Landing-site decisions

Lunar Landing Site Explorer

Compare where major lunar landers touched down and why different regions served different scientific and engineering goals. Coordinates are reference values, not navigation data.

Site / missionDateRegionTypeCoordinatesWhy it matters
Luna 91966-02-03Oceanus Procellarumsoft landing7.130°, -64.370°First successful soft landing on the Moon
Surveyor 11966-06-02Oceanus Procellarumsoft landing-2.474°, -43.339°First successful U.S. lunar soft landing
Apollo 111969-07-20Mare Tranquillitatiscrewed landing0.674°, 23.473°First crewed lunar landing
Apollo 121969-11-19Oceanus Procellarumcrewed landing-3.013°, -23.422°Precision landing near Surveyor 3
Apollo 141971-02-05Fra Maurocrewed landing-3.645°, -17.471°Crewed geological exploration of Fra Mauro
Apollo 151971-07-30Hadley-Apenninecrewed landing26.132°, 3.634°First use of the Lunar Roving Vehicle
Apollo 161972-04-21Descartes Highlandscrewed landing-8.973°, 15.501°Crewed exploration of lunar highlands
Apollo 171972-12-11Taurus-Littrowcrewed landing20.191°, 30.772°Final Apollo lunar landing and longest Apollo surface exploration
Chang'e 32013-12-14Mare Imbriumlander and rover44.121°, -19.511°China's first lunar soft landing
Chang'e 42019-01-03Von Kármán craterlander and rover-45.457°, 177.588°First soft landing on the lunar far side
Chandrayaan-3 Vikram2023-08-23Southern high latitudeslander and rover-69.373°, 32.319°India's first successful lunar soft landing
SLIM2024-01-20Shioli crater regionprecision lander-13.316°, 25.251°High-precision landing technology demonstration
IM-1 Odysseus2024-02-22Malapert A regioncommercial landerSee mission sourceFirst U.S. soft lunar landing since Apollo 17
Blue Ghost Mission 12025-03-02Mare Crisiumcommercial landerSee mission sourceCommercial delivery of NASA science payloads

Why the same site is not best for every mission

Landing-site selection balances terrain safety, illumination, Earth visibility, thermal conditions, scientific access, mobility and mission architecture. The examples below show how those priorities change from a first crewed landing to a far-side rover or a south-polar campaign.

Mare Tranquillitatis

Apollo 11

Terrain
Broad mare plain selected for relatively manageable landing terrain within Apollo-era constraints.
Illumination
Mission timing provided suitable Sun angle for landing visibility and surface operations.
Earth communications
Direct Earth line of sight from the near side.
Science
Mare basalt, regolith and early crewed surface experiments.
Resource context
Not selected for resource prospecting.
Operational trade-off
Favourable first-landing safety and communications took priority over reaching the most geologically diverse site.

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Hadley-Apennine

Apollo 15

Terrain
Mountain-front valley beside Hadley Rille, more geologically ambitious than earlier Apollo sites.
Illumination
Daylight operations with low-angle terrain relief useful for field geology.
Earth communications
Direct Earth line of sight from the near side.
Science
Hadley Rille, Apennine highlands, mare materials and broader rover-supported field geology.
Resource context
Not selected for resource prospecting.
Operational trade-off
Greater terrain complexity was accepted because rover mobility and improved landing capability opened access to richer geology.

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Taurus-Littrow

Apollo 17

Terrain
Valley enclosed by massifs with access to highland and volcanic materials.
Illumination
Daylight EVA operations planned around landing and traverse geometry.
Earth communications
Direct Earth line of sight from the near side.
Science
Ancient highland material, mare basalt and pyroclastic deposits including orange soil.
Resource context
Not selected for resource prospecting.
Operational trade-off
A complex field site was chosen to maximise geological diversity during the final Apollo landing mission.

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Von Kármán crater

Change 4

Terrain
Far-side crater floor within the South Pole-Aitken Basin.
Illumination
Normal lunar day/night cycle for the landing latitude.
Earth communications
No direct Earth line of sight; relay communications are required.
Science
Far-side surface geology, South Pole-Aitken context and in-situ measurements unavailable to Apollo sites.
Resource context
Primarily scientific rather than resource-driven.
Operational trade-off
Unique far-side science required a dedicated relay architecture and operations through a second spacecraft.

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Southern high latitudes

Chandrayaan 3

Terrain
Southern high-latitude landing region selected for a soft-landing technology demonstration and local surface science.
Illumination
Operations were timed for local daylight; long lunar night constrained the nominal surface lifetime.
Earth communications
Direct and mission-architecture communications supported near-side high-latitude operations.
Science
Local temperature profile, plasma environment, seismic activity and elemental chemistry.
Resource context
Near the broader south-polar exploration zone but not a direct permanently shadowed ice-extraction demonstration.
Operational trade-off
High southern latitude increased exploration relevance while retaining a landing region compatible with the mission design.

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Shackleton / south-polar region

Shackleton Region

Terrain
Rugged polar topography with crater rims, slopes and nearby permanently shadowed terrain.
Illumination
Very low Sun angles; elevated terrain can receive extended illumination while adjacent crater interiors remain in permanent shadow.
Earth communications
Earth visibility depends strongly on local horizon and exact site; relay capability can improve resilience.
Science
Polar volatiles, ancient geology, illumination and thermal extremes.
Resource context
High interest because cold traps can preserve water ice and other volatiles, but abundance and accessibility vary by location.
Operational trade-off
Exceptional science and resource interest come with difficult lighting, thermal boundaries, terrain and navigation conditions.

Explore the south-polar environment