SpaceAtlas Space Object Data
NASA JPL SBDB · 215588

215588

215588 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.114 AU it takes 1.18 yr to circle the Sun.

Apollo Observations: 437
Orbital Period · P
1.18 yr
v(q)
64.1 km/s
v(Q)
12.4 km/s
Diameter · ≈
0.46 km
TJ
5.35
Eccentricity · e
0.6754

Orbit and dynamics

The path is an ellipse reaching 0.362 AU from the Sun at perihelion and 1.866 AU at aphelion, a radial span of 1.504 AU.

Applying Kepler's third law to a = 1.114 AU gives an orbital period of 1.18 yr, or about 429 days.

The high eccentricity (0.675) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.05° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 64.1 km/s at perihelion and falls to 12.4 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

The measured diameter is 0.49 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.118 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 437 observations and has a weighted RMS residual of 0.4906 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
1.114 AU
Eccentricity
0.6754
Perihelion
0.362 AU
Aphelion
1.866396 AU
Inclination
3.05°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
338.33°

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-Jul-17 00:52 0.053871 AU
8058920 km
22.00 km/s
2030-Mar-26 18:32 0.363058 AU
54312681 km
13.66 km/s
2034-Jul-22 05:16 0.302156 AU
45201821 km
14.12 km/s
2037-Mar-25 14:54 0.051300 AU
7674436 km
20.13 km/s
2040-Jun-28 10:43 0.422911 AU
63266657 km
34.62 km/s
2044-Apr-06 09:14 0.248983 AU
37247295 km
29.25 km/s
2047-Jul-12 09:00 0.140070 AU
20954143 km
25.53 km/s
2050-Jan-27 23:47 0.492458 AU
73670667 km
17.36 km/s
2050-Apr-03 06:00 0.465016 AU
69565329 km
13.89 km/s
2054-Jul-22 11:41 0.174548 AU
26111992 km
16.98 km/s
2057-Mar-22 09:24 0.192974 AU
28868562 km
16.23 km/s
2061-Jul-13 09:04 0.445172 AU
66596799 km
13.57 km/s
2061-Sep-08 09:21 0.477382 AU
71415355 km
14.80 km/s
2064-Mar-31 11:21 0.107553 AU
16089750 km
24.86 km/s
2067-Jul-06 13:45 0.271244 AU
40577547 km
29.74 km/s
2071-Apr-14 12:27 0.405845 AU
60713568 km
34.27 km/s
2074-Jul-18 14:25 0.059374 AU
8882256 km
20.82 km/s
2077-Mar-24 22:36 0.328760 AU
49181767 km
13.87 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.488 km
Albedo
0.118
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.42

Orbit Quality

RMS
0.49064
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.