SpaceAtlas Space Object Data
NASA JPL SBDB · 2000 HP40

2000 HP40

2000 HP40 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.291 AU once every 1.47 yr.

Amor Observations: 69
Orbital Period · P
1.47 yr
v(q)
30.8 km/s
v(Q)
22.3 km/s
Diameter · ≈
0.06 km
TJ
4.98
Eccentricity · e
0.1599

Orbit and dynamics

Between its closest point (1.085 AU) and its farthest (1.497 AU), the heliocentric distance changes by 0.412 AU over every revolution.

One full revolution takes 1.47 yr (536 days), computed from the semi-major axis of 1.291 AU.

An eccentricity of 0.16 makes the orbit moderately elongated.

The orbital plane is tilted 14.14° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 30.8 km/s at perihelion and falls to 22.3 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 24.02 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

Astrometry from 69 individual observations underpins this orbit; the fit leaves an RMS residual of 0.61 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
1.291 AU
Eccentricity
0.1599
Perihelion
1.085 AU
Aphelion
1.497431 AU
Inclination
14.14°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
278.17°

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
2028-Oct-03 16:54 0.456969 AU
68361655 km
8.87 km/s
2031-Oct-30 07:15 0.497644 AU
74446496 km
9.89 km/s
2041-Feb-04 09:17 0.445188 AU
66599151 km
4.63 km/s
2044-May-02 05:07 0.118496 AU
17726821 km
7.56 km/s
2047-Apr-30 01:56 0.321494 AU
48094823 km
11.75 km/s
2047-Aug-08 00:56 0.379020 AU
56700549 km
3.10 km/s
2050-Sep-28 16:29 0.447460 AU
66939094 km
8.50 km/s
2053-Oct-24 22:20 0.491133 AU
73472471 km
9.79 km/s
2063-Jan-19 10:17 0.473933 AU
70899384 km
5.96 km/s
2066-May-02 00:19 0.212497 AU
31789103 km
8.26 km/s
2069-Apr-30 18:07 0.216236 AU
32348409 km
9.77 km/s
2072-Sep-19 14:12 0.432652 AU
64723795 km
7.86 km/s
2075-Oct-19 00:20 0.480841 AU
71932751 km
9.58 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
24.02

Orbit Quality

RMS
0.61002
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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