SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 RX2

2017 RX2

2017 RX2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.741 AU and a period of 0.64 yr.

Aten Observations: 43
Orbital Period · P
0.64 yr
v(q)
63.7 km/s
v(Q)
18.8 km/s
Diameter · ≈
0.02 km
TJ
7.65
Eccentricity · e
0.5444

Orbit and dynamics

Between its closest point (0.338 AU) and its farthest (1.145 AU), the heliocentric distance changes by 0.807 AU over every revolution.

One full revolution takes 0.64 yr (233 days), computed from the semi-major axis of 0.741 AU.

The high eccentricity (0.544) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.69° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 63.7 km/s at perihelion and falls to 18.8 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 = 26.55 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 43 individual observations underpins this orbit; the fit leaves an RMS residual of 0.2852 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
0.7413 AU
Eccentricity
0.5444
Perihelion
0.338 AU
Aphelion
1.144864 AU
Inclination
1.69°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
130.99°

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-Jul-25 11:59 0.126276 AU
18890663 km
17.78 km/s
2031-Aug-27 14:55 0.129472 AU
19368798 km
10.67 km/s
2038-Aug-09 05:27 0.112247 AU
16791912 km
10.74 km/s
2040-Sep-19 14:57 0.084905 AU
12701681 km
15.93 km/s
2045-Jul-27 04:25 0.045922 AU
6869907 km
11.95 km/s
2047-Sep-19 09:37 0.012293 AU
1839077 km
12.59 km/s
2052-Jul-23 23:27 0.081736 AU
12227504 km
15.57 km/s
2054-Sep-05 00:12 0.113191 AU
16933191 km
10.74 km/s
2061-Aug-14 02:47 0.127952 AU
19141418 km
10.70 km/s
2063-Sep-19 20:13 0.123222 AU
18433702 km
17.00 km/s
2068-Jul-28 01:59 0.057630 AU
8621282 km
11.64 km/s
2070-Sep-19 13:25 0.005680 AU
849726 km
12.86 km/s
2075-Jul-25 11:24 0.137884 AU
20627089 km
17.56 km/s
2077-Aug-22 15:53 0.134670 AU
20146324 km
10.66 km/s
2079-Sep-19 01:07 0.144051 AU
21549677 km
18.01 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
26.55

Orbit Quality

RMS
0.28522
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

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