SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 VP2

2022 VP2

2022 VP2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.89 AU and a period of 0.84 yr.

Aten Observations: 40
Orbital Period · P
0.84 yr
v(q)
38.9 km/s
v(Q)
25.6 km/s
Diameter · ≈
0.02 km
TJ
6.59
Eccentricity · e
0.2058

Orbit and dynamics

Between its closest point (0.707 AU) and its farthest (1.073 AU), the heliocentric distance changes by 0.366 AU over every revolution.

One full revolution takes 0.84 yr (307 days), computed from the semi-major axis of 0.89 AU.

An eccentricity of 0.206 makes the orbit moderately elongated.

A steep inclination of 23.06° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 38.9 km/s at perihelion and falls to 25.6 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 = 26.52 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 40 individual observations underpins this orbit; the fit leaves an RMS residual of 0.509 arcseconds.

Condition code U = 6 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
0.89 AU
Eccentricity
0.2058
Perihelion
0.707 AU
Aphelion
1.073162 AU
Inclination
23.06°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
205.67°

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-Nov-18 17:04 0.231007 AU
34558125 km
17.29 km/s
2028-Jun-07 23:47 0.338397 AU
50623530 km
15.41 km/s
2032-Nov-25 00:55 0.456981 AU
68363392 km
23.39 km/s
2033-Jul-10 17:26 0.417597 AU
62471648 km
13.49 km/s
2033-Dec-16 04:48 0.417167 AU
62407353 km
13.30 km/s
2034-Mar-17 22:02 0.369964 AU
55345788 km
16.76 km/s
2038-Nov-20 16:46 0.225790 AU
33777646 km
12.05 km/s
2039-Apr-13 04:47 0.269120 AU
40259733 km
15.35 km/s
2043-Nov-14 21:21 0.013357 AU
1998235 km
12.56 km/s
2044-May-07 20:49 0.260673 AU
38996104 km
15.34 km/s
2048-Nov-16 08:08 0.159086 AU
23798999 km
15.69 km/s
2049-May-30 03:06 0.312487 AU
46747419 km
15.50 km/s
2053-Nov-21 20:40 0.353123 AU
52826380 km
20.44 km/s
2054-Jun-24 01:36 0.383117 AU
57313428 km
14.90 km/s
2055-Mar-04 16:32 0.447817 AU
66992466 km
18.32 km/s
2059-Jul-25 01:54 0.435788 AU
65192917 km
11.63 km/s
2059-Dec-04 13:33 0.352066 AU
52668352 km
13.05 km/s
2060-Mar-25 09:23 0.326082 AU
48781239 km
16.08 km/s
2064-Nov-18 11:06 0.185372 AU
27731242 km
11.91 km/s
2065-Apr-15 22:05 0.262876 AU
39325657 km
15.29 km/s
2069-Nov-14 12:07 0.013269 AU
1985028 km
12.44 km/s
2070-May-06 15:43 0.259685 AU
38848354 km
15.33 km/s
2074-Nov-16 01:14 0.097130 AU
14530412 km
14.77 km/s
2075-May-25 00:55 0.292454 AU
43750451 km
15.51 km/s
2079-Nov-20 05:46 0.283184 AU
42363769 km
18.56 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
26.52

Orbit Quality

RMS
0.50896
Condition
6
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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