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

S/C Mass (kg) :                               1629.470
Fuel Mass (kg) :                               31.275
Oxidizer Mass (kg) :                           47.284

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/113 06:00:00.000
Semimajor Axis (km) :                         42166.61807
Eccentricity :                                0.000122
Inclination (deg) :                           0.575515
Right Ascension of Ascending Node (deg) :     89.858770
Argument of Perigee (deg) :                   49.974999
Mean Anomaly (deg) :                          53.359581
Apogee Ht (km):                               35793.63690
Perigee Ht (km):                              35783.31924

West Longitude (deg) :                        108.333
Longitude Drift Rate (deg/day) :              0.007000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 25/108 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/044.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3305.69063
Fuel Mass (kg) :                              407.195463
Oxidizer Mass (kg) :                          34.9351702

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/112 10:00:00.000
Semimajor Axis (km):                          42205.0343
Eccentricity :                                0.00008983
Inclination (deg) :                           0.07482546
Right Ascension of Ascending Node (deg) :     268.429639
Argument of Perigee (deg) :                   174.694545
Mean Anomaly (deg) :                          196.362506
Apogee Ht (km) :                              35830.6817
Perigee Ht (km) :                             35823.0989

West Longitude (deg) :                        81.2334488
Longitude Drift Rate (deg/day) :              0.50872422 WEST

Comments:
GOES-16 data propagated from orbit epoch 25/112 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/111.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3473.18732
Fuel Mass (kg) :                              551.300427
Oxidizer Mass (kg) :                          29.1868927

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/112 10:00:00.000
Semimajor Axis (km):                          42164.9220
Eccentricity :                                0.00026003
Inclination (deg) :                           0.01527635
Right Ascension of Ascending Node (deg) :     278.631282
Argument of Perigee (deg) :                   167.590511
Mean Anomaly (deg) :                          170.128140
Apogee Ht (km) :                              35797.7423
Perigee Ht (km) :                             35775.8137

West Longitude (deg) :                        104.368172
Longitude Drift Rate (deg/day) :              0.00084496 EAST

Comments:
GOES-17 data propagated from orbit epoch 25/112 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/111.
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Spacecraft :                                  GOES-18

S/C Mass (kg) :                               3697.43370
Fuel Mass (kg) :                              763.564842
Oxidizer Mass (kg) :                          34.2688602

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/112 10:00:00.000
Semimajor Axis (km):                          42165.6000
Eccentricity :                                0.00004785
Inclination (deg) :                           0.00499968
Right Ascension of Ascending Node (deg) :     99.4136276
Argument of Perigee (deg) :                   10.2295755
Mean Anomaly (deg) :                          114.086398
Apogee Ht (km) :                              35789.4734
Perigee Ht (km) :                             35785.4385

West Longitude (deg) :                        136.986513
Longitude Drift Rate (deg/day) :              0.00442810 WEST

Comments:
GOES-18 data propagated from orbit epoch 25/112 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/112.
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Spacecraft :                                  GOES-19

S/C Mass (kg) :                               3909.72057
Fuel Mass (kg) :                              949.621571
Oxidizer Mass (kg) :                          29.4989954

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             25/112 13:00:00.000
Semimajor Axis (km):                          42166.9134
Eccentricity :                                0.00009822
Inclination (deg) :                           0.01632730
Right Ascension of Ascending Node (deg) :     102.788752
Argument of Perigee (deg) :                   270.549973
Mean Anomaly (deg) :                          317.329495
Apogee Ht (km) :                              35792.9111
Perigee Ht (km) :                             35784.6276

West Longitude (deg) :                        75.1726191
Longitude Drift Rate (deg/day) :              0.00494757 WEST

Comments:
GOES-19 data propagated from orbit epoch 25/112 13:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 25/112.
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