SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 JR7

2013 JR7

2013 JR7 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.249 AU it takes 1.40 yr to circle the Sun.

Apollo Observations: 7
Orbital Period · P
1.40 yr
v(q)
33.4 km/s
v(Q)
21.3 km/s
Diameter · ≈
0.02 km
TJ
5.11
Eccentricity · e
0.2221

Orbit and dynamics

The path is an ellipse reaching 0.971 AU from the Sun at perihelion and 1.526 AU at aphelion, a radial span of 0.555 AU.

Applying Kepler's third law to a = 1.249 AU gives an orbital period of 1.40 yr, or about 510 days.

An eccentricity of 0.222 makes the orbit moderately elongated.

The orbital plane is tilted 9.11° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.4 km/s at perihelion and falls to 21.3 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 = 26.8 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 7 observations and has a weighted RMS residual of 0.8299 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
1.249 AU
Eccentricity
0.2221
Perihelion
0.971 AU
Aphelion
1.526403 AU
Inclination
9.11°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
101.19°

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
2027-Apr-28 08:07 0.020224 AU
3025408 km
11.10 km/s
2034-Apr-19 20:22 0.197910 AU
29606861 km
15.49 km/s
2034-Oct-30 16:10 0.366285 AU
54795486 km
7.83 km/s
2041-Apr-11 14:58 0.396565 AU
59325314 km
20.22 km/s
2041-Nov-12 19:39 0.438085 AU
65536569 km
8.57 km/s
2045-Feb-12 10:26 0.456504 AU
68292040 km
7.28 km/s
2045-Sep-11 12:50 0.392992 AU
58790818 km
18.03 km/s
2052-Mar-02 05:41 0.397601 AU
59480231 km
6.10 km/s
2052-Sep-03 18:50 0.276120 AU
41307012 km
13.23 km/s
2059-Mar-31 03:34 0.320918 AU
48008628 km
4.62 km/s
2059-Aug-27 05:58 0.191184 AU
28600764 km
8.60 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
26.8

Orbit Quality

RMS
0.82992
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.

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