Economics of Orbital Vs. Terrestrial Data Centers
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The debate around the economics of orbital versus terrestrial data centers is heating up, with experts weighing in on the potential demand and applications that could justify the costs of space-based infrastructure. While some commenters, like d_silin, argue that demand is the driving factor, others, such as ikiris and CobrastanJorji, are skeptical, questioning what specific software applications would benefit from running in space and pointing out that cost is a significant hurdle. The discussion takes a darker turn with hirsin's accusation that orbital data centers are a potential haven for illicit activities, but others, like Glyptodon, suggest that the premise is driven by the growing need for space-centric infrastructure. As the conversation unfolds, it becomes clear that the feasibility of space data centers hinges on identifying unique use cases that can't be met by terrestrial alternatives.
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At any rate, one basic communication's satellite worth of compute would be more than enough. No need for TPUs.
Its like that scene at the end of Real Genius, "Maybe somebody already has a use for it, one for which it's perfectly designed." Lets look at the facts: Impossible to raid, not under any direct legal jurisdiction, high bandwidth line of sight communications options to satellite feed points that would be difficult to tap outside of other orbital actors, Power feed that is untethered to any planetary grid or at risk of terrestrial actors, etc.
It's definitely much easier and much much cheaper to send a single rocket there blowing the assembled rather large target into still sizeable chucks of orbital debris than it is to deploy and assemble the thing there in the first place. And there are a few terrestrial actors rather capable of this. More than there are who could make it happen under whatever optimistic assumptions anyway.
In itself, a structure of this size in orbit is an efficient catcher of micrometeorites and orbital debris. Over "non-eternal" timeframes you don't even need a bad actor with good rockets.
Nevermind that in such a case, the eventual fate of these sizeable chunks of orbital debris is to become rods of god ... just without particular steerability.
It'd be a sight.
But oddly this doesn't seem to be how the concept is typically framed.
My second level curiosity is how much cheaper/competitive it'd be if we had space elevators.
I suspect it is about the regulatory environment. The regulatory environment on data centers is moving quickly. Data centers used to be considered a small portion of the economy and thus benign and not worth extorting/controlling. This seems to be changing, rapidly.
Given that data centers only exchange information with their consumers they are a natural candidate for using orbit as a way to escape regulators.
Further, people are likely betting that regulators will take considerable time to adjust since space is multinational.
My point is that you can actually reduce it all to dollars. And I believe that the cost of orbital data centers will come down due to technological advances, while the cost of regulation will only go up, because of local and global opposition.
I'm not sure. A couple of points:
1) The regulatory landscape is enormous. It is unknown from which angle regulators will "slow you down."
2) As I mentioned the regulatory frameworks in this area are evolving very quickly. It is unknown what the regulations will be in 1, 2, 5 years and how that will impact your business.
That's not true for people experienced in the particular industry. Others can find a lawyer that will give them a good picture.
It’s a bit like the cyberpunk future when the ultra riches live in moon bases or undersea bases and ordinary people fight for resources in a ruined earth.
The numbers don't quite work out in favor of orbital datacenters at the current values. But we can tell from analyses like this what has to change to get there.
These numbers are just random bullsh*t numbers.
And what problems do orbital datacenters solve? They still need uplink, so not libertarian we can do what we want, you have no jurisdiction here thing.
This is just a sci-fi idea that is theoretically possible and is riding the ai bubble for users and investors that don’t know better.
I 100% agree with this. There are ~2,600 billionaires in the world and we should encourage all of them to spend their money. Even buying a superyacht is a benefit to the economy. But the best billionaires, like Bill Gates and Elon Musk, are actually trying to advance the tech tree.
We are honestly lucky that Musk is wired funny. Any normal human being would retire and hang out on the beach with supermodels after all the abuse he has taken. But he takes it all as a personal challenge and doubles down. That is both his worst quality and his best.
First, he seeks and creates conflict. He isn't 'taking' abuse, except in the sense that he is reaching out and grasping at it.
Everyone in that position takes lots of abuse. If they built their own fortune, they generally don't retire to the beach or they would have long ago.
