SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 GM7

2017 GM7

2017 GM7 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.281 AU it takes 3.44 yr to circle the Sun.

Apollo Observations: 150
Orbital Period · P
3.44 yr
v(q)
37.3 km/s
v(Q)
10.4 km/s
Diameter · ≈
0.58 km
TJ
3.22
Eccentricity · e
0.5625

Orbit and dynamics

Between its closest point (0.998 AU) and its farthest (3.564 AU), the heliocentric distance changes by 2.566 AU over every revolution.

One full revolution takes 3.44 yr (1,258 days), computed from the semi-major axis of 2.281 AU.

The high eccentricity (0.562) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 30.96° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 37.3 km/s at perihelion and falls to 10.4 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 = 18.94 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.58 km.

Observation record and orbit quality

Astrometry from 150 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5656 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
2.281 AU
Eccentricity
0.5625
Perihelion
0.998 AU
Aphelion
3.564063 AU
Inclination
30.96°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
213.61°

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
2048-Jul-18 15:06 0.431304 AU
64522203 km
25.36 km/s
2055-May-29 09:01 0.295970 AU
44276454 km
20.08 km/s
2079-Jul-12 06:08 0.324439 AU
48535394 km
23.28 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
18.94

Orbit Quality

RMS
0.56561
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

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