SpaceAtlas Space Object Data
NASA JPL SBDB · 620000

620000

620000 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.277 AU it takes 1.44 yr to circle the Sun.

Apollo Observations: 131
Orbital Period · P
1.44 yr
v(q)
49.1 km/s
v(Q)
14.2 km/s
Diameter · ≈
0.36 km
TJ
4.84
Eccentricity · e
0.5523

Orbit and dynamics

Between its closest point (0.572 AU) and its farthest (1.982 AU), the heliocentric distance changes by 1.41 AU over every revolution.

One full revolution takes 1.44 yr (527 days), computed from the semi-major axis of 1.277 AU.

The high eccentricity (0.552) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 21.42° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 49.1 km/s at perihelion and falls to 14.2 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 = 19.95 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.36 km.

Observation record and orbit quality

Astrometry from 131 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5174 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
1.277 AU
Eccentricity
0.5523
Perihelion
0.572 AU
Aphelion
1.982287 AU
Inclination
21.42°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
64.21°

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
2027-Oct-02 05:39 0.412948 AU
61776195 km
24.43 km/s
2030-Jul-22 07:43 0.407649 AU
60983348 km
21.96 km/s
2033-May-13 20:54 0.464525 AU
69491919 km
21.12 km/s
2036-Feb-18 13:42 0.352076 AU
52669808 km
23.41 km/s
2040-Sep-30 03:16 0.402539 AU
60218971 km
23.80 km/s
2043-Jul-20 20:00 0.410286 AU
61377846 km
22.16 km/s
2046-May-12 15:59 0.463763 AU
69378001 km
20.87 km/s
2049-Feb-17 13:38 0.357510 AU
53482730 km
23.70 km/s
2053-Sep-29 17:00 0.397243 AU
59426740 km
23.47 km/s
2056-Jul-18 15:16 0.412471 AU
61704739 km
22.30 km/s
2059-May-10 18:51 0.462933 AU
69253763 km
20.50 km/s
2062-Feb-17 02:06 0.369459 AU
55270223 km
24.35 km/s
2066-Sep-28 05:51 0.386503 AU
57819983 km
22.76 km/s
2069-Jul-16 05:11 0.416094 AU
62246781 km
22.54 km/s
2072-May-07 06:01 0.461515 AU
69041671 km
20.02 km/s
2075-Feb-16 13:18 0.382369 AU
57201619 km
25.04 km/s
2079-Sep-27 12:08 0.381027 AU
57000795 km
22.35 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
19.95

Orbit Quality

RMS
0.5174
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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