But I think we'd be better off if taking a political position did not automatically piss off half the country. I think a lot of competent but normal people refuse the get involved in politics because of how toxic it is.
I wish Musk had stayed out of politics, but I'm glad he hasn't given up on Tesla/SpaceX just because of the enemies he's made. I think any normal person would have.
He's been possibly the world's leading troll since long before his MAGA phase. Let's be serious.
You’re falling victim to the ‘broken windows fallacy’ here; money which is invested is actually more productive in improving medium and long term economic productivity than ‘consumption’ goods. Even ‘retained’ money (under one’s mattress) is not net-negative, as it increases the value of its circulating counterparts.
Scenario B: A homeowner adds a new window to their home.
Scenario C: A homeowner buys an online-course to learn how to make windows and then adds one to their home.
Scenario A has approximately no benefit to the economy. The homeowner is no better off (same number of windows) but had to spend money. The window maker might be better off, but only to the same extent that the homeowner is worse off.
I totally agree that Scenario A is not a benefit to the economy. That's the "broken window fallacy".
But Scenario B is definitely better for the economy. The homeowner has decided that having a new window is better than having the money. So the homeowner is better off. The window maker is also better off because they get the money. This is what happens when a billionaire buys a yacht.
Scenario C is the best. The homeowner has a new skill, which they can use to add more windows to their house or maybe their neighbors' houses. Over time, the amount of money spent on window-making will decrease, but the number of windows will stay constant or increase. That's a net benefit. And the online-course creator still made money.
This is what Musk is doing. He is developing new technologies that enable new capabilities and/or make existing things cheaper (e.g., electric cars, access to space, rural internet connectivity).
There is also Scenario D: The homeowner doesn't buy a new window but just keeps his money under his mattress. This is clearly the worst for the economy. Hording money like that means that there is less money circulating and lowered economic activity. The window maker is worse off, and even the homeowner is worse off if they would like to have a new window.
Billionaires who don't spend their money are the real danger, not the ones who tweet too much.
Investing their money is slightly better in that it makes the price of borrowing cheaper. But that only helps up to a point. Someone has to spend money or else there's no point in being able to borrow some. So I wish more billionaires were following Scenario C.
Scenario D: A homeowner adds 10 window to their home because the populous think he is stingy and will send him to the guillotine if he does not start spending his money on new windows!
Scenario D provides no benefit to society.
If the billionaire does want the yacht, then no encouragement is needed.
Diminishing names used for delegitimization are not something reddit invented. Calling George W. Bush "dubya", Barack Obama "barry", or Richard Nixon "look it up" are all great examples of a time-honored tradition.
Hope I cleared that up for you.
https://finance.yahoo.com/news/musks-net-worth-hits-600-2022...
He is a walking billboard.
Somehow I don't think those are the only options. AFAIK Starlink is using a lot of non-rad-hard silicon already.
Random errors will occur you just need to be checking fast enough to fix and update that bad bit flip.
I am sure there's all sorts of fun algorithms in this space but I am under the impression there is SOME tax to doing this. What is the tax? Is it 10% ir 60% I have no idea would love to know!
The unit economics of orbital GPUs suggest that we'll need to run them for much longer than that. This is actually one of the few good points of orbital data centers, normally older hardware is cycled out because it's not economic to run anymore due to power efficiency improvements, but if your power is "free" and you've already got sufficient solar power onboard for the compute, you can just keep running old compute as long as you can keep the satellite up there.
I'd be interested to know what the average lifespan or failure rate of Starlink has been. That's good that some are still up there 6+ years later, but I know many aren't. I'm not sure how many of those ran out of fuel, had hardware failures, or were simply obsolete, but an AFR would be interesting to see.
https://planet4589.org/space/con/star/stats.html
https://news.ycombinator.com/item?id=16527007 ("First firing of air-breathing electric thruster (esa.int)" (2018))
Besides, that's even more mass to be lofted. Pushing the economics further into the ludicrous end.
