Below are the weekly GOES element sets: ============================================================= Spacecraft : GOES-09 S/C Mass (kg) : 991.641 Fuel Mass (kg) : 7.605 Oxidizer Mass (kg) : 8.696 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 06/072 12:00:00.000 Semimajor Axis (km) : 42166.7444 Eccentricity : 0.00030772 Inclination (deg) : 2.13585898 Right Ascension of Ascending Node (deg) : 87.23122676 Argument of Perigee (deg) : 270.80210500 Mean Anomaly (deg) : 153.30104700 Apogee Ht (km): 35801.58013979 Perigee Ht (km): 35775.62863421 West Longitude (deg) : 199.647 Longitude Drift Rate (deg/day) : 0.005 EAST Comments: GOES-9 data propagated from OATS orbit epoch 05/351 12:00:00.000 UTC. Fuel and oxidizer remaining are estimates after EW#32_Park at 200. ============================================================= Spacecraft : GOES-10 S/C Mass (kg) : 1000.203 Fuel Mass (kg) : 4.045 Oxidizer Mass (kg) : 9.718 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 06/072 6:00:00.000 Semimajor Axis (km) : 42165.8159 Eccentricity : 0.00016986 Inclination (deg) : 0.58903614 Right Ascension of Ascending Node (deg) : 94.35726193 Argument of Perigee (deg) : 247.79672000 Mean Anomaly (deg) : 142.96968500 Apogee Ht (km): 35794.83795169 Perigee Ht (km): 35780.51377431 West Longitude (deg) : 135.601 Longitude Drift Rate (deg/day) : 0.005 EAST Comments: GOES-10 data propagated from OATS orbit epoch 06/072 6:00 UTC. Fuel and oxidizer remaining are estimates after EW#41. ============================================================= Spacecraft : GOES-11 S/C Mass (kg) : 1136.283 Fuel Mass (kg) : 55.496 Oxidizer Mass (kg) : 88.573 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 06/072 6:00:00.000 Semimajor Axis (km) : 42162.6249 Eccentricity : 0.00052273 Inclination (deg) : 0.17719551 Right Ascension of Ascending Node (deg) : 103.69947350 Argument of Perigee (deg) : 228.82371060 Mean Anomaly (deg) : 183.62511570 Apogee Ht (km): 35806.52465784 Perigee Ht (km): 35762.44520416 West Longitude (deg) : 104.590 Longitude Drift Rate (deg/day) : 0.057 EAST Comments: GOES-11 data propagated from OATS orbit epoch 05/220 00:00:00.000 UTC. Fuel and oxidizer remaining are estimates after ZAP#6. ============================================================= Spacecraft : GOES-12 S/C Mass (kg) : 1172.514 Fuel Mass (kg) : 42.708 Oxidizer Mass (kg) : 75.039 Coordinate System : True of Date Epoch (yy/ddd hh:mm:ss.sss GMT) : 06/072 6:00:00.000 Semimajor Axis (km) : 42166.5962 Eccentricity : 0.00023002 Inclination (deg) : 0.24476979 Right Ascension of Ascending Node (deg) : 261.98554920 Argument of Perigee (deg) : 157.31147270 Mean Anomaly (deg) : 126.68961320 Apogee Ht (km): 35798.15541324 Perigee Ht (km): 35778.75692876 West Longitude (deg) : 74.727 Longitude Drift Rate (deg/day) : 0.001 EAST Comments: GOES-12 data propagated from OATS orbit epoch 06/072 6:00 UTC. Fuel and oxidizer remaining are estimates after EW#18. =============================================================