Asteroids

2014MO68

Last update: 2023-06-01 00:01 UTC

Orbital Properties

Epoch

60000.0

MJD

Orbit type

Apollo

Perihelion (q)

0.960

Aphelion (Q)

3.838

Eccentricity (e)

0.600

Inclination (i)

2.5

deg

Orbit period (P)

1357.5

Earth MOID

0.00635

U parameter

7.7

Next Earth close approach

Date

2040-08-26

Nominal distance (from Earth center)

0.06238

9332304

Maximum Brightness

130.1

mag

Risk

Object is not in risk list

Object is not in priority list

Physical Properties

Absolute Magnitude (H)

23.4

mag

Diameter

80*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2014-06-30

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

2.399373

1-sigma variation

0.002311

Unit

Eccentricity (e)

Value

0.599717

1-sigma variation

0.000364

Unit

Inclination (i)

Value

2.5451

1-sigma variation

0.0008

Unit

Ascending Node (Ω)

Value

317.5658

1-sigma variation

0.0031

Unit

Arg. of Perihelion (ω)

Value

22.9713

1-sigma variation

0.0042

Unit

Mean Anomaly (M)

Value

104.52303

1-sigma variation

1.19057

Unit

Perihelion

Value

0.960429

1-sigma variation

Unit

Aphelion

Value

3.838317

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

-0.024684

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

2.445222

1-sigma variation

Unit

MOID

Value

0.006351

1-sigma variation

Unit

Orbit Period

Value

1357.5167

1-sigma variation

Unit

U parameter

Value

7.7

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	5.34146E-6	8.40850E-7	1.82366E-6	7.05386E-6	-9.68572E-6	-2.75159E-3
e	8.40850E-7	1.32366E-7	2.87082E-7	1.11040E-6	-1.52467E-6	-4.33154E-4
i	1.82366E-6	2.87082E-7	6.23086E-7	2.40081E-6	-3.29855E-6	-9.39438E-4
Ω	7.05386E-6	1.11040E-6	2.40081E-6	9.44786E-6	-1.29302E-5	-3.63372E-3
ω	-9.68572E-6	-1.52467E-6	-3.29855E-6	-1.29302E-5	1.77266E-5	4.98948E-3
M	-2.75159E-3	-4.33154E-4	-9.39438E-4	-3.63372E-3	4.98948E-3	1.41745E0

Date of computation: 2023-05-08 23:50 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

23.372

Unit

mag

Source

[1]

Slope Parameter (G)

Value

0.15**

Unit

mag

Source

[2]

[1]

Albedo
Diameter

Size and albedo

Value

Unit

Source

Albedo

Value

Unit

Source

[-]

Diameter

Value

80*

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

Unit

Source

[1]

Unobserved

Value

3236

Unit

Source

[1]

Astrometry Summary

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

Optical

Value

Unit

Source

RMS of Residuals

Value

0.484765

Unit

arcsec

Source

[1]

First Observation

Value

2014-06-20.41351

Unit

Source

[2]

Last Observation

Value

2014-07-22.410996

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

20 (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 2014MO68 from 1950 to 2123

Body	Date in UTC	Time uncert. in min	Nominal distance in au	Min. possibile distance in au	Distance uncert. in au
EARTH	1962-07-18 15:21	> 1 w	0.0914696	0.0111493	0.1466445
EARTH	1988-09-17 18:25	> 1 mo	0.0539055	0.0403507	0.0623540
EARTH	2014-07-18 00:22	< 1 min	0.0815856	0.0814612	0.0000415
EARTH	2040-08-26 16:05	> 1 mo	0.0623826	0.0417207	0.0391090
EARTH	2077-10-21 11:36	> 1 d	0.1619425	0.0717669	0.0312347

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