> For ML accelerators to be effective in space, they must withstand the environment of low-Earth orbit. We tested Trillium, Google’s v6e Cloud TPU, in a 67MeV proton beam to test for impact from total ionizing dose (TID) and single event effects (SEEs). > > The results were promising. While the High Bandwidth Memory (HBM) subsystems were the most sensitive component, they only began showing irregularities after a cumulative dose of 2 krad(Si) — nearly three times the expected (shielded) five year mission dose of 750 rad(Si). No hard failures were attributable to TID up to the maximum tested dose of 15 krad(Si) on a single chip, indicating that Trillium TPUs are surprisingly radiation-hard for space applications.
Exploring a space-based, scalable AI infrastructure system design - https://research.google/blog/exploring-a-space-based-scalabl... - https://news.ycombinator.com/item?id=45813267 (Nov 4 2025, 44 points, 73 comments)
> Project Suncatcher is a moonshot exploring a new frontier: equipping solar-powered satellite constellations with TPUs and free-space optical links to one day scale machine learning compute in space.
If you go out to MEO then suddenly you're outside that protective magnetic shield and you have to deal with charged particles smashing into you and you want a large mass of water or wax shielding if you don't have radiation tolerant electronics.
SSO, a low earth orbit whose plane is perpendicular to the direction of the sun so it gets constant sunlight, is harsher than normal LEO orbits because it passes over the poles where the protection from the Earth's magnetic field is weakest, but it's still a lot better than higher orbits. This is probably where you want a datacenter to get constant sunlight and as much protection as possible.
I think “won’t”. I could be wrong of course, but I imagine efforts to put servers into orbit will die before anything is launched. It’s just a bad idea. Maybe a few grifters will make bank taking suckers’ money before it becomes common knowledge that this is stupid, but I will be genuinely surprised if real servers with GPUs are launched.
I don’t mean to be facetious here. But saying “will” is treating it as inevitable that this will happen, which is how the grifters win.
Silently wrong results are very fashionable these days, you know. Deterministic results are very 2010s.
It's great that this site drills down even further to demonstrate that there is absolutely no point at which the launch costs ever make this economical or viable, so I really don't understand what people are doing.
Especially because this site was harping for years about the cost of launches and putting things in to orbit, the whole reason why SpaceX got started and has grown as it has. As soon as that became an inconvenient number, we now just make things up (Just pretend that launch costs are 10% of what they actually are to get people to invest?).
[1]: https://starcloudinc.github.io/wp.pdf
I think datacentres in space are predicated on Starship bringing launch costs down. Way down.
The $5M is a marginal cost-target for fully reusable Starship.
With that said, my employer now appears to be in this business, so I guess if there's money there, we can build the satellites. (Note: opinions my own) I just don't see how it makes sense from a practical technical perspective.
Space is a much harder place to run datacenters.
Unless you have a plan to change the laws of physics, space will always be a good insulator compared to what we have here on Earth.
No need to rewrite anything. Radiators are 30% heavier per watt than solar panels. This is far from impossible.
Let’s say you need 50m^2 solar panels to run it, then just a ton of surface area to dissipate. I’d love to be proven wrong but space data centers just seem like large 2d impact targets.
So now we have arrived to a revised solution: a puny 8RU server at 130 kg, requires 100sqm and 1000 kg of solar panels, then 50-75 sqm of the heat radiators at 1000-1500 kg, then 100-200 kg of batteries and then the housing for all that stuff plus station keeping engines and propellant, motors to rotate all panels, pumps, etc. I guess at least 500kg is needed, maybe a bit less.
So now we have a 3 ton satellite, which costs to launch around 10 million dollars at an optimistic 3000/kg on F9. And that's not counting cost to manufacture the satellite and the server own cost.
I think the proposal is quite absurd with modern tech and costs.
I bet you a million dollars cash that you would not be able to reach them.
If it was just about cooling and power availability, you'd think people would be running giant solar+compute barges in international waters, but nobody is doing that. Even the "seasteading" guys from last decade.
These proposals, if serious, are just to avoid planning permission and land ownership difficulties. If unserious, it's simply to get attention. And we're talking about it, aren't we?
In general I don't understand this line of thinking. This would be such a basic problem to miss, so my first instinct would be to just look up what solution other people propose. It is very easy to find this online.
