SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 PK25

2017 PK25

2017 PK25 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.814 AU and a period of 0.73 yr.

Aten Observations: 14
Orbital Period · P
0.73 yr
v(q)
52.8 km/s
v(Q)
20.7 km/s
Diameter · ≈
0.03 km
TJ
7.03
Eccentricity · e
0.4371

Orbit and dynamics

Between its closest point (0.458 AU) and its farthest (1.17 AU), the heliocentric distance changes by 0.712 AU over every revolution.

One full revolution takes 0.73 yr (268 days), computed from the semi-major axis of 0.814 AU.

The high eccentricity (0.437) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 25.87° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 52.8 km/s at perihelion and falls to 20.7 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 = 25.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 14 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5066 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
0.8139 AU
Eccentricity
0.4371
Perihelion
0.458 AU
Aphelion
1.169656 AU
Inclination
25.87°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
259.41°

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
2028-Feb-28 21:34 0.471048 AU
70467816 km
23.73 km/s
2028-Aug-13 13:51 0.054021 AU
8081475 km
14.79 km/s
2031-Aug-08 06:53 0.243635 AU
36447251 km
22.52 km/s
2036-Apr-24 12:52 0.444112 AU
66438236 km
14.43 km/s
2036-Jul-11 22:20 0.367009 AU
54903746 km
13.72 km/s
2039-Mar-10 06:58 0.461356 AU
69017867 km
22.29 km/s
2039-Aug-11 17:21 0.126612 AU
18940915 km
13.87 km/s
2042-Aug-11 01:32 0.138185 AU
20672177 km
20.04 km/s
2047-Jun-29 23:29 0.401892 AU
60122134 km
13.80 km/s
2050-Mar-20 05:20 0.454599 AU
68007083 km
20.61 km/s
2050-Aug-06 04:09 0.199690 AU
29873154 km
13.55 km/s
2053-Feb-12 15:17 0.487976 AU
73000153 km
25.69 km/s
2053-Aug-13 04:30 0.037078 AU
5546846 km
17.72 km/s
2056-Aug-01 11:05 0.382600 AU
57236112 km
27.17 km/s
2058-Jun-14 06:48 0.431309 AU
64522902 km
14.52 km/s
2061-Mar-30 10:00 0.450114 AU
67336133 km
18.83 km/s
2061-Jul-29 22:40 0.263789 AU
39462318 km
13.57 km/s
2064-Feb-21 09:42 0.478185 AU
71535398 km
24.77 km/s
2064-Aug-13 23:22 0.006331 AU
947147 km
16.06 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
25.3

Orbit Quality

RMS
0.50658
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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