Asteroids

2016CL246

Last update: 2023-03-26 03:34 UTC

Orbital Properties

Epoch

60000.0

MJD

Orbit type

Apollo

Perihelion (q)

0.796

Aphelion (Q)

2.076

Eccentricity (e)

0.446

Inclination (i)

48.8

deg

Orbit period (P)

628.3

Earth MOID

0.21772

U parameter

2.0

Next Earth close approach

Date

Nominal distance (from Earth center)

Maximum Brightness

mag

Risk

Object is not in risk list

Object is not in priority list

Physical Properties

Absolute Magnitude (H)

19.6

mag

Diameter

400*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2016-02-11

Observatory

Pan-STARRS 1, Haleakala

Orbit Visualiser

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External links

Proper elements

Epoch

Near present day

Near middle of observation arc

Orbit properties

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

Value

1-sigma variation

Unit

Epoch

Value

60000.0000

1-sigma variation

Unit

MJD

Semimajor Axis

Value

1.435606

1-sigma variation

5.358E-8

Unit

Eccentricity (e)

Value

0.445850

1-sigma variation

0.000001

Unit

Inclination (i)

Value

48.7737

1-sigma variation

0.0001

Unit

Ascending Node (Ω)

Value

310.6911

1-sigma variation

8.062E-6

Unit

Arg. of Perihelion (ω)

Value

7.3509

1-sigma variation

0.0003

Unit

Mean Anomaly (M)

Value

198.80150

1-sigma variation

0.00064

Unit

Perihelion

Value

0.795541

1-sigma variation

Unit

Aphelion

Value

2.075671

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

-0.217917

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

1.076698

1-sigma variation

Unit

MOID

Value

0.217725

1-sigma variation

Unit

Orbit Period

Value

628.2771

1-sigma variation

Unit

U parameter

Value

2.0

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	2.87116E-15	-6.21833E-14	2.71277E-12	1.31259E-13	-1.43346E-11	3.12349E-11
e	-6.21833E-14	1.64839E-12	-6.58341E-11	-3.19156E-12	3.59125E-10	-7.98540E-10
i	2.71277E-12	-6.58341E-11	4.20571E-9	5.67745E-11	-1.55617E-8	3.44339E-8
Ω	1.31259E-13	-3.19156E-12	5.67745E-11	6.50038E-11	-7.85482E-10	1.64879E-9
ω	-1.43346E-11	3.59125E-10	-1.55617E-8	-7.85482E-10	8.25960E-8	-1.82543E-7
M	3.12349E-11	-7.98540E-10	3.44339E-8	1.64879E-9	-1.82543E-7	4.04458E-7

Date of computation: 2023-02-12 14:30 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

19.628

Unit

mag

Source

[1]

Slope Parameter (G)

Value

0.15**

Unit

mag

Source

[1]

[2]

Albedo
Diameter

Size and albedo

Value

Unit

Source

Albedo

Value

Unit

Source

[-]

Diameter

Value

400*

Unit

Source

[3]

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 ODIM	ESA orbit determination and impact monitoring system
[2]	NEODyS	NEO Dynamic Site: https://newton.spacedys.com/neodys2
[3]	Estimation	Estimated from absolute magnitude

Observational Information

Arc Length
Unobserved

Arc Information

Value

Unit

Source

Arc Length

Value

2591

Unit

Source

[1]

Unobserved

Value

Unit

Source

[1]

Astrometry Summary

RMS of Residuals
First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

RMS of Residuals

Value

0.658576

Unit

arcsec

Source

[1]

First Observation

Value

2016-01-07.595717

Unit

Source

[2]

Last Observation

Value

2023-02-10.386298

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

51 (1)

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

[3]

Last Observation

Value

Unit

Source

[3]

Delay (Discarded)

Value

0 (0)

Unit

Source

[1]

Doppler (Discarded)

Value

0 (0)

Unit

Source

[1]

Total Radar Observations (Discarded)

Value

0 (0)

Unit

Source

[1]

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

Sources

No.	Name	Additional
[1]	ESA ODIM	ESA orbit determination and impact monitoring system
[2]	MPC	Minor Planet Center: https://www.minorplanetcenter.net
[3]	JPL Radar Observations	Jet Propulsion Laboratory: https://ssd.jpl.nasa.gov/dat/radar_data_ast.txt

Computation parameters

As seen from:

Initial Date: *

Final Date: *

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