The cost curve
Launch Cost per Kilogram to LEO: 1970 to 2026
The number that unlocked the regime.
From the Saturn V through the Space Shuttle and the expendable-rocket era, putting a kilogram into low Earth orbit cost between $5,000 and $54,000 in 2024 dollars. The Falcon 9 broke the curve. A dedicated reusable Falcon 9 launch now lists at $74 million for up to 22,800 kg to LEO — roughly $3,000/kg — and SpaceX’s internal marginal cost on a reused booster may be a fraction of that. The result is a 94% cost reduction in under two decades, and it made the current regime possible: Starlink’s 10,000+ satellites would have been economically unthinkable at Shuttle-era prices.
| Vehicle | Era | Payload to LEO | Approx. $/kg to LEO | Reusable? |
|---|---|---|---|---|
| Saturn V | 1967–1973 | 140,000 kg | ~$7,100 | No |
| Space Shuttle | 1981–2011 | 27,500 kg | ~$54,000 | Partial (orbiter) |
| Titan IV | 1989–2005 | 21,680 kg | ~$20,000 | No |
| Delta IV Heavy | 2004–2024 | 28,790 kg | ~$12,200 | No |
| Atlas V | 2002–2025 | 18,850 kg | ~$8,500 | No |
| Ariane 5 | 1996–2023 | 20,000 kg | ~$9,000 | No |
| Falcon 9 Block 5reusable | 2018– | 22,800 kg | ~$2,700–3,100 | First stage, 20+ reuses |
| Falcon Heavyreusable | 2018– | 63,800 kg (expended) | ~$1,400 | Side boosters recovered |
| Starshiptarget | 2025– | 100–150,000 kg | <$100 (target) | Fully reusable (goal) |
Saturn V $/kg computed from $995M per-launch cost (2024 USD) over 140,000 kg. Shuttle $/kg includes full program cost amortized per flight. Falcon 9 $/kg uses the $70M list price; SpaceX’s internal marginal cost on a reused booster may be under $15M. Starship target is an aspirational design goal, not a quoted price.
The active fleet
Operational Launch Vehicles Serving Earth Orbit in 2026
Who flies today, and what they charge.
The global launch fleet is dominated by one vehicle — SpaceX’s Falcon 9 — which flew 165 times in 2025, more than the rest of the world combined. Behind it sit China’s Long March family, the small-sat launcher Electron from Rocket Lab, Europe’s Ariane 6, and ULA’s Vulcan Centaur. The market is not a balanced competition. It is one provider setting the floor price and everyone else operating around it.
| Vehicle | Operator | Payload to LEO | Approx. $/kg | 2025 launches | Reuse |
|---|---|---|---|---|---|
| Falcon 9 Block 5 | SpaceX (US) | 22,800 kg | ~$2,700 | 165 | 1st stage, 20+ flights |
| Falcon Heavy | SpaceX (US) | 63,800 kg (exp.) | ~$1,400 | 3 | Side boosters recovered |
| Long March 5 | CASC (China) | 25,000 kg | ~$5,000–8,000 | ~3 | Expendable |
| Long March 2/3/4 family | CASC (China) | 3,000–13,500 kg | varies | ~50 | Expendable |
| Chinese commercial launchers | Various (China) | varies | varies | ~39 | Expendable (reuse in testing) |
| Electron | Rocket Lab (US/NZ) | 300 kg | ~$25,000 | 21 | Partial (catch tested) |
| Ariane 6 (A62/A64) | Arianespace (Europe) | 10,350–21,650 kg | ~$5,300–7,400 | 5 | Expendable |
| Vulcan Centaur | ULA (US) | 27,200 kg | ~$4,000 | 1 | Expendable |
| Soyuz-2 | Roscosmos (Russia) | 8,200 kg | ~$6,000 | ~15 | Expendable |
| H3 | JAXA/MHI (Japan) | ~6,500 kg | ~$7,700 | 4 | Expendable |
| PSLV / LVM3 | ISRO (India) | 3,250–8,000 kg | ~$4,500–6,000 | 5 | Expendable |
Chinese commercial launchers include vehicles from Galactic Energy, CAS Space, Orienspace, iSpace, and others operating from Jiuquan, Wenchang, and sea-launch platforms. Dollar-per-kg for Chinese vehicles is estimated from publicly available contract data. Electron’s high $/kg reflects the premium for a dedicated small-sat ride, not inefficiency — the vehicle is optimized for orbital insertion of payloads under 300 kg.
The next generation
Launch Vehicles in Development or Early Operations
The vehicles that will set the next price floor — and the ones that didn’t make it.
The vehicles listed above are the fleet as it stands. Below it is a second tier — vehicles in test, early operations, or actively preparing for first flight. Some will reshape the cost curve. Others will fail. The small-launcher survey (NewSpace Index, IAC 2025) tracks 216 launch vehicle projects worldwide; about half of those initiated in the peak years are already dormant or canceled. Reaching orbit is hard; reaching orbit profitably is harder.
