SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 WP28

2017 WP28

2017 WP28 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.176 AU it takes 1.28 yr to circle the Sun.

Apollo Observations: 57
Orbital Period · P
1.28 yr
v(q)
82.6 km/s
v(Q)
9.1 km/s
Diameter · ≈
0.23 km
TJ
4.99
Eccentricity · e
0.8009

Orbit and dynamics

The path is an ellipse reaching 0.234 AU from the Sun at perihelion and 2.118 AU at aphelion, a radial span of 1.884 AU.

Applying Kepler's third law to a = 1.176 AU gives an orbital period of 1.28 yr, or about 466 days.

The high eccentricity (0.801) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 10.08° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 82.6 km/s at perihelion and falls to 9.1 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 = 20.92 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.23 km.

Observation record and orbit quality

The current orbit solution is based on 57 observations and has a weighted RMS residual of 0.5627 arcseconds.

Condition code U = 1 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

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
1.176 AU
Eccentricity
0.8009
Perihelion
0.234 AU
Aphelion
2.117858 AU
Inclination
10.08°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
292.69°

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-Feb-05 08:36 0.160269 AU
23975842 km
25.56 km/s
2031-Nov-18 03:11 0.247779 AU
37067265 km
35.30 km/s
2038-Jan-19 01:01 0.374349 AU
56001870 km
39.47 km/s
2040-Nov-02 08:34 0.239658 AU
35852302 km
22.24 km/s
2043-Feb-09 06:58 0.261349 AU
39097190 km
21.91 km/s
2045-Nov-23 15:06 0.370705 AU
55456734 km
39.70 km/s
2052-Jan-25 10:17 0.258795 AU
38715188 km
35.16 km/s
2054-Nov-06 06:13 0.134574 AU
20131959 km
25.77 km/s
2057-Feb-09 09:01 0.375895 AU
56233022 km
19.34 km/s
2059-Nov-29 19:52 0.484216 AU
72437694 km
43.85 km/s
2066-Jan-30 05:57 0.165140 AU
24704579 km
31.11 km/s
2068-Nov-10 04:32 0.112822 AU
16878005 km
29.45 km/s
2071-Feb-07 07:45 0.483218 AU
72288312 km
18.27 km/s
2077-Nov-02 23:24 0.415343 AU
62134389 km
18.84 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
20.92

Orbit Quality

RMS
0.56273
Condition
1
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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