SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 SX1

2016 SX1

2016 SX1 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.879 AU and a period of 0.82 yr.

Aten Observations: 43
Orbital Period · P
0.82 yr
v(q)
36.8 km/s
v(Q)
27.4 km/s
Diameter · ≈
0.01 km
TJ
6.73
Eccentricity · e
0.1466

Orbit and dynamics

The path is an ellipse reaching 0.75 AU from the Sun at perihelion and 1.008 AU at aphelion, a radial span of 0.258 AU.

Applying Kepler's third law to a = 0.879 AU gives an orbital period of 0.82 yr, or about 301 days.

An eccentricity of 0.147 makes the orbit moderately elongated.

Its inclination of 2.62° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36.8 km/s at perihelion and falls to 27.4 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 = 28.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 43 observations and has a weighted RMS residual of 0.3755 arcseconds.

Condition code U = 5 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
0.879 AU
Eccentricity
0.1466
Perihelion
0.75 AU
Aphelion
1.007861 AU
Inclination
2.62°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
101.41°

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
2030-Sep-03 17:18 0.031159 AU
4661315 km
3.70 km/s
2035-Jun-07 11:55 0.188175 AU
28150517 km
4.06 km/s
2035-Oct-28 04:41 0.142721 AU
21350825 km
7.38 km/s
2040-Apr-16 06:04 0.238615 AU
35696363 km
6.72 km/s
2040-Oct-19 01:42 0.369895 AU
55335480 km
14.92 km/s
2044-Sep-03 14:14 0.310645 AU
46471847 km
13.47 km/s
2045-Mar-04 09:41 0.231294 AU
34601024 km
6.69 km/s
2049-Aug-29 10:26 0.073265 AU
10960361 km
6.32 km/s
2054-Oct-22 06:14 0.016600 AU
2483379 km
3.41 km/s
2059-Oct-20 06:28 0.313870 AU
46954226 km
14.28 km/s
2063-Sep-03 08:46 0.094055 AU
14070430 km
10.09 km/s
2077-Aug-31 13:23 0.101837 AU
15234603 km
8.12 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
28.6

Orbit Quality

RMS
0.37546
Condition
5
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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