Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3262.28566 Fuel Mass (kg) : 363.790490 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/153 05:00:00.000 Semimajor Axis (km): 42166.0830 Eccentricity : 0.00005463 Inclination (deg) : 0.29070390 Right Ascension of Ascending Node (deg) : 81.0163737 Argument of Perigee (deg) : 282.477335 Mean Anomaly (deg) : 217.541658 Apogee Ht (km) : 35790.2425 Perigee Ht (km) : 35785.6354 West Longitude (deg) : 104.653495 Longitude Drift Rate (deg/day) : 0.00091827 WEST Comments: GOES-16 data propagated from orbit epoch 26/153 05:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/152. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3456.85802 Fuel Mass (kg) : 534.971124 Oxidizer Mass (kg) : 29.1868927 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/153 12:00:00.000 Semimajor Axis (km): 42164.9291 Eccentricity : 0.00006460 Inclination (deg) : 0.89036736 Right Ascension of Ascending Node (deg) : 84.4921172 Argument of Perigee (deg) : 9.16563677 Mean Anomaly (deg) : 247.824515 Apogee Ht (km) : 35789.5088 Perigee Ht (km) : 35784.0614 West Longitude (deg) : 89.4903430 Longitude Drift Rate (deg/day) : 0.00239593 EAST Comments: GOES-17 data propagated from orbit epoch 26/153 12:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/152. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3646.05082 Fuel Mass (kg) : 712.211519 Oxidizer Mass (kg) : 34.2392986 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/153 11:00:00.000 Semimajor Axis (km): 42167.0912 Eccentricity : 0.00002837 Inclination (deg) : 0.01729915 Right Ascension of Ascending Node (deg) : 61.0951362 Argument of Perigee (deg) : 155.931602 Mean Anomaly (deg) : 61.9044575 Apogee Ht (km) : 35790.1434 Perigee Ht (km) : 35787.7510 West Longitude (deg) : 137.000584 Longitude Drift Rate (deg/day) : 0.00172769 WEST Comments: GOES-18 data propagated from orbit epoch 26/153 11:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/152. ============================================================= Spacecraft : GOES-19 S/C Mass (kg) : 3854.14029 Fuel Mass (kg) : 894.055805 Oxidizer Mass (kg) : 29.4844801 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 26/153 10:00:00.000 Semimajor Axis (km): 42165.2384 Eccentricity : 0.00004750 Inclination (deg) : 0.00992434 Right Ascension of Ascending Node (deg) : 61.7392950 Argument of Perigee (deg) : 88.4652199 Mean Anomaly (deg) : 175.495389 Apogee Ht (km) : 35789.0970 Perigee Ht (km) : 35785.0917 West Longitude (deg) : 75.1896625 Longitude Drift Rate (deg/day) : 0.00313355 EAST Comments: GOES-19 data propagated from orbit epoch 26/153 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 26/153. =============================================================