SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 SW10

2019 SW10

2019 SW10 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.286 AU it takes 1.46 yr to circle the Sun.

Apollo Observations: 28
Orbital Period · P
1.46 yr
v(q)
49.6 km/s
v(Q)
13.9 km/s
Diameter · ≈
0.07 km
TJ
4.87
Eccentricity · e
0.5626

Orbit and dynamics

Between its closest point (0.563 AU) and its farthest (2.01 AU), the heliocentric distance changes by 1.447 AU over every revolution.

One full revolution takes 1.46 yr (533 days), computed from the semi-major axis of 1.286 AU.

The high eccentricity (0.563) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.48° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 49.6 km/s at perihelion and falls to 13.9 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 = 23.38 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.07 km.

Observation record and orbit quality

Astrometry from 28 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4138 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.286 AU
Eccentricity
0.5626
Perihelion
0.563 AU
Aphelion
2.009504 AU
Inclination
1.48°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
156.65°

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-May-28 04:46 0.251475 AU
37620118 km
26.42 km/s
2030-May-02 07:07 0.101031 AU
15114006 km
11.58 km/s
2038-Oct-17 04:04 0.042139 AU
6303869 km
19.14 km/s
2046-May-24 06:18 0.172010 AU
25732314 km
24.07 km/s
2049-Apr-28 12:35 0.168183 AU
25159749 km
10.55 km/s
2052-Feb-14 04:44 0.411554 AU
61567605 km
18.83 km/s
2054-Oct-09 12:55 0.469052 AU
70169229 km
9.63 km/s
2054-Dec-25 05:38 0.375141 AU
56120333 km
16.25 km/s
2057-Oct-21 23:45 0.034251 AU
5123833 km
16.16 km/s
2060-Oct-01 01:50 0.373470 AU
55870347 km
29.25 km/s
2065-Jun-02 06:33 0.376120 AU
56266785 km
29.93 km/s
2068-May-12 16:47 0.021586 AU
3229206 km
17.23 km/s
2079-Oct-13 12:27 0.059367 AU
8881203 km
21.82 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
23.38

Orbit Quality

RMS
0.41385
Condition
7
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.