Asteroids

2022OE6

Last update: 2022-08-07 23:50 UTC

Orbital Properties

Epoch

59800.0

MJD

Orbit type

Apollo

Perihelion (q)

0.945

Aphelion (Q)

3.897

Eccentricity (e)

0.610

Inclination (i)

0.3

deg

Orbit period (P)

1376.0

Earth MOID

0.00288

U parameter

8.4

Next Earth close approach

Date

2037-10-28

Nominal distance (from Earth center)

0.10942

16368287

Maximum Brightness

124.8

mag

Risk

Object is not in risk list

Object is in priority list

Physical Properties

Absolute Magnitude (H)

27.2

mag

Diameter

13*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2022-07-29

Observatory

Pan-STARRS 2, Haleakala

Orbit Visualiser

Click the button to start Orbit Visualiser

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

59800.0000

1-sigma variation

Unit

MJD

Semimajor Axis

Value

2.421122

1-sigma variation

0.007487

Unit

Eccentricity (e)

Value

0.609729

1-sigma variation

0.001240

Unit

Inclination (i)

Value

0.3142

1-sigma variation

0.0006

Unit

Ascending Node (Ω)

Value

53.3991

1-sigma variation

0.0333

Unit

Arg. of Perihelion (ω)

Value

297.9134

1-sigma variation

0.0328

Unit

Mean Anomaly (M)

Value

353.23973

1-sigma variation

0.03489

Unit

Perihelion

Value

0.944893

1-sigma variation

Unit

Aphelion

Value

3.897352

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

0.193723

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

1.123347

1-sigma variation

Unit

MOID

Value

0.002877

1-sigma variation

Unit

Orbit Period

Value

1376.0163

1-sigma variation

Unit

U parameter

Value

8.4

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	5.60587E-5	9.28550E-6	4.33873E-6	2.41160E-4	-2.36248E-4	2.61212E-4
e	9.28550E-6	1.53804E-6	7.18647E-7	3.99370E-5	-3.91228E-5	4.32668E-5
i	4.33873E-6	7.18647E-7	3.36004E-7	1.87838E-5	-1.84104E-5	2.02179E-5
Ω	2.41160E-4	3.99370E-5	1.87838E-5	1.10752E-3	-1.09025E-3	1.12433E-3
ω	-2.36248E-4	-3.91228E-5	-1.84104E-5	-1.09025E-3	1.07366E-3	-1.10148E-3
M	2.61212E-4	4.32668E-5	2.02179E-5	1.12433E-3	-1.10148E-3	1.21716E-3

Date of computation: 2022-08-03 13:00 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

27.214

Unit

mag

Source

[1]

Slope Parameter (G)

Value

0.15**

Unit

mag

Source

[1]

Albedo
Diameter

Size and albedo

Value

Unit

Source

Albedo

Value

Unit

Source

[-]

Diameter

Value

13*

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

[-]

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Sources

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

Observational Information

Arc Length
Unobserved

Arc Information

Value

Unit

Source

Arc Length

Value

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

0.596612

Unit

arcsec

Source

[1]

First Observation

Value

2022-07-29.394255

Unit

Source

[2]

Last Observation

Value

2022-08-03.037513

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

17 (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

[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: *

Output option:

One line per time step

Time step:*

* - these fields are required

Close approaches for 2022OE6 from 1950 to 2122

Body	Date in UTC	Time uncert. in min	Nominal distance in au	Min. possibile distance in au	Distance uncert. in au
EARTH	1950-10-20 05:41	> 1 mo	0.0513734	0.0029382	150.6945095
EARTH	1973-10-16 17:10	> 1 mo	0.0060651	0.0026087	0.7137552
EARTH	2022-08-05 18:17	< 1 min	0.0191895	0.0190884	0.0000336
EARTH	2037-10-28 22:21	> 1 mo	0.1094152	0.0032297	0.4202653
MARS	2038-01-04 12:28	> 1 mo	0.0473113	0.0243784	0.2997428
MARS	2041-10-16 06:41	> 1 w	0.0259364	0.0258949	0.0192981
MARS	2045-07-18 06:51	> 1 mo	0.0429073	0.0259660	0.3340942
EARTH	2067-11-09 15:33	> 1 mo	0.1952458	0.0030738	0.7986929
EARTH	2082-11-02 13:54	> 1 mo	0.1101344	0.0031390	0.5682330
EARTH	2116-08-14 02:14	> 1 mo	0.0113189	0.0042893	0.8819408

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