Object profile · DEIMOS
Deimos
Outer irregular natural satellite of Mars
Mars's smaller, smoother-looking moon, with craters partly softened by a thick blanket of loose debris.
- Atlas data reviewed
- Editorial stage
- Published
- Visibility
- Public
Direct observationOfficial grayscale observation. The frame is selected for surface readability and is not a size comparison.
NASA/JPL/University of Arizona ↗What this world is
Deimos is only about 12 kilometres across by mean diameter. Weak gravity cannot pull it into a sphere or hold an atmosphere.
Why it looks this way now
Spacecraft images show a heavily cratered surface partly buried by regolith. Its origin is still debated alongside Phobos.
Where it sits
The outer Martian moon, taking a little more than one Earth day to circle Mars.
Swipe sideways to inspect the full map
Deimos is 2 of 2 profiled Mars moons by distance, at a mean center distance of about 23,463 km.
The left panel locates Mars, dashed lines mark the scale change, and muted orbits and dots represent other profiled moons on the right. Phobos is the adjacent profiled moon inside; it is the outermost profiled moon in the system.
Read the numbers
Reference values retain their units, context, evidence state and published uncertainty.
Physical measurements
- Mean radiusglobal mean
- 6.20kmCalculated measurementThe mean radius is about 0.0036 times the radius of Earth's Moon.
Irregular moons have no single true radius; the mean radius is an equal-volume comparison.
Published uncertainty: ± 0.24 km
JPL tabulated uncertainty for the adopted mean radius.
- Massglobal mean
- 1.44135E15kgCalculated measurementMass is not read from a scale. Motion under gravity constrains GM, from which mass is derived.
Calculated from JPL GM with a conventional gravitational constant, then rounded for display.
Approximate value
Derived from JPL's gravitational parameter GM and a conventional gravitational constant, then rounded.
- Mean densityglobal mean
- 1.4710g/cm³Calculated measurementA low bulk density points to a porous body rather than compact solid rock.
This is a whole-body average and cannot by itself prove the composition of every interior layer.
Published uncertainty: ± 0.166 g/cm³
JPL tabulated uncertainty for the adopted mean density.
- Reference gravitysurface
- 0.002503m/s²Calculated measurementRepresentative surface gravity is about 0.026% of Earth's.
Shape, terrain and local mass distribution make real gravity vary by location.
Approximate value
Calculated from the adopted GM and mean radius. Irregular shape and local terrain can change the actual value.
- Temperaturesurface
- -40°CScientific modelThe reference temperature is an orientation value; sunlight and darkness produce a broad range.
A small airless world heats and cools quickly, so one number cannot represent every place and time.
Approximate value
Representative surface estimate used for orientation. Temperature changes strongly with illumination, and the selected summary source does not publish a compact global uncertainty.
Orbit and rotation
- Average distancesystem reference
- 23,463kmCalculated measurementThis is a representative center-to-center distance between Deimos and Mars.
The real distance changes around an elliptical orbit.
Approximate value
Rounded orbital distance from the moon center to the planet center. The real orbit is not a perfect circle.
- Rotation periodrelative to distant stars
- 1.26244Earth daysCalculated measurementTidal locking makes one rotation take nearly the same time as one orbit around the planet.
This is a sidereal rotation, not a local sunrise-to-sunrise solar day.
Approximate value
Rounded synchronous rotation period. The same hemisphere normally faces the primary planet.
- Orbital periodrelative to distant stars
- 1.26244Earth daysCalculated measurementThis reports the time for one orbit, not a claim that the path is perfectly circular.
A rounded sidereal period is used for the beginner-facing display.
Approximate value
Rounded sidereal orbital period.
Atmosphere and inside
Atmosphere
Deimos has no persistent atmosphere and cannot retain released gas for long.
Surface and interior
The best beginner model is a porous interior beneath impact-churned debris, not a proven set of sharply separated layers.
- 1Porous rock-rich interior
Bulk density and orbit data are consistent with a porous body, but do not uniquely reveal how rock, voids and possible ice are arranged.
Scientific model - 2Impact-broken regolith
Repeated impacts have ground the outer material into loose blocks and fine dust.
Direct observation
How we know
Images constrain size, orbital and radio tracking constrain GM, and spectra and thermal emission constrain materials. Every number retains its method and limitation.
- 01Direct observation
Spacecraft imaging and shape reconstruction
Repeated views reveal the limb, terrain, crater record and the shape used to estimate size.
Where this method stops
Lighting, viewing angle and incomplete coverage can hide topography. A mosaic is not a single untouched photograph.
- 02Calculated measurement
Radio tracking and orbital dynamics
Engineers measure spacecraft motion and moon orbits, solve for GM, and then derive mass and gravity.
Where this method stops
The result depends on trajectory coverage and a dynamical model. Very small moons leave weaker gravitational signatures.
- 03Direct observation
Spectroscopy and thermal sensing
The spectrum and thermal glow constrain surface materials, gases and representative temperature.
Where this method stops
A spectrum samples the visible surface or atmosphere. It does not directly photograph deep interior layers.
Evidence key
- Direct observation
- An instrument or sample recorded the phenomenon, with processing still disclosed.
- Calculated measurement
- Observed motion or signal is converted into a physical quantity using equations and reference constants.
- Scientific model
- A tested interpretation that fits observations but is not directly imaged or sampled.
- Vastward explanation
- Original beginner-facing synthesis, traceable to the source records but not itself a measurement.
- Artist visualization
- An interpretive image, not observational evidence.
Missions and instruments
Mars Reconnaissance Orbiter
HiRISE obtained detailed images of Deimos from Mars orbit and improved its shape record.
Official mission ↗- HiRISE cameraImages the limb, terrain, color differences and time-dependent surface changes.
- Spacecraft radio scienceMeasures Doppler and range changes that constrain trajectory, gravity and mass.
- CRISM imaging spectrometerSeparates light by wavelength to constrain composition, gases and temperature.
Official source trail
Links below are the exact records used for this profile. Access dates are retained with the content.
- 01
NASA Science · official-page
Deimos
- Source updated
- No source update date published
- Access checked
- 2026-07-31
- 02
NASA Jet Propulsion Laboratory, Solar System Dynamics · dataset
Planetary Satellite Physical Parameters
- Source updated
- No source update date published
- Access checked
- 2026-07-31
- 03
NASA Science Photojournal · image
Martian Moon Deimos in High Resolution
- Source updated
- No source update date published
- Access checked
- 2026-07-31
- 04
NASA Science · official-page
Mars Reconnaissance Orbiter
- Source updated
- No source update date published
- Access checked
- 2026-07-31
Continue exploring
Atlas is a starting point. Use these relationships to move into explanation, experiment and mission thinking.
Understand moon systems
Place Deimos back inside Mars's moon system and connect orbit, tides and resonance.
academyCompare the major moons
Compare size, density, gravity and orbit without treating similar colors as identical composition.
lab