The physics is quite simple and you can definitely make it work out. The Stefan Boltzman law works in your favor the higher you can push your temperatures.
If anything a orbital datacenter could be a slightly easier case. Ideally it will be in an orbit which always sees the sun. Most other satellites need to be in the earth shadow from time to time making heaters as well radiators necessary.
I suppose one could get some sub part of the whole satellite to a higher temperature so as to radiate heat efficiently, but that would itself take power, the power required to concentrate heat which naturally/thermodynamically prefers to stay spread out. How much power does that take? I have no idea.
You not only need absolute huge radiators for a space data centre, you need an active cooling/pumping system to make sure the heat is evenly distributed across them.
I'm fairly sure no one has built a kilometer-sized fridge radiator before, especially not in space.
You can't just stick some big metal fins on a box and call it a day.
If we run the radiators at 80C (a reasonable temp for silicon), that's about 350K, assuming the outside is 0K which makes the radiator be able to radiate away about 1500W, so roughly double.
Depending on what percentage of time we spend in sunlight (depends on orbit, but the number's between 50%-100%, with a 66% a good estimate for LEO), we can reduce the radiator surface area by that amount.
So a LEO satellite in a decaying orbit (designed to crash back onto the Earth after 3 years, or one GPU generation) could work technically with 33% of the solar panel area dedicated to cooling.
Realistically, I'd say solar panels are so cheap, that it'd make more sense to create a huge solar park in Africa and accept the much lower efficiency (33% of LEO assuming 8 hours of sunlight, with a 66% efficiency of LEO), as the rest of the infrastructure is insanely more trivial.
But it's fun to think about these things.
It receives around 2.5kW[0] of energy (in orbit), of which it converts 500W to electric energy, some small amount is reflected and the rest ends up as heat, so use 1kW/m^2 as your input value.
> If we run the radiators at 80C (a reasonable temp for silicon), that's about 350K, assuming the outside is 0K which makes the radiator be able to radiate away about 1500W, so roughly double.
1500W for 2m^2 is less than 2000kW, so your panel will heat up.
[0] https://www.sciencedirect.com/topics/engineering/solar-radia...
Put another way, 2 sq m intercepts 2600 w of solar power but only radiates ~1700 w at 350 k, which means it needs to be run at a higher temperature of nearly 125 celsius to achieve equilibrium.
You need enough radiators for peak capacity, not just for the average. It's analogous to how you can't put a smaller heat sink on your home PC just because you only run it 66% of the time.
This is all fundamental to the universe. All energy in the universe comes exclusively from systems moving from a low entropy state to a higher entropy state. Energy isn't a static absolute value we can just use. It must be extracted from an energy gradient.
Or 3.651 km squared and 2.581 km squared.
Cue jokes about running out of orbital space. Or SpaceX coming up with a new Super Super Heavy.
Heat dissipation isn't going to work across surfaces at that scale passively. So there will need to be radiators with fluid exchange over all that real estate. Orders of magnitude more trouble, weight, risk and expense than transferring electrons.
Which means cooling area now needs to be talked about in cooling volume and flow. So the cascade of complexity challenges goes all the way back to infernal launch volume logistics.
Cooling is going to be orders of magnitude more trouble than power.
At least we can assume renegade space trash is going to get caught by these mitts.
How are these ideas getting any respect?
Could the compute be distributed instead? Instead of gathering all the power into a centrap location to power the GPUs there, stick the GPUs on the back of the solar panels as modules? That way even if you need active fluid exchanger it doesn’t have to span kilometers just meters.
I guess that would increase the cost of networking between the modules. Not sure if that would be prohibitive or not.
That would increase latency, slowing down compute.
3491 V1 sats × 22.68 m² = 79176 m²
5856 V2-mini sats × 104.96 m² = 614 646 m²
Total: 0.7 km² of PERC Mono cells with 23% efficiency.
At around 313W/m² we get 217MW. But half the orbit it's in shade, so only ~100MW.
The planned Starship-launched V2 constellation (40k V3 sats, 256.94 m²) comes out at 10 km², ~1.5GW.
So it's not like these ideas are "out there".
Distances are not our friend in orbit. Efficiency scales down for many things, as distances scale up.
