SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 GA80

2013 GA80

2013 GA80 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.174 AU it takes 1.27 yr to circle the Sun.

Apollo Observations: 234
Orbital Period · P
1.27 yr
v(q)
32.1 km/s
v(Q)
23.6 km/s
Diameter · ≈
0.18 km
TJ
5.23
Eccentricity · e
0.1534

Orbit and dynamics

The path is an ellipse reaching 0.994 AU from the Sun at perihelion and 1.354 AU at aphelion, a radial span of 0.36 AU.

Applying Kepler's third law to a = 1.174 AU gives an orbital period of 1.27 yr, or about 465 days.

An eccentricity of 0.153 makes the orbit moderately elongated.

A steep inclination of 32.19° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 32.1 km/s at perihelion and falls to 23.6 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 = 21.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.18 km.

Observation record and orbit quality

The current orbit solution is based on 234 observations and has a weighted RMS residual of 0.2977 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
1.174 AU
Eccentricity
0.1534
Perihelion
0.994 AU
Aphelion
1.354092 AU
Inclination
32.19°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
155.2°

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-16 10:17 0.097624 AU
14604403 km
16.76 km/s
2031-Oct-24 05:25 0.302597 AU
45267935 km
15.96 km/s
2032-May-03 16:40 0.426035 AU
63733969 km
22.41 km/s
2040-Nov-05 17:00 0.435221 AU
65108145 km
18.72 km/s
2041-Apr-13 04:09 0.190835 AU
28548479 km
16.94 km/s
2045-Oct-26 11:59 0.281029 AU
42041323 km
16.03 km/s
2046-Apr-30 11:15 0.327733 AU
49028205 km
20.64 km/s
2050-Oct-09 23:48 0.482621 AU
72199070 km
16.11 km/s
2055-Apr-10 20:17 0.296640 AU
44376655 km
17.62 km/s
2059-Oct-29 17:47 0.277028 AU
41442824 km
16.25 km/s
2060-Apr-26 02:45 0.222052 AU
33218553 km
19.02 km/s
2064-Oct-13 15:52 0.429859 AU
64306025 km
16.08 km/s
2069-Apr-07 21:15 0.399706 AU
59795110 km
18.69 km/s
2073-Oct-31 14:03 0.293845 AU
43958548 km
16.58 km/s
2074-Apr-23 02:52 0.122654 AU
18348786 km
17.85 km/s
2078-Oct-17 13:12 0.385216 AU
57627549 km
16.01 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
21.5

Orbit Quality

RMS
0.29773
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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