Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-14 S/C Mass (kg) : 1653.859 Fuel Mass (kg) : 40.426 Oxidizer Mass (kg) : 62.523 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 23/264 06:00:00.000 Semimajor Axis (km) : 42165.26311 Eccentricity : 0.000416 Inclination (deg) : 0.396779 Right Ascension of Ascending Node (deg) : 262.740470 Argument of Perigee (deg) : 228.441331 Mean Anomaly (deg) : 210.119179 Apogee Ht (km): 35804.68213 Perigee Ht (km): 35769.56409 West Longitude (deg) : 108.584 Longitude Drift Rate (deg/day) : 0.003000 EAST Comments: GOES-14 data propagated from OATS orbit epoch 23/260 00:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 23/263. ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3400.40637 Fuel Mass (kg) : 495.061208 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 23/264 08:00:00.000 Semimajor Axis (km): 42166.4541 Eccentricity : 2.1340e-05 Inclination (deg) : 0.07113132 Right Ascension of Ascending Node (deg) : 269.032537 Argument of Perigee (deg) : 216.414402 Mean Anomaly (deg) : 279.288298 Apogee Ht (km) : 35789.2170 Perigee Ht (km) : 35787.4173 West Longitude (deg) : 75.2122990 Longitude Drift Rate (deg/day) : 0.00099763 WEST Comments: GOES-16 data propagated from orbit epoch 23/264 08:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 23/263. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3533.25924 Fuel Mass (kg) : 611.372352 Oxidizer Mass (kg) : 29.1868926 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 23/264 11:30:00.000 Semimajor Axis (km): 42166.2299 Eccentricity : 0.00020175 Inclination (deg) : 0.00640403 Right Ascension of Ascending Node (deg) : 299.404076 Argument of Perigee (deg) : 210.804760 Mean Anomaly (deg) : 277.684802 Apogee Ht (km) : 35796.6000 Perigee Ht (km) : 35779.5858 West Longitude (deg) : 104.718158 Longitude Drift Rate (deg/day) : 0.00035084 EAST Comments: GOES-17 data propagated from orbit epoch 23/264 11:30:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 23/263. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3765.64953 Fuel Mass (kg) : 831.731934 Oxidizer Mass (kg) : 34.3176038 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 23/264 10:00:00.000 Semimajor Axis (km): 42165.8770 Eccentricity : 5.7211e-05 Inclination (deg) : 0.00315711 Right Ascension of Ascending Node (deg) : 359.219661 Argument of Perigee (deg) : 99.1724803 Mean Anomaly (deg) : 274.627999 Apogee Ht (km) : 35790.1524 Perigee Ht (km) : 35785.3277 West Longitude (deg) : 137.013677 Longitude Drift Rate (deg/day) : 0.00137122 EAST Comments: GOES-18 data propagated from orbit epoch 23/264 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 23/263. =============================================================