Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-14 S/C Mass (kg) : 1630.155 Fuel Mass (kg) : 31.530 Oxidizer Mass (kg) : 47.714 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/240 06:00:00.000 Semimajor Axis (km) : 42165.29453 Eccentricity : 0.000374 Inclination (deg) : 0.031837 Right Ascension of Ascending Node (deg) : 215.632816 Argument of Perigee (deg) : 303.231809 Mean Anomaly (deg) : 158.769989 Apogee Ht (km): 35802.94366 Perigee Ht (km): 35771.36540 West Longitude (deg) : 108.318 Longitude Drift Rate (deg/day) : 0.006000 EAST Comments: GOES-14 data propagated from OATS orbit epoch 24/235 00:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/239. ============================================================= Spacecraft : GOES-16 S/C Mass (kg) : 3345.79905 Fuel Mass (kg) : 447.303876 Oxidizer Mass (kg) : 34.9351702 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/240 08:00:00.000 Semimajor Axis (km): 42165.4034 Eccentricity : 0.00002174 Inclination (deg) : 0.06927056 Right Ascension of Ascending Node (deg) : 265.172811 Argument of Perigee (deg) : 304.296485 Mean Anomaly (deg) : 171.381146 Apogee Ht (km) : 35788.1762 Perigee Ht (km) : 35786.3427 West Longitude (deg) : 75.2011416 Longitude Drift Rate (deg/day) : 0.00255231 EAST Comments: GOES-16 data propagated from orbit epoch 24/240 08:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/239. ============================================================= Spacecraft : GOES-17 S/C Mass (kg) : 3498.77925 Fuel Mass (kg) : 576.892359 Oxidizer Mass (kg) : 29.1868927 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/240 11:30:00.000 Semimajor Axis (km): 42165.6830 Eccentricity : 0.00017850 Inclination (deg) : 0.00611527 Right Ascension of Ascending Node (deg) : 310.849112 Argument of Perigee (deg) : 243.494390 Mean Anomaly (deg) : 209.640003 Apogee Ht (km) : 35795.0654 Perigee Ht (km) : 35780.0125 West Longitude (deg) : 104.712102 Longitude Drift Rate (deg/day) : 0.00325381 EAST Comments: GOES-17 data propagated from orbit epoch 24/240 11:30:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/239. ============================================================= Spacecraft : GOES-18 S/C Mass (kg) : 3725.15844 Fuel Mass (kg) : 791.257632 Oxidizer Mass (kg) : 34.3008065 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 24/240 10:00:00.000 Semimajor Axis (km): 42165.6081 Eccentricity : 0.00002572 Inclination (deg) : 0.00467388 Right Ascension of Ascending Node (deg) : 68.7520508 Argument of Perigee (deg) : 155.424873 Mean Anomaly (deg) : 124.949817 Apogee Ht (km) : 35788.5485 Perigee Ht (km) : 35786.3796 West Longitude (deg) : 137.005692 Longitude Drift Rate (deg/day) : 0.00135227 WEST Comments: GOES-18 data propagated from orbit epoch 24/240 10:00:00.000 UTC. Fuel and oxidizer remaining are estimates after the last maneuver on 24/239. =============================================================