SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 SO10

2017 SO10

2017 SO10 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: 54
Orbital Period · P
1.24 yr
v(q)
38.3 km/s
v(Q)
20 km/s
Diameter · ≈
0.04 km
TJ
5.39
Eccentricity · e
0.3129

Orbit and dynamics

Between its closest point (0.795 AU) and its farthest (1.519 AU), the heliocentric distance changes by 0.724 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 0.313 makes the orbit moderately elongated.

The orbital plane is tilted 5.5° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 38.3 km/s at perihelion and falls to 20 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 = 24.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 54 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3316 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
0.3129
Perihelion
0.795 AU
Aphelion
1.519025 AU
Inclination
5.5°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
299.81°

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
2027-Sep-21 08:25 0.218842 AU
32738364 km
15.85 km/s
2032-Sep-14 01:13 0.347976 AU
52056510 km
19.89 km/s
2034-Apr-08 01:31 0.417616 AU
62474476 km
22.10 km/s
2039-Apr-01 16:29 0.274155 AU
41012963 km
18.11 km/s
2043-Jul-13 01:00 0.491566 AU
73537264 km
9.10 km/s
2044-Mar-25 05:22 0.134853 AU
20173708 km
14.20 km/s
2048-Jul-22 03:39 0.463979 AU
69410231 km
8.77 km/s
2049-Mar-18 02:02 0.010876 AU
1627059 km
10.37 km/s
2053-Jul-31 03:58 0.447416 AU
66932506 km
8.41 km/s
2054-Mar-10 00:22 0.053053 AU
7936671 km
7.53 km/s
2058-Aug-10 03:07 0.395225 AU
59124852 km
7.87 km/s
2063-Aug-22 11:11 0.317894 AU
47556298 km
7.06 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
24.6

Orbit Quality

RMS
0.33164
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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