SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 HJ

2017 HJ

2017 HJ belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.293 AU it takes 1.47 yr to circle the Sun.

Apollo Observations: 65
Orbital Period · P
1.47 yr
v(q)
45.7 km/s
v(Q)
15 km/s
Diameter · ≈
0.01 km
TJ
4.88
Eccentricity · e
0.5056

Orbit and dynamics

Between its closest point (0.64 AU) and its farthest (1.947 AU), the heliocentric distance changes by 1.307 AU over every revolution.

One full revolution takes 1.47 yr (537 days), computed from the semi-major axis of 1.293 AU.

The high eccentricity (0.506) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.21° 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 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 = 27.53 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 65 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4385 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.293 AU
Eccentricity
0.5056
Perihelion
0.64 AU
Aphelion
1.946741 AU
Inclination
1.21°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
116.18°

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-02 15:00 0.106742 AU
15968383 km
19.51 km/s
2039-May-03 15:42 0.324051 AU
48477402 km
24.73 km/s
2042-Apr-13 15:49 0.041159 AU
6157317 km
13.28 km/s
2045-Feb-07 14:28 0.317083 AU
47434984 km
14.05 km/s
2045-Apr-30 22:33 0.427510 AU
63954601 km
8.11 km/s
2047-Sep-26 10:01 0.418594 AU
62620746 km
8.23 km/s
2047-Dec-18 12:39 0.314410 AU
47035100 km
14.09 km/s
2050-Oct-14 13:55 0.004049 AU
605705 km
13.17 km/s
2053-Sep-24 21:43 0.274270 AU
41030182 km
24.46 km/s
2064-Apr-24 05:44 0.131943 AU
19738449 km
19.38 km/s
2067-Mar-18 23:01 0.224411 AU
33571416 km
9.54 km/s
2070-Jan-15 13:13 0.343942 AU
51453061 km
15.39 km/s
2072-Nov-22 08:07 0.249369 AU
37305103 km
11.02 km/s
2075-Oct-07 08:52 0.034034 AU
5091418 km
17.30 km/s
2078-Sep-18 20:59 0.401139 AU
60009486 km
28.50 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
27.53

Orbit Quality

RMS
0.43848
Condition
6
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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