Asteroids

2013CV32 help

Last update: 2025-03-29 00:36 UTC

Orbital Properties

Epoch

60800.0

MJD

Orbit type

Apollo

Perihelion (q)

0.475

Aphelion (Q)

3.095

Eccentricity (e)

0.734

Inclination (i)

18.1

deg

Orbit period (P)

871.1

Earth MOID

0.13567

U parameter

3.3

Next Earth close approach

Date

2093-12-30

Nominal distance (from Earth center)

0.16133

24135351

Maximum Brightness

19.2

mag

Risk

Object is not in risk list

Object is not in priority list

Physical Properties

Absolute Magnitude (H)

20.8

mag

Diameter

190 - 400*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2013-02-03

Observatory

Pan-STARRS 1, Haleakala

ORBIT VISUALISATION TOOLS

External links

Proper elements

Epoch

Near present day

Near middle of observation arc

Orbit properties

Epoch
Semimajor Axis
Eccentricity (e)
Inclination (i)
Long. of Ascending Node (Ω)
Arg. of Perihelion (ω)
Mean Anomaly (M)
Perihelion distance
Aphelion distance
Asc. Node-Earth Sep.
Desc. Node-Earth Sep.
MOID
Orbit Period
U parameter

Value

1-sigma variation

Unit

Epoch

Value

60800.0000

1-sigma variation

Unit

MJD

Semimajor Axis

Value

1.785045

1-sigma variation

0.000002

Unit

Eccentricity (e)

Value

0.734052

1-sigma variation

0.000014

Unit

Inclination (i)

Value

18.1359

1-sigma variation

0.0002

Unit

Long. of Ascending Node (Ω)

Value

306.4904

1-sigma variation

0.0002

Unit

Arg. of Perihelion (ω)

Value

50.0413

1-sigma variation

0.0021

Unit

Mean Anomaly (M)

Value

100.04643

1-sigma variation

0.00137

Unit

Perihelion distance

Value

0.474728

1-sigma variation

Unit

Aphelion distance

Value

3.095361

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

-0.455410

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

0.572777

1-sigma variation

Unit

MOID

Value

0.135671

1-sigma variation

Unit

Orbit Period

Value

871.1081

1-sigma variation

Unit

U parameter

Value

3.3

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	2.56533E-12	2.17282E-11	2.49318E-10	-2.52465E-10	-3.38770E-9	-2.19614E-9
e	2.17282E-11	1.84881E-10	2.10974E-9	-2.14116E-9	-2.87724E-8	-1.86340E-8
i	2.49318E-10	2.10974E-9	2.48743E-8	-2.50084E-8	-3.28613E-7	-2.13358E-7
Ω	-2.52465E-10	-2.14116E-9	-2.50084E-8	2.54429E-8	3.33098E-7	2.16240E-7
ω	-3.38770E-9	-2.87724E-8	-3.28613E-7	3.33098E-7	4.48175E-6	2.90318E-6
M	-2.19614E-9	-1.86340E-8	-2.13358E-7	2.16240E-7	2.90318E-6	1.88138E-6

Date of computation: 2025-03-29 00:36 UTC

Note: The ASCII file is in a format suitable for Orbfit input.

Download ASCII file:

Physical properties

Rotation Period
Quality
Amplitude
Rotation Direction
Spinvector L
Spinvector B

Rotational properties

Value

Unit

Source

Rotation Period

Value

Unit

Source

[-]

Quality

Value

Unit

Source

[-]

Amplitude

Value

Unit

mag

Source

[-]

Rotation Direction

Value

Unit

Source

[-]

Spinvector L

Value

Unit

Source

[-]

Spinvector B

Value

Unit

Source

[-]

Taxonomy
Taxonomy (all)

Taxonomy

Value

Unit

Source

Taxonomy

Value

Unit

Source

[-]

Taxonomy (all)

Value

Unit

Source

[-]

Absolute Magnitude (H)
Slope Parameter (G)

H / G

Value

Unit

Source

Absolute Magnitude (H)

Value

20.764

Unit

mag

Source

[1]

Slope Parameter (G)

Value

0.15**

Unit

mag

Source

[1]

Albedo
Diameter

Size and albedo

Value

Unit

Source

Albedo

Value

0.05 - 0.25

Unit

Source

[2]

Diameter

Value

190 - 400*

Unit

Source

[2]

Color Index Information

Color Index Information

Value

Unit

Source

Color Index Information

Value

Unit

mag

Source

[-]

Sightings

Sightings

Value

Unit

Source

Sightings

Value

Unit

Source

[-]

Download this part as:

Sources

No.	Name	Additional
[1]	ESA Aegis	ESA orbit determination and impact monitoring system
[2]	Estimation	Estimated from absolute magnitude

Observational Information

Arc Length
Unobserved
Normalized RMS of residuals

Arc Information

Value

Unit

Source

Arc Length

Value

2554

Unit

Source

[1]

Unobserved

Value

1926

Unit

Source

[1]

Normalized RMS of residuals

Value

0.689521

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2013-02-03.359

Unit

Source

[2]

Last Observation

Value

2020-02-01.11726

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

59 (0)

Unit

Source

[1]

Radar Summary

First Observation
Last Observation
Delay (Discarded)
Doppler (Discarded)
Total Optical Observations (Discarded)

Radar

Value

Unit

Source

First Observation

Value

Unit

Source

[-]

Last Observation

Value

Unit

Source

[-]

Delay (Discarded)

Value

0 (0)

Unit

Source

[-]

Doppler (Discarded)

Value

0 (0)

Unit

Source

[-]

Total Radar Observations (Discarded)

Value

0 (0)

Unit

Source

[-]

Note: The ASCII file is in a format suitable for Orbfit input.

Sources

No.	Name	Additional
[1]	ESA Aegis	ESA orbit determination and impact monitoring system
[2]	MPC	Minor Planet Center: https://www.minorplanetcenter.net

Computation parameters

As seen from:

Initial Date: *

Final Date: *

Output option:

One line per time step

Time step:*

* - these fields are required

Close Approaches for 2013CV32 from 1950 to 2125

Body	Date in UTC	Time uncert. in min	Nominal distance in au	Min. possible distance in au	Distance uncert. in au
EARTH	1958-01-04 14:44	28.3	0.1535174	0.1531034	0.0001401
EARTH	1989-01-08 13:08	15.5	0.1968875	0.1963391	0.0001831
EARTH	2093-12-30 12:14	51.8	0.1613349	0.1596157	0.0005774
EARTH	2125-01-07 20:54	70.7	0.1410344	0.1391617	0.0006346

Download as:

Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
54.12098453	0.43904313	0.13567132	MINIMUM
310.94309828	156.60499659	0.24494366	MINIMUM
2.89777496	262.36940149	0.55678344	SADDLE
0.01196794	74.83276413	1.46072038	SADDLE
180.96138914	72.93374073	2.14246932	SADDLE
179.09053921	252.19384435	4.07827513	MAXIMUM

Download:

MOID Plots

Click on the images to zoom-in and zoom-out