SpaceAtlas Space Object Data
NASA JPL SBDB · 373135

373135

373135 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.653 AU it takes 2.13 yr to circle the Sun.

Apollo Observations: 217
Orbital Period · P
2.13 yr
v(q)
40 km/s
v(Q)
13.4 km/s
Diameter · ≈
0.44 km
TJ
4.12
Eccentricity · e
0.4975

Orbit and dynamics

Between its closest point (0.83 AU) and its farthest (2.475 AU), the heliocentric distance changes by 1.645 AU over every revolution.

One full revolution takes 2.13 yr (776 days), computed from the semi-major axis of 1.653 AU.

The high eccentricity (0.497) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.39° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 40 km/s at perihelion and falls to 13.4 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

Size and surface

The measured diameter is 1.05 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.025 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

Astrometry from 217 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5921 arcseconds.

Condition code U = 0 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

About these computed values

Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Orbital Parameters

Semi-Major Axis
1.653 AU
Eccentricity
0.4975
Perihelion
0.83 AU
Aphelion
2.475367 AU
Inclination
4.39°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
40.99°

Orbit diagram

The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.

3D orbit (interactive)

Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.

Close approaches

Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).

Date (UTC)Miss distanceVelocity
2028-Mar-14 01:59 0.488282 AU
73045945 km
27.24 km/s
2030-Jun-03 18:48 0.189122 AU
28292323 km
10.64 km/s
2032-Sep-11 01:32 0.384968 AU
57590320 km
23.90 km/s
2047-May-31 02:37 0.184478 AU
27597498 km
10.54 km/s
2049-Sep-10 18:45 0.368835 AU
55176982 km
23.42 km/s
2064-May-25 02:49 0.177108 AU
26494986 km
10.39 km/s
2066-Sep-09 18:21 0.343325 AU
51360633 km
22.63 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
1.05 km
Albedo
0.025
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.52

Orbit Quality

RMS
0.59206
Condition
0
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.