SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 GG4

2017 GG4

2017 GG4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.662 AU it takes 2.14 yr to circle the Sun.

Apollo Observations: 77
Orbital Period · P
2.14 yr
v(q)
53.5 km/s
v(Q)
10 km/s
Diameter · ≈
0.37 km
TJ
3.89
Eccentricity · e
0.6854

Orbit and dynamics

Between its closest point (0.523 AU) and its farthest (2.801 AU), the heliocentric distance changes by 2.278 AU over every revolution.

One full revolution takes 2.14 yr (783 days), computed from the semi-major axis of 1.662 AU.

The high eccentricity (0.685) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 21.99° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 53.5 km/s at perihelion and falls to 10 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 = 19.94 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.37 km.

Observation record and orbit quality

Astrometry from 77 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5222 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
1.662 AU
Eccentricity
0.6854
Perihelion
0.523 AU
Aphelion
2.801135 AU
Inclination
21.99°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
76.45°

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
2032-May-01 21:01 0.352264 AU
52697983 km
21.14 km/s
2036-Oct-29 15:59 0.302161 AU
45202690 km
31.56 km/s
2047-May-03 21:06 0.356661 AU
53355665 km
21.14 km/s
2051-Oct-30 21:02 0.308907 AU
46211784 km
31.82 km/s
2062-May-04 03:54 0.359850 AU
53832746 km
21.13 km/s
2066-Oct-30 23:29 0.312602 AU
46764646 km
32.00 km/s
2077-May-06 20:27 0.372854 AU
55778217 km
21.32 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
19.94

Orbit Quality

RMS
0.52218
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.