SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 NP2

2024 NP2

2024 NP2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.048 AU it takes 1.07 yr to circle the Sun.

Apollo Observations: 30
Orbital Period · P
1.07 yr
v(q)
42.2 km/s
v(Q)
20 km/s
Diameter · ≈
0.05 km
TJ
5.8
Eccentricity · e
0.3565

Orbit and dynamics

Between its closest point (0.675 AU) and its farthest (1.422 AU), the heliocentric distance changes by 0.747 AU over every revolution.

One full revolution takes 1.07 yr (392 days), computed from the semi-major axis of 1.048 AU.

An eccentricity of 0.356 makes the orbit moderately elongated.

The orbital plane is tilted 5.14° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 42.2 km/s at perihelion and falls to 20 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 = 24.11 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

Astrometry from 30 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5382 arcseconds.

Condition code U = 8 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.048 AU
Eccentricity
0.3565
Perihelion
0.675 AU
Aphelion
1.421612 AU
Inclination
5.14°
Orbital Period
— yr
Epoch
2460495.5
Mean Anomaly
84.91°

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
2035-Nov-18 18:22 0.060058 AU
8984502 km
15.56 km/s
2039-Jun-20 09:23 0.019326 AU
2891120 km
9.36 km/s
2040-Jul-07 12:24 0.194560 AU
29105827 km
21.98 km/s
2050-Nov-19 00:58 0.060577 AU
9062118 km
15.18 km/s
2052-Sep-13 16:13 0.409478 AU
61257070 km
9.50 km/s
2053-Aug-05 22:30 0.339059 AU
50722509 km
8.67 km/s
2054-Jun-20 12:05 0.018510 AU
2769100 km
9.69 km/s
2055-Jul-08 18:27 0.359438 AU
53771186 km
22.32 km/s
2065-Nov-14 04:11 0.199533 AU
29849707 km
18.08 km/s
2067-Sep-25 15:45 0.399269 AU
59729858 km
9.19 km/s
2068-Aug-19 09:25 0.376169 AU
56274122 km
9.21 km/s
2070-Jul-01 03:17 0.132521 AU
19824860 km
17.16 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
24.11

Orbit Quality

RMS
0.53824
Condition
8
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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