Below are the weekly GOES element sets:
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Spacecraft :                                  GOES-13

S/C Mass (kg) :                               1701.583
Fuel Mass (kg) :                               52.481
Oxidizer Mass (kg) :                           99.692

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             19/109 06:00:00.000
Semimajor Axis (km) :                         42169.20493
Eccentricity :                                0.001259
Inclination (deg) :                           0.353956
Right Ascension of Ascending Node (deg) :     280.365546
Argument of Perigee (deg) :                   145.823555
Mean Anomaly (deg) :                          170.617229
Apogee Ht (km):                               35844.14929
Perigee Ht (km):                              35737.98058

West Longitude (deg) :                        60.222
Longitude Drift Rate (deg/day) :              0.037000 WEST

Comments:
GOES-13 data propagated from OATS orbit epoch 19/103 03:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 19/055.
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Spacecraft :                                  GOES-14

S/C Mass (kg) :                               1851.739
Fuel Mass (kg) :                              114.081
Oxidizer Mass (kg) :                          186.748

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             19/109 06:00:00.000
Semimajor Axis (km) :                         42167.51022
Eccentricity :                                0.000756
Inclination (deg) :                           0.138102
Right Ascension of Ascending Node (deg) :     113.246892
Argument of Perigee (deg) :                   119.750556
Mean Anomaly (deg) :                          319.671265
Apogee Ht (km):                               35821.24284
Perigee Ht (km):                              35757.49760

West Longitude (deg) :                        104.439
Longitude Drift Rate (deg/day) :              0.002000 WEST

Comments:
GOES-14 data propagated from OATS orbit epoch 19/103 03:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 19/108.
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Spacecraft :                                  GOES-15

S/C Mass (kg) :                               1900.829
Fuel Mass (kg) :                              127.004
Oxidizer Mass (kg) :                          214.642

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             19/109 06:00:00.000
Semimajor Axis (km) :                         42169.24546
Eccentricity :                                0.000075
Inclination (deg) :                           0.069310
Right Ascension of Ascending Node (deg) :     116.750394
Argument of Perigee (deg) :                   295.771817
Mean Anomaly (deg) :                          116.847384
Apogee Ht (km):                               35794.24771
Perigee Ht (km):                              35787.96322

West Longitude (deg) :                        127.675
Longitude Drift Rate (deg/day) :              0.039000 WEST

Comments:
GOES-15 data propagated from OATS orbit epoch 19/109 00:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 19/108.
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Spacecraft :                                  GOES-16

S/C Mass (kg) :                               3663.92926
Fuel Mass (kg) :                              758.551341
Oxidizer Mass (kg) :                          34.9679259

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             19/108 10:00:00.000
Semimajor Axis (km):                          42164.0195
Eccentricity :                                0.00012494
Inclination (deg) :                           0.00510851
Right Ascension of Ascending Node (deg) :     230.448447
Argument of Perigee (deg) :                   204.182547
Mean Anomaly (deg) :                          206.406075
Apogee Ht (km) :                              35791.1506
Perigee Ht (km) :                             35780.6144

West Longitude (deg) :                        75.2047816
Longitude Drift Rate (deg/day) :              0.00201355 EAST

Comments:
GOES-16 data propagated from orbit epoch 19/108 10:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 19/107.
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Spacecraft :                                  GOES-17

S/C Mass (kg) :                               3759.44011
Fuel Mass (kg) :                              837.519472
Oxidizer Mass (kg) :                          29.2206449

Coordinate System :                           True of Date

Epoch (yy/ddd hh:mm:ss.sss GMT) :             19/108 09:00:00.000
Semimajor Axis (km):                          42167.5110
Eccentricity :                                0.00022912
Inclination (deg) :                           0.00299745
Right Ascension of Ascending Node (deg) :     170.137518
Argument of Perigee (deg) :                   232.703771
Mean Anomaly (deg) :                          161.151249
Apogee Ht (km) :                              35799.0358
Perigee Ht (km) :                             35779.7123

West Longitude (deg) :                        137.193397
Longitude Drift Rate (deg/day) :              0.00143198 EAST

Comments:
GOES-17 data propagated from orbit epoch 19/108 09:00:00.000 UTC.
Fuel and oxidizer remaining are estimates after the last maneuver on 19/108.
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