Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-14 S/C Mass (kg) : 1650.731 Fuel Mass (kg) : 39.257 Oxidizer Mass (kg) : 60.563 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/185 06:00:00.000 Semimajor Axis (km) : 42166.65136 Eccentricity : 0.000296 Inclination (deg) : 0.375228 Right Ascension of Ascending Node (deg) : 98.624178 Argument of Perigee (deg) : 14.179788 Mean Anomaly (deg) : 150.439299 Apogee Ht (km): 35801.00802 Perigee Ht (km): 35776.01470 West Longitude (deg) : 108.497 Longitude Drift Rate (deg/day) : 0.004000 EAST Comments: GOES-14 data propagated from OATS orbit epoch 24/184 00:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/184. ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3353.44752 Fuel Mass (kg) : 448.102356 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/184 08:00:00.000 Semimajor Axis (km): 42164.8462 Eccentricity : 1.1537e-05 Inclination (deg) : 0.07225480 Right Ascension of Ascending Node (deg) : 271.817470 Argument of Perigee (deg) : 282.909533 Mean Anomaly (deg) : 130.925511 Apogee Ht (km) : 35787.1957 Perigee Ht (km) : 35786.2227 West Longitude (deg) : 75.2011545 Longitude Drift Rate (deg/day) : 4.8421e-05 WEST Comments: GOES-16 data propagated from orbit epoch 24/184 08:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/183. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3501.18910 Fuel Mass (kg) : 579.302211 Oxidizer Mass (kg) : 29.1868926 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/184 11:30:00.000 Semimajor Axis (km): 42164.8300 Eccentricity : 9.4657e-05 Inclination (deg) : 0.00283509 Right Ascension of Ascending Node (deg) : 33.9598793 Argument of Perigee (deg) : 115.037871 Mean Anomaly (deg) : 199.786669 Apogee Ht (km) : 35790.6842 Perigee Ht (km) : 35782.7018 West Longitude (deg) : 104.717638 Longitude Drift Rate (deg/day) : 2.0981e-05 WEST Comments: GOES-17 data propagated from orbit epoch 24/184 11:30:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/183. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3726.79027 Fuel Mass (kg) : 792.889467 Oxidizer Mass (kg) : 34.3008065 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/184 10:00:00.000 Semimajor Axis (km): 42166.0065 Eccentricity : 4.4749e-05 Inclination (deg) : 0.00402790 Right Ascension of Ascending Node (deg) : 65.5941204 Argument of Perigee (deg) : 156.854987 Mean Anomaly (deg) : 71.4728045 Apogee Ht (km) : 35789.7564 Perigee Ht (km) : 35785.9825 West Longitude (deg) : 137.010010 Longitude Drift Rate (deg/day) : 0.00350793 WEST Comments: GOES-18 data propagated from orbit epoch 24/184 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/183. =============================================================