SpaceAtlas Space Object Data
NASA JPL SBDB · 2011 JY1

2011 JY1

2011 JY1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.264 AU it takes 1.42 yr to circle the Sun.

Apollo Observations: 108
Orbital Period · P
1.42 yr
v(q)
41.1 km/s
v(Q)
17.1 km/s
Diameter · ≈
0.04 km
TJ
5.01
Eccentricity · e
0.4127

Orbit and dynamics

The path is an ellipse reaching 0.742 AU from the Sun at perihelion and 1.786 AU at aphelion, a radial span of 1.044 AU.

Applying Kepler's third law to a = 1.264 AU gives an orbital period of 1.42 yr, or about 519 days.

The high eccentricity (0.413) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.56° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 41.1 km/s at perihelion and falls to 17.1 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 = 24.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 108 observations and has a weighted RMS residual of 0.421 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
1.264 AU
Eccentricity
0.4127
Perihelion
0.742 AU
Aphelion
1.785653 AU
Inclination
2.56°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
263.31°

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-May-22 11:20 0.447804 AU
66990563 km
24.79 km/s
2030-Oct-23 17:14 0.387844 AU
58020573 km
6.73 km/s
2031-Jan-25 13:31 0.242329 AU
36251925 km
10.70 km/s
2031-Jun-03 23:49 0.474787 AU
71027062 km
8.09 km/s
2038-May-08 20:08 0.163730 AU
24493701 km
16.41 km/s
2040-Nov-22 15:06 0.088251 AU
13202116 km
9.01 km/s
2048-Apr-18 21:50 0.100639 AU
15055419 km
8.70 km/s
2050-Nov-05 07:14 0.179468 AU
26847998 km
16.96 km/s
2057-Oct-09 01:48 0.480486 AU
71879625 km
8.47 km/s
2058-Feb-19 04:13 0.240671 AU
36003812 km
10.59 km/s
2058-May-18 17:50 0.379252 AU
56735297 km
6.14 km/s
2060-Oct-22 15:24 0.450643 AU
67415308 km
25.11 km/s
2065-May-16 04:37 0.310164 AU
46399840 km
20.72 km/s
2067-Dec-28 21:29 0.203196 AU
30397651 km
9.05 km/s
2075-May-02 12:24 0.043474 AU
6503586 km
12.87 km/s
2077-Nov-16 01:25 0.014606 AU
2185003 km
11.42 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
24.6

Orbit Quality

RMS
0.42101
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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