SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 WT28

2017 WT28

2017 WT28 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.9 AU and a period of 0.85 yr.

Aten Observations: 28
Orbital Period · P
0.85 yr
v(q)
35.9 km/s
v(Q)
27.5 km/s
Diameter · ≈
0.01 km
TJ
6.6
Eccentricity · e
0.1315

Orbit and dynamics

The path is an ellipse reaching 0.781 AU from the Sun at perihelion and 1.018 AU at aphelion, a radial span of 0.237 AU.

Applying Kepler's third law to a = 0.9 AU gives an orbital period of 0.85 yr, or about 312 days.

An eccentricity of 0.132 makes the orbit moderately elongated.

The orbital plane is tilted 5.76° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35.9 km/s at perihelion and falls to 27.5 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 = 28.1 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 28 observations and has a weighted RMS residual of 0.439 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
0.8997 AU
Eccentricity
0.1315
Perihelion
0.781 AU
Aphelion
1.018011 AU
Inclination
5.76°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
134.25°

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
2029-Aug-10 01:23 0.229226 AU
34291709 km
5.75 km/s
2030-Feb-09 12:15 0.187187 AU
28002845 km
8.72 km/s
2034-Nov-28 18:55 0.391721 AU
58600593 km
16.36 km/s
2035-Jul-05 13:51 0.242270 AU
36243117 km
7.01 km/s
2036-Feb-04 10:14 0.352612 AU
52749935 km
14.47 km/s
2040-Nov-22 14:17 0.207776 AU
31082919 km
10.71 km/s
2041-May-31 21:54 0.221125 AU
33079902 km
6.78 km/s
2046-Nov-21 21:35 0.025535 AU
3820010 km
5.37 km/s
2047-Apr-24 22:51 0.172671 AU
25831274 km
5.07 km/s
2052-Nov-29 03:00 0.006917 AU
1034696 km
4.02 km/s
2053-Apr-02 13:39 0.142877 AU
21374152 km
3.81 km/s
2059-Feb-08 08:40 0.098302 AU
14705795 km
5.22 km/s
2063-Dec-02 04:30 0.404407 AU
60498403 km
19.21 km/s
2065-Feb-06 11:41 0.190167 AU
28448625 km
11.72 km/s
2069-Nov-24 08:51 0.138160 AU
20668386 km
12.45 km/s
2071-Jan-29 18:36 0.357565 AU
53490899 km
18.73 km/s
2075-Nov-21 05:52 0.004221 AU
631512 km
5.97 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
28.1

Orbit Quality

RMS
0.43897
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.

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