Well, 1 ton means a launch price of $1 million at $1,000/kg. That is also heavy for a 1 meter cube. Usually sats that size range from 50 kg up to 250 kg. Your mass is really determined by what you want to do vs the available technology. Given increasing miniaturization, there is no reason not to try to make your sat as small as possible. Thanks to the CubeSat program there are actually many common sat components being produced by MEMS processes: accelerometers, reaction wheels, plasma thrusters, etc.<br /><br />As things advance, you'll essentially build an Iridium equivalent sat phone, a PDA sized personal server, then build in a fuel tank (aerosol cans or CO2 cartridges) for your laser diode plasma thruster, MEMS reaction wheels, accelerometers and star trackers. Digital web cameras on gimbal mounts, deployable solar panels, perhaps even a betavoltaic cell.<br /><br />For personal satellites, you do want to be concerned about too many in orbit. Definitely there should be defined orbital corridors for personal satellites and rules about deorbiting at end of life, or maneuver to recycling/refuelling stations.<br /><br />What is the market for personal satellites: Here is a question where I think we are at the point where IBM chairman once said he thought the world market for computers was 3, or perhaps slightly beyond that point. We know from the CubeSat movement that the numbers the established satellite industry uses are false. There are now over 100 teams building CubeSats, both at the university, high school, and private enterprise levels. With a launch price point 40 times lower than today, this number should expand significantly to a true consumer markent, just as the original PC market opened up with machines priced from $2000-3000 in 1990 dollars (about $3500-5000 in current year dollars).<br /><br />Before this, back to the 1970's, recall the Altair personal computer. It was sold as a kit you had to assemble, its only user interface was some blinking lights on the