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This comment reads like an S-1 pitch deck and almost every claim is false or misleading. The $16B is not profit its revenue, and I strongly suggest to learn th
by johnbarron 7mo ago
This comment reads like an S-1 pitch deck and almost every claim is false or misleading.
The $16B is not profit its revenue, and I strongly suggest to learn the difference before investing. The $8B figure is EBITDA, also known as, earnings before interest, taxes, depreciation, AND amortization.
For a company running around 9500 LEO satellites with a less than 5 year lifespan, depreciation is the business.
Their FCC filings show that about 500 satellites deorbited just in the first of half of 2025 alone, and they were all under 5 years old. The estimates for constellation sustenance are currently at $5-8B per year in satellite manufacturing (about $500K each) and launch costs are about $3M each. That is the real capex that EBITDA hides. Net income has never been disclosed and probably for good reason...
And lets not even mention the $19 billion EchoStar acquisition who is almost certainly! not included in the $8 billion EBITDA figures reported...
The most critical is that xAI is excluded from the number. XAI had a $1.46B net loss in Q3 2025 on just $107M in revenue, accelerating from $1B the prior quarter. They were burning $1B a month at the time of filing. This pig was then merged into SpaceX in Feb 2026 along with X/Twitter. So start with $8B EBITDA, subtract $5-8B satellite replacement, subtract $4-6B per year in xAI losses, subtract interest and taxes specially amortization and you are very very deep in the red. Once audited financials go public, every analyst with a calculator and a working brain will see this.
Also the revenue is largely circular... Over 70% of Falcon 9 launches in 2025 were internal Starlink missions so SpaceX is its own biggest customer. Starlink is 70% of total revenue. The so called "launch business" and "internet business" are the same capital cycle booked as two revenue lines ;-)
Replace legacy ISPs? Really? Starlink has 0.2% residential market share after 5 years, with declining ARPU ($85 avg vs $120 US) and congestion already emerging at 10M subs. It is a niche rural/maritime ISP, not an AT&T killer.
And on the valuation? NVIDIA for example, who has an almost actual monopoly on AI chips, with $216B revenue, and $120B net income, at 56% margins, trades at 20x revenue. Tesla…. already considered absurdly overvalued at P/E 355, trades at 15x. Amazon at 3x. Meta at 10x. SpaceX wants 110x !! times revenue, with no audited financials, unknown net income, and a freshly absorbed money losing AI company. Even on bullish 2026 projected revenue of $24B, it's 73x so nearly 4x NVIDIA multiple, and NVIDIA actually prints profit...
Starship on another side is very very far from routine... 11 flights, 5 failures. But notice on thing...In 2025 alone on Flight 7 the upper stage exploded from harmonic vibrations. Then Flight 8 exploded from propellant mixing. Flight 9 was destroyed on reentry...Ship 36 exploded on test stand
...the first V3 booster exploded during pressure testing and was scrapped.
See a pattern here? Each failure from a different root cause. So multiple unsolved failure modes, not iteration. It has never reached orbit, never caught a ship, never demonstrated orbital refueling.
This offering is the most scandalous ever and the structure tells you everything. The filing is confidential, REAL financials only need to go public 15 days before the roadshow. Nasdaq is literally changing its index rules effective May 1 to allow a fast track Nasdaq-100 entry in 15 trading days. This is a rule that never existed before, and is made for this IPO, forcing billions in passive index buying on day one.
Public float is just 3% to 4%. This is one of the tightest floats for any major US IPO in modern history, and I have been following the markets for 20 years. They do 30% retail allocation what is three times the norm and tells you exactly who the target buyer is.
Given this level of rule bending, dont be shocked if the S-1 with real audited numbers quietly drops at the last legally permissible moment, maybe minutes before the IPO? ensuring hype and retail commitments are fully baked, before anyone really looks at what the financials actually say.
It will be a wildly successful IPO. Same playbook as Tesla 2010, just with more zeros and fewer functioning prototypes.
- enopod_ 7mo agoBest comment I read on SpaceX in a long time
- DennisP 7mo agoThose are a lot of great points but I'll nitpick a couple things. While it's true that Starship has never reached orbit, they have reached orbital velocity several times. They could have gone into orbit if they'd aimed in that direction, but they didn't because it's a test rocket and they didn't want it to stay up there if anything went wrong. And I don't think the multiple failure causes mean they aren't iterating. They're making changes with every launch. It might mean that everything's a tradeoff, and a lot of times when you fix one thing, you create a problem somewhere else. Building a fully, rapidly reusable rocket is a really difficult task. Something you didn't mention is that even on the "successful" flights they suffered some damage on reentry. They'll have to fix that if they want rapid reuse, which is essential for the super low costs Elon estimates. I'm not sure what you mean by "never caught a ship" but they did catch a landing first stage with their launch tower, which was a pretty fancy trick nobody had tried before.
- mmmm2 7mo agoI assume he means they haven't caught the orbiter.
- deleted 6mo ago[deleted]
- kortilla 7mo ago>See a pattern here? Each failure from a different root cause. So multiple unsolved failure modes, not iteration. It has never reached orbit, never caught a ship, never demonstrated orbital refueling. Solid comment on the ISP business but this is straight up bullshit. They absolutely better have different root causes. That’s exactly what iteration looks like. Blowing up subsequent ships for the same problem would be incompetence. Also the ship has very explicitly been held from an orbital trajectory to ensure predictable reentry in the event of no re-engine light. It’s very apparent from external analysis it was capable of the extra few seconds of engine runtime for an elliptical orbit.