SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 RG15

2012 RG15

2012 RG15 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.077 AU it takes 1.12 yr to circle the Sun.

Apollo Observations: 78
Orbital Period · P
1.12 yr
v(q)
46.8 km/s
v(Q)
17.6 km/s
Diameter · ≈
0.4 km
TJ
5.36
Eccentricity · e
0.4536

Orbit and dynamics

The path is an ellipse reaching 0.588 AU from the Sun at perihelion and 1.566 AU at aphelion, a radial span of 0.978 AU.

Applying Kepler's third law to a = 1.077 AU gives an orbital period of 1.12 yr, or about 408 days.

The high eccentricity (0.454) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 48.94° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 46.8 km/s at perihelion and falls to 17.6 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 = 19.76 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.4 km.

Observation record and orbit quality

The current orbit solution is based on 78 observations and has a weighted RMS residual of 0.3861 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
1.077 AU
Eccentricity
0.4536
Perihelion
0.588 AU
Aphelion
1.565527 AU
Inclination
48.94°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
170.71°

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-Mar-01 11:44 0.283065 AU
42345914 km
29.64 km/s
2031-Sep-02 05:29 0.098829 AU
14784591 km
28.99 km/s
2038-Feb-09 06:09 0.290207 AU
43414317 km
33.60 km/s
2040-Aug-23 05:37 0.214606 AU
32104555 km
24.37 km/s
2041-Sep-15 10:54 0.437939 AU
65514726 km
36.70 km/s
2048-Mar-03 20:09 0.303687 AU
45430960 km
29.38 km/s
2050-Sep-03 09:03 0.135272 AU
20236361 km
29.72 km/s
2057-Feb-11 22:53 0.267070 AU
39953072 km
32.84 km/s
2059-Aug-25 03:45 0.167887 AU
25115553 km
24.89 km/s
2060-Sep-17 06:49 0.483590 AU
72344014 km
37.89 km/s
2066-Jan-25 00:13 0.479784 AU
71774635 km
38.66 km/s
2067-Mar-08 17:21 0.340757 AU
50976552 km
29.06 km/s
2068-Aug-20 06:00 0.459050 AU
68672829 km
22.83 km/s
2069-Sep-05 09:22 0.192968 AU
28867653 km
30.92 km/s
2076-Feb-16 18:31 0.246440 AU
36866827 km
31.89 km/s
2078-Aug-26 17:28 0.103222 AU
15441719 km
25.73 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
19.76

Orbit Quality

RMS
0.38605
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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