This saved console is a toy staging model, not live mission telemetry. Its nominal spring push speed is point two two meters per second. Selecting the thirty-minute source marker assigns eighteen hundred seconds and a drift distance of three hundred ninety-six meters. Selecting ninety minutes assigns fifty-four hundred seconds and eleven hundred eighty-eight meters. Both bars use point four pixels per meter. Source timeline jumps calculate speed times total selected time; they do not integrate a real mission trajectory. The source configuration labels the full stack at forty-one hundred kilograms and the remaining composite at twenty-nine hundred fifty. Separating the transfer module changes the displayed mass by eleven hundred fifty kilograms. Both bars use point one pixels per kilogram. These are fixed source parameters, not a measured momentum or mass estimate. The pyro control marks separation and triggers a finite visual flash; the free-running clock advances thirty simulated seconds per real second until the original Pause control is used. The source acquisition rule compares simulated time against sixty-seven hundred eighty seconds, equivalent to one hundred thirteen minutes. A ninety-minute timeline jump sets fifty-four hundred seconds, below this threshold. The one-hundred-thirteen-minute jump reaches the threshold and labels carrier acquisition locked. Both bars use point zero seven pixels per second. This is a source if-statement, not evidence of a received spacecraft signal. The original thirty-to-ninety-minute stream-pause band and all telemetry labels remain unchanged.