Medium- and heavy-lift vehicles
| Vehicle | Developer | Target payload (LEO) | Target $/kg | Reuse |
|---|---|---|---|---|
| Starship / Super Heavy | SpaceX (US) | 100–150,000 kg | <$100 (aspirational) | Full (booster + ship) |
| New Glenn | Blue Origin (US) | 45,000 kg | ~$1,500–2,200 | 1st stage (landed twice in 3 flights) |
| Neutron | Rocket Lab (US) | 13,000 kg | ~$3,800–5,400 | 1st stage (RTLS design) |
| Terran R | Relativity Space (US) | 33,500 kg (exp.) / 23,500 kg (reused) | ~$1,600 (target) | 1st stage (20 flights target) |
| Nova | Stoke Space (US) | 3,000–7,000 kg | TBD | Full (booster + upper stage) |
| Eclipse | Firefly Aerospace / Northrop Grumman (US) | ~16,000 kg | TBD | TBD |
| Zhuque-3 (ZQ-3) | LandSpace (China) | ~21,000 kg | TBD | 1st stage (vertical landing) |
| Long March 10 / CZ-10 | CASC/CALT (China) | ~27,000 kg (reusable) | TBD | 1st stage (grid-fin RTLS) |
| Other Chinese commercial | Galactic Energy, iSpace, Space Pioneer, Deep Blue, Orienspace | varies | TBD | Various (reuse in testing) |
Small-lift vehicles
| Vehicle | Developer | Payload (LEO) | Country |
|---|---|---|---|
| Alpha Block II | Firefly Aerospace | 1,030 kg | US |
| Spectrum | Isar Aerospace | ~1,000 kg | Germany (launched from Norway) |
| Vikram-I | Skyroot Aerospace | ~300 kg | India |
| Eris | Gilmour Space | 215–305 kg | Australia |
| KAIROS | Space One | ~250 kg | Japan |
| Rocket 4 | Astra | ~300 kg | US |
The attrition rate is part of the story. For every vehicle that reaches operational service, several fail or go dormant. Astra reached a $2.1 billion SPAC valuation in 2021 and was privatized for roughly $10 million in 2024. ABL Space Systems raised over $500 million, suffered a failed maiden launch in 2023, and pivoted to missile work in 2024. Relativity’s Terran 1 flew once (partial failure, 2023) and was canceled in favor of the much larger Terran R. Virgin Orbit filed for bankruptcy in 2023 after its air-launched LauncherOne failed over the UK. The pattern is consistent: reaching orbit is a necessary but insufficient condition for commercial viability. The survivors need both a working rocket and a price the manifest will pay.
Starship’s sub-$100/kg target assumes full and rapid reuse of both stages at high cadence — a design aspiration, not a demonstrated price. All “target $/kg” figures are developer-stated goals or analyst estimates, not market-tested prices. LandSpace’s booster landing on August 19, 2026 made it the second organization in history, after SpaceX, to land an orbital-class booster. The NewSpace Index (Erik Kulu, IAC 2025) tracks 216 launch vehicle projects globally; roughly half of those initiated in peak investment years are dormant or canceled.
Launch cadence
Global Orbital Launch Rate: 2015 to 2026
The market grew threefold in five years.
Global orbital launch attempts rose from 86 in 2015 to 329 in 2025 — a 25% jump over 2024’s record. The growth is driven by two sources: SpaceX launching its own Starlink satellites (roughly 70% of all spacecraft deployed in 2025 were Starlinks), and China’s parallel expansion of both state and commercial launch capacity. Together the United States and China accounted for 88% of all orbital launches in 2025.
| Year | Global attempts | SpaceX | China (all) | Rest of world | Successes |
|---|---|---|---|---|---|
| 2015 | 86 | 7 | 19 | 60 | 82 |
| 2020 | 114 | 26 | 39 | 49 | 104 |
| 2021 | 146 | 31 | 55 | 60 | 133 |
| 2022 | 186 | 61 | 64 | 61 | 175 |
| 2023 | 223 | 98 | 67 | 58 | 211 |
| 2024 | 263 | 134 | 68 | 61 | 254 |
| 2025 | 329 | 165 | 92 | 72 | 321 |
| 2026 (YTD) | ~160 | ~80 | ~50 | ~30 | ~154 |
Data drawn from Jonathan McDowell’s Space Report, Payload Space, and SpaceNews year-end analyses. 2026 figures are through approximately mid-August and are running ahead of 2025 pace. “Rest of world” includes Russia, Europe, Japan, India, South Korea, Israel, Iran, and others. Chinese commercial launches accounted for 54% of China’s total in 2025.
Two dynamics are worth noting. First, SpaceX’s launch rate may plateau or decline slightly as Starlink deployment matures — but Starship, once operational, would absorb much of that cadence and carry far more mass per flight. Second, China is targeting 140 launches in 2026, with explicit state policy to reach at least 100 large liquid-propellant launches per year and 2,000 satellites annually to serve the Guowang and Qianfan broadband constellations.
Where the launches go
Launch Demand by Mission Type
Constellations ate the manifest.
