SpaceAtlas Space Object Data
NASA JPL SBDB · 523598

523598

523598 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.416 AU it takes 1.68 yr to circle the Sun.

Apollo Observations: 158
Orbital Period · P
1.68 yr
v(q)
46.2 km/s
v(Q)
13.5 km/s
Diameter · ≈
0.25 km
TJ
4.4
Eccentricity · e
0.5468

Orbit and dynamics

Between its closest point (0.642 AU) and its farthest (2.19 AU), the heliocentric distance changes by 1.548 AU over every revolution.

One full revolution takes 1.68 yr (615 days), computed from the semi-major axis of 1.416 AU.

The high eccentricity (0.547) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 33.73° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 46.2 km/s at perihelion and falls to 13.5 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 = 20.77 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.25 km.

Observation record and orbit quality

Astrometry from 158 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4907 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
1.416 AU
Eccentricity
0.5468
Perihelion
0.642 AU
Aphelion
2.190269 AU
Inclination
33.73°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
249.61°

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-Oct-06 05:35 0.377373 AU
56454150 km
33.21 km/s
2030-Mar-08 21:53 0.176328 AU
26378278 km
28.06 km/s
2035-Mar-22 22:10 0.174811 AU
26151321 km
20.65 km/s
2045-Aug-16 12:00 0.487318 AU
72901761 km
17.46 km/s
2050-Sep-12 02:35 0.142883 AU
21375000 km
21.50 km/s
2055-Sep-28 16:54 0.203422 AU
30431483 km
28.76 km/s
2057-Mar-01 01:16 0.353545 AU
52889629 km
32.63 km/s
2062-Mar-15 12:24 0.031126 AU
4656369 km
24.34 km/s
2067-Mar-27 14:08 0.318923 AU
47710196 km
18.45 km/s
2077-Aug-28 02:02 0.387452 AU
57961955 km
18.10 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
20.77

Orbit Quality

RMS
0.49073
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.

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