SpaceAtlas Space Object Data
NASA JPL SBDB · 325102

325102

325102 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.626 AU and a period of 0.50 yr.

Aten Observations: 175
Orbital Period · P
0.50 yr
v(q)
78.5 km/s
v(Q)
18 km/s
Diameter · ≈
0.33 km
TJ
8.85
Eccentricity · e
0.6268

Orbit and dynamics

Between its closest point (0.234 AU) and its farthest (1.019 AU), the heliocentric distance changes by 0.785 AU over every revolution.

One full revolution takes 0.50 yr (181 days), computed from the semi-major axis of 0.626 AU.

The high eccentricity (0.627) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 5.11° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 78.5 km/s at perihelion and falls to 18 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 0.36 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.124 points to a comparatively bright, reflective surface.

Observation record and orbit quality

Astrometry from 175 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3625 arcseconds.

Condition code U = 1 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
0.6262 AU
Eccentricity
0.6268
Perihelion
0.234 AU
Aphelion
1.018702 AU
Inclination
5.11°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
85.53°

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
2054-Mar-08 06:59 0.457920 AU
68503873 km
29.28 km/s
2055-Mar-06 11:56 0.411653 AU
61582351 km
27.47 km/s
2056-Mar-03 18:29 0.365549 AU
54685378 km
25.66 km/s
2057-Mar-02 03:56 0.319964 AU
47865986 km
23.90 km/s
2058-Feb-28 18:13 0.275503 AU
41214628 km
22.16 km/s
2059-Feb-27 13:40 0.232737 AU
34817031 km
20.43 km/s
2060-Feb-26 16:06 0.192364 AU
28777265 km
18.77 km/s
2061-Feb-25 05:11 0.155793 AU
23306367 km
17.20 km/s
2062-Feb-25 08:22 0.124781 AU
18666904 km
15.70 km/s
2063-Feb-26 07:52 0.102242 AU
15295167 km
14.39 km/s
2064-Feb-28 10:16 0.090413 AU
13525526 km
13.31 km/s
2065-Mar-02 20:06 0.087906 AU
13150514 km
12.54 km/s
2066-Mar-07 09:59 0.089441 AU
13380226 km
12.09 km/s
2067-Mar-12 16:54 0.089745 AU
13425679 km
11.96 km/s
2068-Mar-17 01:26 0.086486 AU
12938181 km
12.05 km/s
2069-Mar-21 19:05 0.080946 AU
12109417 km
12.45 km/s
2070-Mar-25 10:36 0.077951 AU
11661353 km
13.12 km/s
2071-Mar-27 19:53 0.084464 AU
12635635 km
14.16 km/s
2072-Mar-28 01:44 0.103518 AU
15486045 km
15.39 km/s
2073-Mar-28 10:12 0.132960 AU
19890495 km
16.85 km/s
2074-Mar-28 03:57 0.168837 AU
25257644 km
18.41 km/s
2075-Mar-27 10:30 0.208557 AU
31199730 km
20.03 km/s
2076-Mar-25 09:13 0.250772 AU
37514887 km
21.73 km/s
2077-Mar-24 02:53 0.294495 AU
44055827 km
23.45 km/s
2078-Mar-22 15:51 0.339025 AU
50717457 km
25.18 km/s
2079-Mar-21 01:34 0.384143 AU
57466932 km
26.96 km/s

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

Physical Parameters

Diameter
0.361 km
Albedo
0.124
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
20.17

Orbit Quality

RMS
0.36255
Condition
1
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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