SpaceAtlas Space Object Data
NASA JPL SBDB · 2008 PF1

2008 PF1

2008 PF1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.356 AU it takes 1.58 yr to circle the Sun.

Apollo Observations: 132
Orbital Period · P
1.58 yr
v(q)
43.9 km/s
v(Q)
14.9 km/s
Diameter · ≈
0.13 km
TJ
4.73
Eccentricity · e
0.4932

Orbit and dynamics

The path is an ellipse reaching 0.687 AU from the Sun at perihelion and 2.025 AU at aphelion, a radial span of 1.338 AU.

Applying Kepler's third law to a = 1.356 AU gives an orbital period of 1.58 yr, or about 577 days.

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 2.76° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 43.9 km/s at perihelion and falls to 14.9 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 = 22.12 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.13 km.

Observation record and orbit quality

The current orbit solution is based on 132 observations and has a weighted RMS residual of 0.4561 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
1.356 AU
Eccentricity
0.4932
Perihelion
0.687 AU
Aphelion
2.024779 AU
Inclination
2.76°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
48.72°

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-Aug-27 15:05 0.112226 AU
16788789 km
10.99 km/s
2031-Feb-07 13:46 0.017641 AU
2639053 km
13.78 km/s
2038-Oct-09 23:32 0.267451 AU
40010090 km
11.72 km/s
2042-Feb-17 02:19 0.159074 AU
23797195 km
19.03 km/s
2046-Jul-28 14:29 0.402341 AU
60189413 km
26.09 km/s
2049-Nov-11 14:11 0.304949 AU
45619788 km
13.81 km/s
2053-Feb-24 06:49 0.296521 AU
44358940 km
23.21 km/s
2057-Jul-24 00:17 0.484552 AU
72487940 km
28.78 km/s
2060-Oct-02 16:06 0.244756 AU
36615040 km
10.96 km/s
2064-Feb-07 18:31 0.010232 AU
1530639 km
13.37 km/s
2071-Aug-12 23:17 0.083849 AU
12543701 km
17.18 km/s
2074-Nov-26 16:38 0.296453 AU
44348752 km
13.59 km/s
2075-Feb-28 22:46 0.455744 AU
68178267 km
8.09 km/s
2078-Feb-24 01:40 0.238399 AU
35663933 km
22.77 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
22.12

Orbit Quality

RMS
0.45611
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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