SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 RB5

2025 RB5

2025 RB5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.019 AU it takes 1.03 yr to circle the Sun.

Apollo Observations: 37
Orbital Period · P
1.03 yr
v(q)
35.5 km/s
v(Q)
24.5 km/s
Diameter · ≈
0.04 km
TJ
5.97
Eccentricity · e
0.1821

Orbit and dynamics

Between its closest point (0.833 AU) and its farthest (1.205 AU), the heliocentric distance changes by 0.372 AU over every revolution.

One full revolution takes 1.03 yr (376 days), computed from the semi-major axis of 1.019 AU.

An eccentricity of 0.182 makes the orbit moderately elongated.

Its inclination of 4.74° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 35.5 km/s at perihelion and falls to 24.5 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 = 24.64 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 37 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5316 arcseconds.

Condition code U = 2 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
1.019 AU
Eccentricity
0.1821
Perihelion
0.833 AU
Aphelion
1.20456 AU
Inclination
4.74°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
359.44°

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
2057-Feb-11 02:41 0.108761 AU
16270412 km
8.64 km/s
2058-Mar-07 05:49 0.097731 AU
14620414 km
4.62 km/s
2059-Apr-27 04:34 0.171641 AU
25677078 km
6.18 km/s
2060-Jun-06 21:16 0.184229 AU
27560337 km
5.96 km/s
2060-Oct-18 06:51 0.192103 AU
28738157 km
5.42 km/s
2061-Sep-07 20:38 0.102228 AU
15293109 km
4.29 km/s
2062-Aug-31 03:58 0.096441 AU
14427340 km
8.30 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
24.64

Orbit Quality

RMS
0.53158
Condition
2
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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