SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 TC25

2015 TC25

2015 TC25 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.028 AU it takes 1.04 yr to circle the Sun.

Apollo Observations: 48
Orbital Period · P
1.04 yr
v(q)
33 km/s
v(Q)
26.1 km/s
Diameter · ≈
0 km
TJ
5.94
Eccentricity · e
0.1163

Orbit and dynamics

Between its closest point (0.909 AU) and its farthest (1.148 AU), the heliocentric distance changes by 0.239 AU over every revolution.

One full revolution takes 1.04 yr (381 days), computed from the semi-major axis of 1.028 AU.

An eccentricity of 0.116 makes the orbit moderately elongated.

Its inclination of 3.74° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33 km/s at perihelion and falls to 26.1 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 = 29.34 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0 km.

Observation record and orbit quality

Astrometry from 48 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4072 arcseconds.

Condition code U = 2 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
1.028 AU
Eccentricity
0.1163
Perihelion
0.909 AU
Aphelion
1.147556 AU
Inclination
3.74°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
10.43°

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
2038-Sep-22 07:24 0.341489 AU
51086051 km
13.25 km/s
2039-Oct-06 11:21 0.074865 AU
11199706 km
5.54 km/s
2040-Jul-31 23:48 0.136807 AU
20466031 km
2.89 km/s
2041-Jan-21 06:45 0.093912 AU
14049045 km
2.59 km/s
2041-Apr-29 13:11 0.098255 AU
14698761 km
2.64 km/s
2042-Apr-01 05:21 0.146273 AU
21882141 km
7.53 km/s
2043-Apr-13 08:57 0.401961 AU
60132549 km
15.03 km/s
2063-Sep-19 07:22 0.395261 AU
59130152 km
14.87 km/s
2064-Oct-01 12:18 0.139546 AU
20875741 km
7.42 km/s
2065-Sep-02 12:04 0.106153 AU
15880232 km
2.36 km/s
2065-Dec-06 21:18 0.089125 AU
13332870 km
2.73 km/s
2066-May-27 19:50 0.129846 AU
19424624 km
3.03 km/s
2067-Mar-29 02:47 0.078528 AU
11747668 km
5.62 km/s
2068-Apr-09 10:33 0.343883 AU
51444225 km
13.35 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
29.34

Orbit Quality

RMS
0.40716
Condition
2
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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