SpaceAtlas Space Object Data
NASA JPL SBDB · 2004 JP1

2004 JP1

2004 JP1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.134 AU it takes 1.21 yr to circle the Sun.

Apollo Observations: 215
Orbital Period · P
1.21 yr
v(q)
34.9 km/s
v(Q)
22.4 km/s
Diameter · ≈
0.1 km
TJ
5.44
Eccentricity · e
0.2191

Orbit and dynamics

The path is an ellipse reaching 0.886 AU from the Sun at perihelion and 1.382 AU at aphelion, a radial span of 0.496 AU.

Applying Kepler's third law to a = 1.134 AU gives an orbital period of 1.21 yr, or about 441 days.

An eccentricity of 0.219 makes the orbit moderately elongated.

A steep inclination of 20.93° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 34.9 km/s at perihelion and falls to 22.4 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

No direct size measurement is available; from an absolute magnitude of H = 22.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

The current orbit solution is based on 215 observations and has a weighted RMS residual of 0.4322 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
1.134 AU
Eccentricity
0.2191
Perihelion
0.886 AU
Aphelion
1.382459 AU
Inclination
20.93°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
43.62°

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-May-05 04:30 0.301553 AU
45111661 km
18.78 km/s
2033-May-15 12:08 0.057630 AU
8621290 km
13.58 km/s
2033-Dec-09 03:26 0.425303 AU
63624369 km
10.92 km/s
2039-May-26 00:37 0.158986 AU
23784015 km
11.02 km/s
2039-Nov-21 13:17 0.290941 AU
43524187 km
11.00 km/s
2045-Jun-11 22:22 0.377468 AU
56468403 km
11.77 km/s
2045-Nov-09 19:13 0.150696 AU
22543875 km
11.65 km/s
2051-Nov-08 08:25 0.182646 AU
27323465 km
14.63 km/s
2056-Apr-27 18:20 0.454042 AU
67923680 km
22.61 km/s
2057-Nov-11 23:45 0.371487 AU
55573721 km
19.65 km/s
2062-May-08 04:04 0.231553 AU
34639910 km
17.14 km/s
2068-May-17 10:40 0.012583 AU
1882324 km
12.82 km/s
2068-Dec-05 17:04 0.404076 AU
60448886 km
10.93 km/s
2074-May-22 07:45 0.086353 AU
12918213 km
11.56 km/s
2074-Nov-27 15:35 0.343781 AU
51428970 km
10.98 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
22.7

Orbit Quality

RMS
0.43222
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.