SpaceAtlas Space Object Data
NASA JPL SBDB · 528804

528804

528804 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.85 AU it takes 2.52 yr to circle the Sun.

Apollo Observations: 154
Orbital Period · P
2.52 yr
v(q)
53.4 km/s
v(Q)
9 km/s
Diameter · ≈
0.56 km
TJ
3.63
Eccentricity · e
0.7125

Orbit and dynamics

Between its closest point (0.532 AU) and its farthest (3.168 AU), the heliocentric distance changes by 2.636 AU over every revolution.

One full revolution takes 2.52 yr (919 days), computed from the semi-major axis of 1.85 AU.

The high eccentricity (0.713) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.02° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 53.4 km/s at perihelion and falls to 9 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 = 19.02 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.56 km.

Observation record and orbit quality

Astrometry from 154 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5229 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
1.85 AU
Eccentricity
0.7125
Perihelion
0.532 AU
Aphelion
3.168125 AU
Inclination
13.02°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
296.72°

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
2029-Jun-18 14:10 0.411068 AU
61494894 km
17.40 km/s
2034-Jul-21 07:40 0.258512 AU
38672808 km
16.19 km/s
2039-Aug-05 23:50 0.041359 AU
6187145 km
22.19 km/s
2044-Aug-14 12:37 0.143443 AU
21458723 km
27.28 km/s
2049-Aug-23 21:35 0.333185 AU
49843712 km
32.81 km/s
2061-Dec-29 17:14 0.495085 AU
74063631 km
38.18 km/s
2067-Jan-08 11:39 0.297637 AU
44525862 km
32.07 km/s
2072-Jan-19 07:45 0.080253 AU
12005670 km
25.51 km/s
2077-Jan-27 05:55 0.094859 AU
14190753 km
20.74 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
19.02

Orbit Quality

RMS
0.52294
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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