Asteroids

2025AE3 help

Last update: 2025-02-22 05:33 UTC

Orbital Properties

Epoch

60800.0

MJD

Orbit type

Apollo

Perihelion (q)

0.959

Aphelion (Q)

3.450

Eccentricity (e)

0.565

Inclination (i)

6.6

deg

Orbit period (P)

1195.8

Earth MOID

0.02796

U parameter

7.3

Next Earth close approach

Date

2025-02-24

Nominal distance (from Earth center)

0.07029

10515212

Maximum Brightness

19.6

mag

Risk

Object is not in risk list

Object is in priority list

Physical Properties

Absolute Magnitude (H)

22.2

mag

Diameter

100 - 220*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2025-01-06

Observatory

Mt. Lemmon Survey

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

2.204780

1-sigma variation

0.001347

Unit

Eccentricity (e)

Value

0.564897

1-sigma variation

0.000269

Unit

Inclination (i)

Value

6.6098

1-sigma variation

0.0020

Unit

Long. of Ascending Node (Ω)

Value

191.0962

1-sigma variation

0.0091

Unit

Arg. of Perihelion (ω)

Value

349.1688

1-sigma variation

0.0077

Unit

Mean Anomaly (M)

Value

15.57311

1-sigma variation

0.01402

Unit

Perihelion distance

Value

0.959306

1-sigma variation

Unit

Aphelion distance

Value

3.450253

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

-0.033869

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

2.372228

1-sigma variation

Unit

MOID

Value

0.027959

1-sigma variation

Unit

Orbit Period

Value

1195.7662

1-sigma variation

Unit

U parameter

Value

7.3

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	1.81343E-6	3.62244E-7	2.65605E-6	1.21771E-5	-1.01783E-5	-1.88773E-5
e	3.62244E-7	7.23611E-8	5.30576E-7	2.43153E-6	-2.03210E-6	-3.77088E-6
i	2.65605E-6	5.30576E-7	3.89066E-6	1.78147E-5	-1.48838E-5	-2.76491E-5
Ω	1.21771E-5	2.43153E-6	1.78147E-5	8.31015E-5	-6.98582E-5	-1.26749E-4
ω	-1.01783E-5	-2.03210E-6	-1.48838E-5	-6.98582E-5	5.88531E-5	1.05938E-4
M	-1.88773E-5	-3.77088E-6	-2.76491E-5	-1.26749E-4	1.05938E-4	1.96509E-4

Date of computation: 2025-02-19 15:19 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

22.162

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

100 - 220*

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

Unit

Source

[1]

Unobserved

Value

Unit

Source

[1]

Normalized RMS of residuals

Value

0.522438

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2025-01-06.332331

Unit

Source

[2]

Last Observation

Value

2025-02-07.340081

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

31 (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 2025AE3 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	1953-02-03 12:26	> 1 d	0.1908149	0.1190870	0.0254841
EARTH	1966-05-01 11:30	> 1 w	0.1021947	0.0372080	0.1580147
EARTH	2025-02-24 16:57	1.2	0.0702898	0.0701870	0.0000343
EARTH	2061-02-13 05:25	> 1 w	0.1259921	0.0675351	0.1483402
EARTH	2074-05-09 00:42	> 1 w	0.1447582	0.0511441	0.1488703
EARTH	2110-05-09 04:59	> 1 w	0.1332342	0.0519442	0.0786725

Download as:

Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
11.02421850	97.76278323	0.02795934	MINIMUM
1.31546072	259.61564307	1.96222097	SADDLE
180.30435972	258.52513756	2.44742315	SADDLE
180.42957816	78.58910162	4.44662464	MAXIMUM

Download:

MOID Plots

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