Asteroids

2017LA help

Last update: 2025-07-29 02:36 UTC

Orbital Properties

Epoch

60800.0

MJD

Orbit type

Apollo

Perihelion (q)

0.835

Aphelion (Q)

1.363

Eccentricity (e)

0.240

Inclination (i)

41.7

deg

Orbit period (P)

420.9

Earth MOID

0.14621

U parameter

1.0

Next Earth close approach

Date

2031-12-15

Nominal distance (from Earth center)

0.15863

23730206

Maximum Brightness

25.1

mag

Risk

Object is not in risk list

Physical Properties

Absolute Magnitude (H)

20.1

mag

Diameter

260 - 600*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2017-06-01

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

1.099153

1-sigma variation

1.483E-8

Unit

Eccentricity (e)

Value

0.240006

1-sigma variation

0.000001

Unit

Inclination (i)

Value

41.7064

1-sigma variation

3.334E-5

Unit

Long. of Ascending Node (Ω)

Value

79.2983

1-sigma variation

1.759E-5

Unit

Arg. of Perihelion (ω)

Value

11.3379

1-sigma variation

0.0001

Unit

Mean Anomaly (M)

Value

86.92350

1-sigma variation

0.00015

Unit

Perihelion distance

Value

0.835350

1-sigma variation

Unit

Aphelion distance

Value

1.362956

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

-0.146369

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

0.339624

1-sigma variation

Unit

MOID

Value

0.146210

1-sigma variation

Unit

Orbit Period

Value

420.9066

1-sigma variation

Unit

U parameter

Value

1.0

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	2.19829E-16	-5.40174E-15	-1.49305E-14	-4.62195E-15	-4.79878E-13	5.12110E-13
e	-5.40174E-15	2.59029E-13	5.52749E-13	-1.68474E-13	3.32621E-11	-5.28382E-11
i	-1.49305E-14	5.52749E-13	1.11135E-9	-4.71817E-10	-2.32613E-10	7.20237E-10
Ω	-4.62195E-15	-1.68474E-13	-4.71817E-10	3.09255E-10	-2.14795E-10	1.27492E-11
ω	-4.79878E-13	3.32621E-11	-2.32613E-10	-2.14795E-10	9.91774E-9	-1.45272E-8
M	5.12110E-13	-5.28382E-11	7.20237E-10	1.27492E-11	-1.45272E-8	2.26427E-8

Date of computation: 2025-07-29 02:36 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

20.079

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

260 - 600*

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

2898

Unit

Source

[1]

Unobserved

Value

110

Unit

Source

[1]

Normalized RMS of residuals

Value

0.578174

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2017-05-23.50124

Unit

Source

[2]

Last Observation

Value

2025-04-29.91001

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

69 (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

[-]

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 2017LA 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	1978-12-12 06:30	< 1 min	0.1469187	0.1469148	0.0000013
EARTH	1993-12-04 05:14	< 1 min	0.1781927	0.1781852	0.0000025
EARTH	2031-12-15 14:55	< 1 min	0.1586266	0.1586236	0.0000010
EARTH	2046-12-07 18:59	< 1 min	0.1559595	0.1559559	0.0000012
EARTH	2084-12-16 22:45	< 1 min	0.1718853	0.1718768	0.0000028
EARTH	2099-12-10 17:28	< 1 min	0.1471324	0.1471286	0.0000013
EARTH	2114-12-04 03:23	1.0	0.1956725	0.1956510	0.0000072

Download as:

Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
350.58184187	336.99161363	0.14621015	MINIMUM
161.49509800	154.37332197	0.33741763	MINIMUM
71.62585047	74.78942100	0.71073504	SADDLE
263.06554803	235.75802124	0.75913782	SADDLE
37.50390458	206.79671308	1.81933490	SADDLE
174.24367887	341.96513086	2.34425407	MAXIMUM

Download:

MOID Plots

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