SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 RO36

2015 RO36

2015 RO36 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.166 AU it takes 1.26 yr to circle the Sun.

Apollo Observations: 120
Orbital Period · P
1.26 yr
v(q)
43.9 km/s
v(Q)
17.3 km/s
Diameter · ≈
0.09 km
TJ
5.26
Eccentricity · e
0.434

Orbit and dynamics

The path is an ellipse reaching 0.66 AU from the Sun at perihelion and 1.672 AU at aphelion, a radial span of 1.012 AU.

Applying Kepler's third law to a = 1.166 AU gives an orbital period of 1.26 yr, or about 460 days.

The high eccentricity (0.434) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 20.33° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 43.9 km/s at perihelion and falls to 17.3 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 = 22.93 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

The current orbit solution is based on 120 observations and has a weighted RMS residual of 0.3322 arcseconds.

Condition code U = 1 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
1.166 AU
Eccentricity
0.434
Perihelion
0.66 AU
Aphelion
1.672044 AU
Inclination
20.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
243.66°

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-Apr-04 16:55 0.323017 AU
48322723 km
13.05 km/s
2034-May-14 23:38 0.436875 AU
65355603 km
14.68 km/s
2039-Jun-20 12:08 0.449310 AU
67215747 km
13.84 km/s
2044-Aug-31 09:54 0.324974 AU
48615453 km
11.03 km/s
2048-Feb-10 04:29 0.374339 AU
56000268 km
27.10 km/s
2049-Sep-06 07:38 0.100964 AU
15103932 km
14.78 km/s
2053-Feb-19 21:09 0.171099 AU
25596052 km
21.23 km/s
2054-Sep-15 04:55 0.107549 AU
16089058 km
19.74 km/s
2058-Mar-03 23:40 0.088959 AU
13308129 km
16.05 km/s
2059-Sep-24 16:05 0.319630 AU
47816012 km
25.46 km/s
2063-Mar-26 20:24 0.282581 AU
42273447 km
12.84 km/s
2068-May-07 03:01 0.422384 AU
63187679 km
14.47 km/s
2073-Jun-12 04:10 0.455106 AU
68082827 km
14.29 km/s
2078-Sep-03 15:18 0.365612 AU
54694744 km
10.77 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
22.93

Orbit Quality

RMS
0.33215
Condition
1
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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