SpaceAtlas Space Object Data
NASA JPL SBDB · 2006 DP62

2006 DP62

2006 DP62 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.513 AU it takes 1.86 yr to circle the Sun.

Apollo Observations: 51
Orbital Period · P
1.86 yr
v(q)
54.5 km/s
v(Q)
10.8 km/s
Diameter · ≈
0.13 km
TJ
4.24
Eccentricity · e
0.6698

Orbit and dynamics

The path is an ellipse reaching 0.499 AU from the Sun at perihelion and 2.526 AU at aphelion, a radial span of 2.027 AU.

Applying Kepler's third law to a = 1.513 AU gives an orbital period of 1.86 yr, or about 680 days.

The high eccentricity (0.67) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 5.43° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 54.5 km/s at perihelion and falls to 10.8 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 = 22.25 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 51 observations and has a weighted RMS residual of 0.6035 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
1.513 AU
Eccentricity
0.6698
Perihelion
0.499 AU
Aphelion
2.526407 AU
Inclination
5.43°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
5.83°

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-Feb-13 11:06 0.074364 AU
11124642 km
23.27 km/s
2033-Nov-10 02:07 0.491765 AU
73566951 km
24.08 km/s
2035-Jul-27 00:07 0.207520 AU
31044556 km
15.31 km/s
2045-Feb-21 02:24 0.243823 AU
36475381 km
28.59 km/s
2046-Nov-28 14:50 0.462545 AU
69195724 km
21.70 km/s
2048-Aug-26 20:28 0.372718 AU
55757859 km
14.48 km/s
2050-Jun-23 16:21 0.447338 AU
66920799 km
34.65 km/s
2058-Mar-02 19:36 0.438668 AU
65623780 km
34.69 km/s
2059-Dec-24 07:08 0.386777 AU
57861084 km
16.30 km/s
2061-Sep-24 16:34 0.458893 AU
68649437 km
20.51 km/s
2063-Jul-03 11:01 0.252134 AU
37718651 km
28.70 km/s
2073-Jan-27 16:41 0.227152 AU
33981404 km
14.59 km/s
2074-Oct-14 13:43 0.491548 AU
73534560 km
23.58 km/s
2076-Jul-11 11:23 0.071154 AU
10644500 km
23.35 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
22.25

Orbit Quality

RMS
0.60352
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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