (km) :                              35790.1824
Perigee Ht (km) :                             35787.3234

West Longitude (deg) :                        137.200084
Longitude Drift Rate (deg/day) :              0.00314485 EAST

Comments:
GOES-17 data propagated from orbit epoch 21/056 09:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 21/055.
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