DATE: 25 July 1997 (J-206) SUBJECT: NAVIGATION SUMMARY (TEST) (WEST) (EAST) GOES-10f GOES-9e GOES-8d POSITION 104.542 135.385 75.186 DRIFT RATE 0.070E 0.015E 0.046W FUEL REMAINING 146.453f 118.034e 101.805d OXIDIZER REMAINING 242.133f 193.795e 163.794d INCLINATION 0.286 0.301 0.115 MANEUVER DATE ------ ------ 7-30-97 MANEUVER TYPE ------ ------ SK i PROPELLANT COST ------ ------ 0.251 GOES-7g GOES-3 GOES-2 MET-5c MET-6c POSITION 99.182a 109.189 173.212a 9.532 0.297h DRIFT RATE 0.037Ea 0.005W 0.091Wa 0.005E 0.000Eh FUEL REMAINING 16.129ba 4.863 6.761a ------ ------ INCLINATION 3.857ba 11.889 12.857a 1.379 0.208h SPIN RATE 100.386 100.446 99.618 ------ ------ MANEUVER DATE ------ ------ ------ ------ ------ MANEUVER TYPE ------ ------ ------ ------ ------ FUEL COST ------ ------ ------ ------ ------ COMMENTS: (a) Predicted value. (b) Fuel uncertainty +/- 11 pounds - no N/S maneuvers. (c) M5, M6 weekly summary data not available. (d) GOES-8 data propagated from OATS orbit epoch 97:206 12h. Fuel and oxidizer remaining are estimates after EWSK 97:120. (e) GOES-9 data propagated from OATS orbit epoch 97:206 06h. Fuel and oxidizer remaining are estimates after EWSK 97:170. (f) GOES-10 data propagated from FDF orbit epoch 97:205 12h. Fuel and oxidizer remaining are estimates after SHM wheel reset 97:150. (g) GOES-7 Imager off (operations) 11 Jan 96 standby status. (h) M6 data for 8 June 97. (i) GOES-8 EWSK maneuver 97:211 predicted propellant used 0.251 pounds. Definition of terms: SK -- Stationkeeping POSITION -- Degs west long NS -- Inclination change DRIFT RATE -- Degs per day REOR -- Spin axis reorientation SPIN RATE -- RPM EW -- In-plane station change FUEL,OXID,PROP -- Pounds