SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 GD50

2014 GD50

2014 GD50 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.763 AU it takes 2.34 yr to circle the Sun.

Apollo Observations: 331
Orbital Period · P
2.34 yr
v(q)
40.1 km/s
v(Q)
12.6 km/s
Diameter · ≈
0.34 km
TJ
3.76
Eccentricity · e
0.523

Orbit and dynamics

The path is an ellipse reaching 0.841 AU from the Sun at perihelion and 2.685 AU at aphelion, a radial span of 1.844 AU.

Applying Kepler's third law to a = 1.763 AU gives an orbital period of 2.34 yr, or about 855 days.

The high eccentricity (0.523) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 35.01° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.1 km/s at perihelion and falls to 12.6 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 = 20.09 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.34 km.

Observation record and orbit quality

The current orbit solution is based on 331 observations and has a weighted RMS residual of 0.3678 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
1.763 AU
Eccentricity
0.523
Perihelion
0.841 AU
Aphelion
2.685049 AU
Inclination
35.01°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
33.89°

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
2028-May-30 06:17 0.202986 AU
30366282 km
19.78 km/s
2035-Jun-06 01:39 0.347662 AU
52009437 km
18.39 km/s
2035-Oct-31 05:34 0.476678 AU
71310020 km
18.03 km/s
2042-Jun-11 20:35 0.493919 AU
73889193 km
17.80 km/s
2042-Oct-29 20:36 0.400581 AU
59926009 km
19.00 km/s
2049-Oct-30 03:37 0.355724 AU
53215626 km
20.75 km/s
2056-Nov-01 03:07 0.364107 AU
54469670 km
23.26 km/s
2063-Nov-05 11:31 0.428608 AU
64118864 km
26.42 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
20.09

Orbit Quality

RMS
0.36776
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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