SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 GC20

2019 GC20

2019 GC20 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.204 AU it takes 1.32 yr to circle the Sun.

Apollo Observations: 42
Orbital Period · P
1.32 yr
v(q)
33.3 km/s
v(Q)
22.1 km/s
Diameter · ≈
0.13 km
TJ
5.19
Eccentricity · e
0.2022

Orbit and dynamics

The path is an ellipse reaching 0.961 AU from the Sun at perihelion and 1.447 AU at aphelion, a radial span of 0.486 AU.

Applying Kepler's third law to a = 1.204 AU gives an orbital period of 1.32 yr, or about 483 days.

An eccentricity of 0.202 makes the orbit moderately elongated.

A steep inclination of 23.59° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 33.3 km/s at perihelion and falls to 22.1 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 = 22.26 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.13 km.

Observation record and orbit quality

The current orbit solution is based on 42 observations and has a weighted RMS residual of 0.4025 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
1.204 AU
Eccentricity
0.2022
Perihelion
0.961 AU
Aphelion
1.447449 AU
Inclination
23.59°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
318.13°

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-May-05 15:43 0.486526 AU
72783274 km
12.29 km/s
2031-Nov-12 01:32 0.395365 AU
59145733 km
17.46 km/s
2035-Oct-26 08:41 0.179703 AU
26883215 km
14.09 km/s
2039-Oct-10 08:09 0.048881 AU
7312553 km
13.42 km/s
2040-Feb-15 02:34 0.458050 AU
68523238 km
9.88 km/s
2043-Sep-23 07:24 0.265742 AU
39754382 km
15.85 km/s
2044-Mar-08 10:35 0.436572 AU
65310296 km
11.91 km/s
2047-Sep-06 07:36 0.493496 AU
73825913 km
20.39 km/s
2048-Mar-22 10:12 0.427077 AU
63889765 km
12.58 km/s
2052-Apr-03 11:23 0.431832 AU
64601118 km
12.88 km/s
2056-Apr-15 02:16 0.447675 AU
66971272 km
12.90 km/s
2060-Apr-27 05:19 0.470993 AU
70459619 km
12.63 km/s
2064-May-11 02:32 0.497059 AU
74358957 km
11.93 km/s
2068-Nov-02 22:46 0.286296 AU
42829285 km
15.50 km/s
2072-Oct-16 11:59 0.064589 AU
9662334 km
13.33 km/s
2076-Sep-30 11:26 0.162048 AU
24242045 km
14.38 km/s
2077-Feb-28 19:58 0.445318 AU
66618675 km
11.36 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
22.26

Orbit Quality

RMS
0.40246
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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