2 - 30 AGS STATE VECTOR UPDATE PURP PURPOSE FOR AGS STATE VECTOR UPDATE 240 ±XXXXX (100 FT) LM STATE VECTOR-POSITION COMPONENTS 241 ±XXXXX (100 FT) 242 ±XXXXX (100 FT) 260 ±XXXX.X (FPS) LM STATE VECTOR-VELOCITY COMPONENTS 261 ±XXXX.X (FPS) 262 ±XXXX.X (FPS) 254 +XXXX.X (MIN) LM TIME FOR WHICH THE STATE VECTOR IS ACCURATE 244 ±XXXXX (100 FT) CSM STATE VECTOR-POSITION COMPONENTS 245 ±XXXXX (100 FT) 246 ±XXXXX (100 FT) 264 ±XXXX.X (FPS) CSM STATE VECTOR-VELOCITY COMPONENTS 265 ±XXXX.X (FPS) 266 ±XXXX.X (FPS) 272 +XXXX.X (MIN) CSM TIME FOR WHICH THE STATE VECTOR IS ACCURATE
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Apollo 11 Flight Plan, Final - July 1, 1969 resources

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2 - 30 AGS STATE VECTOR UPDATE PURP PURPOSE FOR AGS STATE VECTOR UPDATE 240 ±XXXXX (100 FT) LM STATE VECTOR-POSITION COMPONENTS 241 ±XXXXX (100 FT) 242 ±XXXXX (100 FT) 260 ±XXXX.X (FPS) LM STATE VECTOR-VELOCITY COMPONENTS 261 ±XXXX.X (FPS) 262 ±XXXX.X (FPS) 254 +XXXX.X (MIN) LM TIME FOR WHICH THE STATE VECTOR IS ACCURATE 244 ±XXXXX (100 FT) CSM STATE VECTOR-POSITION COMPONENTS 245 ±XXXXX (100 FT) 246 ±XXXXX (100 FT) 264 ±XXXX.X (FPS) CSM STATE VECTOR-VELOCITY COMPONENTS 265 ±XXXX.X (FPS) 266 ±XXXX.X (FPS) 272 +XXXX.X (MIN) CSM TIME FOR WHICH THE STATE VECTOR IS ACCURATE

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