SpaceAtlas Space Object Data
NASA JPL SBDB · 2005 RX3

2005 RX3

2005 RX3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.527 AU it takes 1.89 yr to circle the Sun.

Apollo Observations: 48
Orbital Period · P
1.89 yr
v(q)
43.4 km/s
v(Q)
13.4 km/s
Diameter · ≈
0.11 km
TJ
4.29
Eccentricity · e
0.5292

Orbit and dynamics

The path is an ellipse reaching 0.719 AU from the Sun at perihelion and 2.335 AU at aphelion, a radial span of 1.616 AU.

Applying Kepler's third law to a = 1.527 AU gives an orbital period of 1.89 yr, or about 689 days.

The high eccentricity (0.529) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 16.85° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 43.4 km/s at perihelion and falls to 13.4 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 = 22.54 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

The current orbit solution is based on 48 observations and has a weighted RMS residual of 0.521 arcseconds.

Condition code U = 0 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
1.527 AU
Eccentricity
0.5292
Perihelion
0.719 AU
Aphelion
2.335088 AU
Inclination
16.85°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
324.51°

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
2036-Mar-12 10:24 0.313602 AU
46914249 km
24.66 km/s
2037-Dec-15 04:08 0.359373 AU
53761493 km
13.26 km/s
2038-Mar-01 07:32 0.447905 AU
67005693 km
9.75 km/s
2039-Sep-10 20:12 0.156090 AU
23350784 km
20.90 km/s
2053-Mar-06 02:47 0.181462 AU
27146289 km
20.39 km/s
2054-Nov-16 23:30 0.332556 AU
49749644 km
13.49 km/s
2056-Sep-02 10:14 0.301483 AU
45101238 km
24.87 km/s
2070-Feb-28 09:18 0.117651 AU
17600326 km
16.56 km/s
2071-Oct-19 12:53 0.251704 AU
37654314 km
12.38 km/s
2073-Aug-26 23:43 0.433409 AU
64837053 km
28.58 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
22.54

Orbit Quality

RMS
0.52102
Condition
0
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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