SpaceAtlas Space Object Data
NASA JPL SBDB · 2005 QP87

2005 QP87

2005 QP87 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.233 AU it takes 1.37 yr to circle the Sun.

Apollo Observations: 85
Orbital Period · P
1.37 yr
v(q)
32 km/s
v(Q)
22.5 km/s
Diameter · ≈
0.01 km
TJ
5.18
Eccentricity · e
0.1753

Orbit and dynamics

The path is an ellipse reaching 1.017 AU from the Sun at perihelion and 1.449 AU at aphelion, a radial span of 0.432 AU.

Applying Kepler's third law to a = 1.233 AU gives an orbital period of 1.37 yr, or about 500 days.

An eccentricity of 0.175 makes the orbit moderately elongated.

Its inclination of 0.27° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32 km/s at perihelion and falls to 22.5 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 27.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 85 observations and has a weighted RMS residual of 0.7004 arcseconds.

Condition code U = 5 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.233 AU
Eccentricity
0.1753
Perihelion
1.017 AU
Aphelion
1.449145 AU
Inclination
0.27°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
64.99°

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-Jan-08 23:40 0.393048 AU
58799095 km
6.54 km/s
2031-Sep-18 02:18 0.022692 AU
3394705 km
3.49 km/s
2035-Mar-17 03:59 0.445127 AU
66590083 km
7.36 km/s
2039-Jan-12 03:43 0.397803 AU
59510533 km
6.78 km/s
2042-Oct-03 14:46 0.035574 AU
5321744 km
7.05 km/s
2046-Mar-06 09:53 0.456948 AU
68358406 km
7.65 km/s
2049-Jun-24 15:31 0.330215 AU
49399462 km
16.48 km/s
2053-Oct-13 20:41 0.170939 AU
25572143 km
12.43 km/s
2060-Jul-04 07:50 0.117196 AU
17532214 km
11.15 km/s
2075-Apr-03 10:19 0.399950 AU
59831700 km
6.68 km/s
2079-Jan-30 05:55 0.440314 AU
65870107 km
7.46 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
27.7

Orbit Quality

RMS
0.70036
Condition
5
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.