SpaceAtlas Space Object Data
NASA JPL SBDB · 513358

513358

513358 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.868 AU it takes 2.55 yr to circle the Sun.

Apollo Observations: 92
Orbital Period · P
2.55 yr
v(q)
43.2 km/s
v(Q)
11 km/s
Diameter · ≈
0.39 km
TJ
3.66
Eccentricity · e
0.5943

Orbit and dynamics

Between its closest point (0.758 AU) and its farthest (2.978 AU), the heliocentric distance changes by 2.22 AU over every revolution.

One full revolution takes 2.55 yr (933 days), computed from the semi-major axis of 1.868 AU.

The high eccentricity (0.594) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 25.03° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 43.2 km/s at perihelion and falls to 11 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

No direct size measurement is available; from an absolute magnitude of H = 19.8 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.39 km.

Observation record and orbit quality

Astrometry from 92 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5012 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
1.868 AU
Eccentricity
0.5943
Perihelion
0.758 AU
Aphelion
2.978152 AU
Inclination
25.03°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
38.41°

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
2031-Feb-21 10:59 0.355816 AU
53229260 km
28.89 km/s
2036-Mar-17 01:51 0.377262 AU
56437531 km
13.79 km/s
2041-Aug-16 14:34 0.094205 AU
14092863 km
21.17 km/s
2054-Feb-15 21:19 0.472533 AU
70690001 km
32.29 km/s
2059-Mar-14 03:28 0.259244 AU
38782366 km
15.98 km/s
2064-Aug-11 03:50 0.123231 AU
18435086 km
18.66 km/s

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

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.8

Orbit Quality

RMS
0.50117
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.