SpaceAtlas Space Object Data
NASA JPL SBDB · 2010 GP67

2010 GP67

2010 GP67 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.114 AU it takes 1.18 yr to circle the Sun.

Apollo Observations: 80
Orbital Period · P
1.18 yr
v(q)
31.4 km/s
v(Q)
25.3 km/s
Diameter · ≈
0.12 km
TJ
5.57
Eccentricity · e
0.1073

Orbit and dynamics

The path is an ellipse reaching 0.995 AU from the Sun at perihelion and 1.234 AU at aphelion, a radial span of 0.239 AU.

Applying Kepler's third law to a = 1.114 AU gives an orbital period of 1.18 yr, or about 429 days.

An eccentricity of 0.107 makes the orbit moderately elongated.

The orbital plane is tilted 13.27° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 31.4 km/s at perihelion and falls to 25.3 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

The measured diameter is 0.25 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.034 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

The current orbit solution is based on 80 observations and has a weighted RMS residual of 0.446 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
1.114 AU
Eccentricity
0.1073
Perihelion
0.995 AU
Aphelion
1.233532 AU
Inclination
13.27°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
232.31°

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
2030-Apr-11 17:50 0.266896 AU
39927048 km
12.52 km/s
2030-Oct-31 07:26 0.229666 AU
34357494 km
7.60 km/s
2037-Apr-26 18:44 0.075070 AU
11230283 km
7.03 km/s
2037-Sep-25 03:21 0.184968 AU
27670793 km
7.58 km/s
2043-Dec-21 18:53 0.331810 AU
49638131 km
6.12 km/s
2044-Sep-02 08:55 0.411555 AU
61567698 km
13.57 km/s
2050-Apr-11 22:13 0.263265 AU
39383949 km
12.45 km/s
2050-Oct-30 16:30 0.228813 AU
34229863 km
7.59 km/s
2057-Apr-28 23:26 0.115747 AU
17315443 km
7.06 km/s
2057-Sep-20 19:51 0.196448 AU
29388178 km
7.76 km/s
2063-Dec-10 14:28 0.322019 AU
48173371 km
6.74 km/s
2064-Sep-02 21:15 0.467874 AU
69992895 km
15.29 km/s
2070-Apr-15 14:31 0.178093 AU
26642309 km
10.46 km/s
2070-Oct-21 10:43 0.203173 AU
30394176 km
7.52 km/s
2077-May-06 00:16 0.215265 AU
32203114 km
7.96 km/s
2077-Sep-11 15:36 0.239886 AU
35886487 km
8.64 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.251 km
Albedo
0.034
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
22.36

Orbit Quality

RMS
0.44595
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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