SpaceAtlas Space Object Data
NASA JPL SBDB · 612443

612443

612443 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.967 AU and a period of 0.95 yr.

Aten Observations: 281
Orbital Period · P
0.95 yr
v(q)
41.7 km/s
v(Q)
22 km/s
Diameter · ≈
0.22 km
TJ
6.18
Eccentricity · e
0.3098

Orbit and dynamics

The path is an ellipse reaching 0.667 AU from the Sun at perihelion and 1.266 AU at aphelion, a radial span of 0.599 AU.

Applying Kepler's third law to a = 0.967 AU gives an orbital period of 0.95 yr, or about 347 days.

An eccentricity of 0.31 makes the orbit moderately elongated.

The orbital plane is tilted 13.54° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 41.7 km/s at perihelion and falls to 22 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 = 21.06 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.22 km.

Observation record and orbit quality

The current orbit solution is based on 281 observations and has a weighted RMS residual of 0.61 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
0.9667 AU
Eccentricity
0.3098
Perihelion
0.667 AU
Aphelion
1.266184 AU
Inclination
13.54°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
210.29°

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
2037-Jun-24 12:43 0.387796 AU
58013437 km
18.12 km/s
2038-Jun-06 14:49 0.237563 AU
35538918 km
9.47 km/s
2039-Apr-08 15:04 0.282801 AU
42306451 km
11.89 km/s
2039-Aug-04 00:06 0.285150 AU
42657809 km
8.86 km/s
2040-Feb-27 02:13 0.322123 AU
48188912 km
14.02 km/s
2040-Sep-06 04:11 0.248349 AU
37152504 km
9.41 km/s
2041-Jan-16 12:02 0.333363 AU
49870330 km
12.03 km/s
2041-Oct-07 19:33 0.148844 AU
22266806 km
9.43 km/s
2042-Oct-12 23:19 0.265813 AU
39765101 km
16.06 km/s
2056-Jun-25 07:28 0.401950 AU
60130885 km
18.65 km/s
2057-Jun-08 08:29 0.238976 AU
35750263 km
9.90 km/s
2058-Apr-10 22:05 0.280339 AU
41938187 km
11.67 km/s
2058-Aug-01 17:44 0.284318 AU
42533302 km
8.78 km/s
2059-Feb-28 21:07 0.320492 AU
47944929 km
13.99 km/s
2059-Sep-05 10:35 0.251612 AU
37640609 km
9.42 km/s
2060-Jan-19 11:36 0.333867 AU
49945752 km
12.25 km/s
2060-Oct-06 09:43 0.152684 AU
22841182 km
9.34 km/s
2061-Oct-13 03:03 0.255121 AU
38165582 km
15.68 km/s
2075-Jun-27 04:59 0.418495 AU
62605940 km
19.26 km/s
2076-Jun-10 00:11 0.242127 AU
36221728 km
10.48 km/s
2077-Apr-14 07:06 0.276708 AU
41394989 km
11.36 km/s
2077-Jul-29 08:03 0.283310 AU
42382528 km
8.65 km/s
2078-Mar-03 20:16 0.317942 AU
47563520 km
13.94 km/s
2078-Sep-02 13:01 0.257908 AU
38582454 km
9.43 km/s
2079-Jan-23 05:26 0.334532 AU
50045315 km
12.63 km/s
2079-Oct-04 13:25 0.162034 AU
24239929 km
9.21 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
21.06

Orbit Quality

RMS
0.61002
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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