SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 FX7

2013 FX7

2013 FX7 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.266 AU it takes 1.42 yr to circle the Sun.

Apollo Observations: 132
Orbital Period · P
1.42 yr
v(q)
36.5 km/s
v(Q)
19.2 km/s
Diameter · ≈
0.17 km
TJ
5.04
Eccentricity · e
0.3097

Orbit and dynamics

The path is an ellipse reaching 0.874 AU from the Sun at perihelion and 1.658 AU at aphelion, a radial span of 0.784 AU.

Applying Kepler's third law to a = 1.266 AU gives an orbital period of 1.42 yr, or about 520 days.

An eccentricity of 0.31 makes the orbit moderately elongated.

The orbital plane is tilted 5.22° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 36.5 km/s at perihelion and falls to 19.2 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 = 21.63 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.17 km.

Observation record and orbit quality

The current orbit solution is based on 132 observations and has a weighted RMS residual of 0.4151 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
1.266 AU
Eccentricity
0.3097
Perihelion
0.874 AU
Aphelion
1.65808 AU
Inclination
5.22°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
68.48°

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
2030-Jan-21 00:46 0.478885 AU
71640112 km
7.84 km/s
2030-Aug-02 11:15 0.099452 AU
14877808 km
9.44 km/s
2033-Feb-25 17:02 0.398885 AU
59672396 km
20.25 km/s
2040-Feb-11 20:37 0.375443 AU
56165499 km
5.48 km/s
2040-Jun-19 18:02 0.140140 AU
20964677 km
7.00 km/s
2050-Apr-27 01:41 0.120489 AU
18024824 km
7.19 km/s
2050-Sep-06 03:05 0.365290 AU
54646577 km
5.78 km/s
2057-Aug-23 04:54 0.408914 AU
61172692 km
20.04 km/s
2060-Mar-20 00:16 0.054434 AU
8143151 km
9.42 km/s
2060-Sep-24 23:37 0.462790 AU
69232343 km
7.87 km/s
2067-Aug-12 04:34 0.193237 AU
28907788 km
13.35 km/s
2070-Mar-04 03:54 0.280267 AU
41927373 km
16.68 km/s
2077-Jan-30 17:44 0.429081 AU
64189671 km
6.82 km/s
2077-Jul-18 14:14 0.108208 AU
16187634 km
6.80 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
21.63

Orbit Quality

RMS
0.41513
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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