SpaceAtlas Space Object Data
NASA JPL SBDB · 6037

6037

6037 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.272 AU it takes 1.43 yr to circle the Sun.

Apollo Observations: 1,102
Orbital Period · P
1.43 yr
v(q)
45.7 km/s
v(Q)
15.3 km/s
Diameter · ≈
0.6 km
TJ
4.95
Eccentricity · e
0.4996

Orbit and dynamics

The path is an ellipse reaching 0.636 AU from the Sun at perihelion and 1.907 AU at aphelion, a radial span of 1.271 AU.

Applying Kepler's third law to a = 1.272 AU gives an orbital period of 1.43 yr, or about 524 days.

The high eccentricity (0.5) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.51° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 45.7 km/s at perihelion and falls to 15.3 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

No direct size measurement is available; from an absolute magnitude of H = 18.86 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.6 km.

Observation record and orbit quality

The current orbit solution is based on 1,102 observations and has a weighted RMS residual of 0.3263 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
1.272 AU
Eccentricity
0.4996
Perihelion
0.636 AU
Aphelion
1.907491 AU
Inclination
3.51°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
302.14°

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
2041-Feb-27 21:36 0.024375 AU
3646423 km
15.02 km/s
2056-Aug-24 19:40 0.063990 AU
9572808 km
13.31 km/s
2064-Feb-22 07:52 0.106072 AU
15868135 km
11.81 km/s
2079-Aug-22 11:43 0.034200 AU
5116279 km
14.82 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
18.86

Orbit Quality

RMS
0.32627
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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