SpaceAtlas Space Object Data
NASA JPL SBDB · 2004 FG29

2004 FG29

2004 FG29 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.878 AU and a period of 0.82 yr.

Aten Observations: 45
Orbital Period · P
0.82 yr
v(q)
54.6 km/s
v(Q)
18.5 km/s
Diameter · ≈
0.02 km
TJ
6.64
Eccentricity · e
0.4929

Orbit and dynamics

Between its closest point (0.445 AU) and its farthest (1.311 AU), the heliocentric distance changes by 0.866 AU over every revolution.

One full revolution takes 0.82 yr (301 days), computed from the semi-major axis of 0.878 AU.

The high eccentricity (0.493) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.43° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 54.6 km/s at perihelion and falls to 18.5 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 = 26 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 45 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5035 arcseconds.

Condition code U = 7 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
0.8784 AU
Eccentricity
0.4929
Perihelion
0.445 AU
Aphelion
1.311363 AU
Inclination
3.43°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
260.54°

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-Mar-14 11:16 0.209139 AU
31286817 km
10.96 km/s
2032-Apr-01 13:51 0.010294 AU
1539905 km
15.88 km/s
2035-Jan-14 10:18 0.377018 AU
56401079 km
29.98 km/s
2036-Feb-12 17:36 0.322769 AU
48285531 km
11.67 km/s
2037-Mar-19 13:30 0.326827 AU
48892681 km
27.84 km/s
2039-Dec-30 23:33 0.073838 AU
11046068 km
17.57 km/s
2041-Mar-20 11:28 0.198970 AU
29765561 km
10.76 km/s
2045-Jan-13 23:44 0.241222 AU
36086269 km
10.84 km/s
2046-Mar-31 03:21 0.094479 AU
14133915 km
18.29 km/s
2049-Jan-10 14:51 0.342800 AU
51282096 km
27.37 km/s
2050-Feb-19 13:05 0.317272 AU
47463274 km
11.67 km/s
2050-Jun-20 22:42 0.468540 AU
70092598 km
16.74 km/s
2051-Mar-16 18:39 0.416246 AU
62269448 km
30.45 km/s
2053-Dec-28 14:02 0.058507 AU
8752532 km
14.92 km/s
2055-Mar-29 12:13 0.064594 AU
9663164 km
11.05 km/s
2060-Mar-27 05:39 0.037275 AU
5576221 km
21.45 km/s
2063-Jan-06 15:16 0.097277 AU
14552379 km
23.73 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
26.0

Orbit Quality

RMS
0.50347
Condition
7
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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