SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 AM10

2019 AM10

2019 AM10 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.157 AU it takes 1.24 yr to circle the Sun.

Apollo Observations: 48
Orbital Period · P
1.24 yr
v(q)
31.7 km/s
v(Q)
24.2 km/s
Diameter · ≈
0.03 km
TJ
5.43
Eccentricity · e
0.1352

Orbit and dynamics

Between its closest point (1.001 AU) and its farthest (1.313 AU), the heliocentric distance changes by 0.312 AU over every revolution.

One full revolution takes 1.24 yr (455 days), computed from the semi-major axis of 1.157 AU.

An eccentricity of 0.135 makes the orbit moderately elongated.

The orbital plane is tilted 6.15° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 31.7 km/s at perihelion and falls to 24.2 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 25.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 48 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4294 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.157 AU
Eccentricity
0.1352
Perihelion
1.001 AU
Aphelion
1.313426 AU
Inclination
6.15°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
0.4°

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-Nov-17 07:02 0.226550 AU
33891326 km
7.79 km/s
2029-Mar-17 21:52 0.207089 AU
30980109 km
3.08 km/s
2033-Oct-30 23:38 0.360619 AU
53947772 km
12.41 km/s
2034-Apr-21 03:48 0.266608 AU
39883927 km
4.08 km/s
2039-May-16 12:56 0.298386 AU
44637891 km
4.92 km/s
2044-Jun-06 05:13 0.309995 AU
46374557 km
5.42 km/s
2049-Jun-26 11:29 0.299681 AU
44831657 km
5.62 km/s
2054-Jul-16 05:43 0.275329 AU
41188606 km
5.49 km/s
2059-Aug-05 22:44 0.238644 AU
35700660 km
5.06 km/s
2060-Feb-01 00:59 0.340862 AU
50992294 km
13.34 km/s
2064-Aug-28 07:44 0.193417 AU
28934728 km
4.20 km/s
2065-Jan-24 21:50 0.191682 AU
28675175 km
9.11 km/s
2070-Jan-19 16:20 0.066489 AU
9946588 km
5.58 km/s
2075-Jan-17 01:53 0.039273 AU
5875228 km
3.83 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
25.2

Orbit Quality

RMS
0.42939
Condition
6
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

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