SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 GC35

2014 GC35

2014 GC35 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.019 AU it takes 1.03 yr to circle the Sun.

Apollo Observations: 33
Orbital Period · P
1.03 yr
v(q)
40.5 km/s
v(Q)
21.5 km/s
Diameter · ≈
0.12 km
TJ
5.81
Eccentricity · e
0.3066

Orbit and dynamics

The path is an ellipse reaching 0.706 AU from the Sun at perihelion and 1.331 AU at aphelion, a radial span of 0.625 AU.

Applying Kepler's third law to a = 1.019 AU gives an orbital period of 1.03 yr, or about 376 days.

An eccentricity of 0.307 makes the orbit moderately elongated.

A steep inclination of 33.11° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.5 km/s at perihelion and falls to 21.5 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 = 22.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

The current orbit solution is based on 33 observations and has a weighted RMS residual of 0.3538 arcseconds.

Condition code U = 2 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
1.019 AU
Eccentricity
0.3066
Perihelion
0.706 AU
Aphelion
1.331425 AU
Inclination
33.11°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
170.37°

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
2047-Apr-21 01:54 0.481532 AU
72036167 km
24.16 km/s
2048-Apr-21 18:19 0.367709 AU
55008458 km
20.92 km/s
2049-Apr-21 04:39 0.284009 AU
42487111 km
18.62 km/s
2050-Apr-18 10:34 0.250228 AU
37433576 km
17.29 km/s
2051-Apr-14 00:34 0.270784 AU
40508713 km
16.69 km/s
2051-Aug-26 04:44 0.475814 AU
71180710 km
21.18 km/s
2052-Apr-07 13:11 0.324439 AU
48535442 km
16.51 km/s
2052-Sep-13 02:47 0.388404 AU
58104344 km
21.90 km/s
2053-Apr-01 06:09 0.389828 AU
58317431 km
16.51 km/s
2053-Sep-30 00:02 0.311033 AU
46529805 km
21.95 km/s
2054-Mar-25 01:12 0.456479 AU
68288303 km
16.52 km/s
2054-Oct-15 22:15 0.270343 AU
40442799 km
22.03 km/s
2055-Oct-31 08:12 0.291602 AU
43622981 km
22.51 km/s
2056-Nov-14 11:34 0.368938 AU
55192347 km
23.57 km/s
2057-Nov-29 10:29 0.477518 AU
71435657 km
25.30 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
22.4

Orbit Quality

RMS
0.35376
Condition
2
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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