Below are the weekly GOES element sets: ============================================================= 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. ============================================================= 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. ============================================================= 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. ============================================================= 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. =============================================================