Consider how structural strength needs go up faster than distance. Consider how any maneuvers take much more energy, for one big satellite, instead of individual satellites, given any rotation requirement. Consider how heat flow dissipation slows across distances.
Whereas, the structural costs of human friendly pressured 3D volume goes down with scale.
You can't just concatenate some satellites and get a bigger satellite with the same characteristics.
You could distribute the compute among smaller satellites. But now you have far greater latency and reduced bandwidth.
So maybe if we had such PV, we could make huge gossamer-thin arrays that don't have much mass, then use the power from these arrays to pump waste heat up to higher temperature so the radiators could be smaller.
The enabling technology here would be those very low mass PV arrays. These would also be very useful for solar-electric spacecraft, driving ion or plasma engines.
But since there are so few such molecules in any cubic meter, there isn't much energy in them. So if you put an object in such a rarefied atmosphere. It wouldn't get heated up by it despite such a gas formally having such a temperature.
The gas would be cooled down upon contact with the body and the body would be heated up by a negligible amount
As you intimated, the radiated heat Energy output of an object is described by the Stefan-Boltzmann Law, which is E = [Object Temp ]^4 * [Stefan-Boltzmann Constant]
However, Temp must be in units of an absolute temperature scale, typically Kelvin.
So the relative heat output of a 90C vs 20C objects will be (translating to K):
383^4 / 293^4 = 2.919x
Plugging in the constant (5.67 * 10^-8 W/(m^2*K^4)) The actual values for heat radiation energy output for objects at 90C and 20C objects is 37.95 W/m^2 and 12.99 W/m^2
The incidence of solar flux must also be taken into account, and satellites at LEO and not in the shade will have one side bathing in 1361 W/m^2 of sunlight, which will be absorbed by the satellite with some fractional efficiency -- the article estimates 0.92 -- and that will also need to be dissipated.
The computer's output needs to be accounted for, for reference[0] a G200 consumes up to 700W, though that is presumably taken from the incident solar radiation so we don't need to add that separately, we can just model the satellite as needing to shed 1361 W/m^2 * 0.92 = 1252 W/m^2 for each square meter of its surface facing the sun.
We've already established that objects at 20C and 90C only radiate 12.99 W/m^2 and 37.95 W/m^2, respectively, so to radiate 1252 W per square meter coming in from the sun facing side we'll need 1252/37.92 = 33 times that area of shaded radiator, if that radiator's surface can be maintained at a uniform 90C. If we wanted the radiator to run cooler, at 20C, we'd need 2.919x as much as at 90C, or 95 square meters of shaded radiator for every square meter of sun facing material.
[0] Nvidia G200 specifications: https://www.nvidia.com/en-us/data-center/h200/
(293^4 - 283^4) = 9.55e8
(363^4 - 283^4) = 1.09e10
So about 10x
I have no problem with your other numbers which I left out as I was just making a very rough estimate.
I'm assuming the radiators are shaded from that flux by the rest of the satellite, for efficiency reasons, so we don't need to account for solar flux directly heating up the radiators themselves and reducing their efficiency.
In the shade, the radiators emission is relative to the background temp of empty space, which is only 2.7 K[0]. I did neglect to account for that temperature, that's true, but it should be negligible in its effects (for our rough estimate purposes).
[0] https://sciencenotes.org/how-cold-is-space-what-is-its-tempe...
See here for all the great ways of getting rid of thermal energy in space: https://www.nasa.gov/smallsat-institute/sst-soa/thermal-cont...
Overall not a great model. But on the other hand, even an amateur can use this model and imagine that additional parts and costs are missing, so if it's showing a bad outlook even in the favorable/cheating conditions for space DCs, then they are even dumber idea if all costs would be factored in fully. Unfortunately many serious journalists can't even do that mental assumption. :(
https://taranis.ie/datacenters-in-space-are-a-terrible-horri...
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If I were to guess, my first bet would be grand PR damage control for all the mexicans, irish, and what have you as in “don’t worry, we’ll soon be in space and out of your backyard” (no, they won’t).
https://www.nytimes.com/2025/10/20/technology/ai-data-center...
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