The single largest consumer of launch services is mega-constellation deployment. In 2025, roughly 70% of all spacecraft placed in orbit were Starlink satellites. Add Amazon’s Project Kuiper (3,236 planned satellites, initial launches underway on Atlas V, Vulcan, and New Glenn), China’s Guowang and Qianfan constellations, and OneWeb, and broadband internet satellites account for the majority of global launch mass.
Beyond constellations, launch demand divides into several categories:
Government and defense. National security launches (GPS replenishment, missile warning, reconnaissance) command premium pricing — $100M+ per mission on Falcon 9 or Vulcan through National Security Space Launch contracts. The US government spent over $95 billion on space programs in 2024, with roughly half from the United States.
Civil science and exploration. NASA, ESA, JAXA, and ISRO missions to LEO, the Moon, Mars, and the outer planets — lower volume but higher per-mission value, and often the anchor customers for new vehicles (Vulcan’s debut carried a NASA-funded lunar lander; New Glenn’s second flight carried NASA’s ESCAPADE Mars orbiters).
Commercial stations and tourism. Axiom Space, Vast, and Orbital Reef are building commercial successors to the ISS. These stations need recurring crew-rotation and cargo-resupply launches — a demand stream that scales with the number of stations in operation.
Earth observation and remote sensing. The fastest-growing non-constellation segment, driven by SAR, multispectral, and hyperspectral imaging payloads from companies serving agriculture, insurance, defense, and climate monitoring.
VLEO as a launch market
Very Low Earth Orbit: The Emerging Demand Band
Orbital, not suborbital — but a different market.
Very low Earth orbit — roughly 200 to 400 km — is fully orbital. Satellites there circle Earth at 7.8 km/s just like anything else in LEO. What makes VLEO distinct is atmospheric drag: at 250 km, residual atmosphere is thick enough that an unpowered satellite reenters within months. Staying there requires continuous propulsion — electric thrusters, air-breathing engines, or frequent reboost. The ISS demonstrated the economics directly: raising its orbit from 350 km to 400 km cut annual fuel consumption from 8,600 kg to 3,600 kg. A 50 km difference halved the propellant bill.
The payoff for accepting that drag penalty is physics. Halving the distance to the ground makes an optical sensor four times more perceptive, a radar sensor eight times, and a lidar sensor 16 times. VLEO imaging satellites can deliver 10 cm visible resolution — previously achievable only from aircraft — from a platform that overflies denied airspace without permission.
| Operator / Program | Country | Target altitude | Mission |
|---|---|---|---|
| Albedo — Clarity-1 | US | <300 km | 10 cm visible + 2 m thermal IR imaging; NRO and AFRL data contracts |
| EOI Space — Stingray | US | ~250 km | 15 cm resolution imaging constellation |
| SpaceX — Starlink Direct-to-Cell | US | VLEO filing (340 km band) | 15,000-satellite VLEO constellation for direct-to-handset service |
| Kreios Space | Spain | <300 km | Air-breathing electric propulsion (ABEP) for sustained VLEO ops; NATO Innovation Fund backed |
| NewOrbit | UK | 200–300 km | VLEO satellite bus for connectivity and remote sensing |
| Bellatrix / TelePIX | India / South Korea | VLEO | Air-breathing VLEO imaging demonstration |
| China VLEO Alliance | China | <300 km | National alliance of 34 organizations; multiple experimental satellites operating below 300 km; CASIC Chutian constellation planned |
| EDA VLEO military study | Europe (EDA) | VLEO | €15.65M contract to Sener-led consortium for military VLEO satellite concept |
The VLEO satellite market is projected to grow from roughly $10M in 2025 to over $1.5B by 2034. The key enabling technologies are electric propulsion systems that can sustain orbits against continuous drag, and materials resistant to atomic oxygen erosion at these altitudes. VLEO’s “self-cleaning” property — debris decays naturally in weeks to months — is a regulatory advantage over the congested 500–600 km band.
What VLEO means for the launch market: shorter satellite lifetimes (drag limits operational life to 3–7 years even with propulsion) mean more frequent replacement launches per constellation. A VLEO constellation of 600 satellites refreshed every five years generates 120 launches per year just for replenishment — a recurring demand stream that compounds the cadence growth already driven by standard LEO constellations. The launch vehicles are the same ones listed above; VLEO is a destination, not a vehicle class.
The inbound alternative
Material Supply from Above: The Lunar Mass Driver
Not every kilogram needs to be lifted.
Everything on this page assumes that material reaches orbit by climbing out of Earth’s gravity well at great expense. But the regime could eventually receive material from the other direction. A lunar mass driver — an electromagnetic launcher on the Moon’s surface — could deliver bulk material (regolith, processed metals, oxygen, water) into Earth orbit at a fraction of the energy cost of lifting it from Earth. The Moon’s surface gravity is one-sixth of Earth’s and it has no atmosphere; the delta-v from the lunar surface to LEO is about 2.5 km/s, versus 9.4 km/s from Earth’s surface.
The mass driver is native to the Moon — it is covered on the Moon destination page — but its customer is here. If and when inbound supply from the Moon becomes operational, it does not compete with launch. It replaces it, for a specific class of bulk material that does not need to be manufactured on Earth. That is the corridor that reprices the regime from above.