Asteroids

2024YR4 help

Last update: 2025-02-24 09:02 UTC

Orbital Properties

Epoch

60800.0

MJD

Orbit type

Apollo

Perihelion (q)

0.852

Aphelion (Q)

4.180

Eccentricity (e)

0.662

Inclination (i)

3.4

deg

Orbit period (P)

1457.6

Earth MOID

0.00283

U parameter

4.4

Next Earth close approach

Date

2028-12-17

Nominal distance (from Earth center)

0.05366

8027248

Maximum Brightness

22.7

mag

Risk

Object is in risk list

Object is not in priority list

Physical Properties

Absolute Magnitude (H)

mag

Diameter

40 - 90*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2024-12-27

Observatory

ATLAS Chile, Rio Hurtado

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

2.515859

1-sigma variation

0.000025

Unit

Eccentricity (e)

Value

0.661547

1-sigma variation

0.000004

Unit

Inclination (i)

Value

3.4082

1-sigma variation

1.323E-5

Unit

Long. of Ascending Node (Ω)

Value

271.3656

1-sigma variation

8.954E-6

Unit

Arg. of Perihelion (ω)

Value

134.3614

1-sigma variation

1.632E-5

Unit

Mean Anomaly (M)

Value

40.40278

1-sigma variation

0.00062

Unit

Perihelion distance

Value

0.851500

1-sigma variation

Unit

Aphelion distance

Value

4.180218

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

1.613321

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

-0.016140

1-sigma variation

Unit

MOID

Value

0.002828

1-sigma variation

Unit

Orbit Period

Value

1457.5650

1-sigma variation

Unit

U parameter

Value

4.4

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	6.42536E-10	9.17341E-11	3.34264E-10	-5.61591E-11	-3.53008E-10	-1.57303E-8
e	9.17341E-11	1.30969E-11	4.77260E-11	-7.97353E-12	-5.04744E-11	-2.24579E-9
i	3.34264E-10	4.77260E-11	1.75125E-10	-2.22904E-11	-1.90207E-10	-8.18364E-9
Ω	-5.61591E-11	-7.97353E-12	-2.22904E-11	8.01728E-11	-3.51885E-11	1.36934E-9
ω	-3.53008E-10	-5.04744E-11	-1.90207E-10	-3.51885E-11	2.66420E-10	8.64535E-9
M	-1.57303E-8	-2.24579E-9	-8.18364E-9	1.36934E-9	8.64535E-9	3.85102E-7

Date of computation: 2025-02-23 18:14 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

24.045

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

40 - 90*

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

0.489192

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2024-12-25.304941

Unit

Source

[2]

Last Observation

Value

2025-02-23.388958

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

445 (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 2024YR4 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	1952-09-02 07:30	207.5	0.0413478	0.0389396	0.0009009
EARTH	1956-08-30 19:54	344.7	0.0654979	0.0575934	0.0027193
EARTH	1960-09-09 02:06	631.0	0.0593988	0.0518095	0.0027182
EARTH	1964-08-30 04:41	521.7	0.0684499	0.0573886	0.0039023
EARTH	1972-08-24 05:48	386.6	0.1625110	0.1496098	0.0043162
EARTH	2012-08-29 00:49	92.9	0.1951119	0.1920366	0.0010259
EARTH	2016-09-08 16:06	93.2	0.0758706	0.0745124	0.0004589
EARTH	2020-10-26 19:45	150.1	0.1392421	0.1390767	0.0000552
EARTH	2024-12-25 04:45	< 1 s	0.0055400	0.0055399	0.0000000
EARTH	2028-12-17 11:50	83.9	0.0536588	0.0527300	0.0003096
EARTH	2032-12-22 08:06	86.9	0.0019391	0.0005567	0.0004608
EARTH	2055-11-13 16:43	> 1 mo	0.1104525	0.0620886	0.5910930
EARTH	2078-09-20 14:08	> 1 mo	0.0670076	0.0666032	0.5124094
EARTH	2097-09-10 12:49	> 1 mo	0.0961108	0.0675396	11.7342301

Download as:

Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
22.95663517	352.06465094	0.00282823	MINIMUM
335.25784117	252.53394409	0.05921836	MINIMUM
358.10736030	300.29440178	0.14548380	SADDLE
358.87219376	121.98806740	1.85978485	SADDLE
179.74966093	123.24406007	3.17256684	SADDLE
179.81183798	303.27555035	5.17039531	MAXIMUM

Download:

MOID Plots

Click on the images to zoom-in and zoom-out

Level lines of the squared distance function

2024YR4

Date in UTC	MJD	σ	Distance ± Width in RE	Stretching in RE/σ	IP	Exp. energy	PS
2032-12-22.586	63588.586	4.177	0.32 ± 0.000	1.09E1	1.62E-5	1.32E-4	-3.44
2039-12-23.349	66145.349	2.776	0.93 ± 0.000	8.99E4	1.77E-7	1.45E-6	-5.68
2043-12-23.152	67606.152	3.697	1.07 ± 0.000	1.07E6	1.00E-9	8.17E-9	-8.03
2047-12-22.047	69066.047	1.472	0.43 ± 0.000	7.21E4	4.76E-6	3.79E-5	-4.44
2047-12-22.051	69066.051	0.355	0.27 ± 0.000	4.89E5	1.99E-6	1.59E-5	-4.82


Based on 445 optical observations (of which 27 are rejected as outliers) from 2024/12/25.305 to 2025/02/23.389.
Coordinates are given on the Target Plane.
Unit is one Earth radius, but impact cross section has radius between 1.31 and 1.31 Earth radii.
Coordinates for LOV = EQU scaled= 1 second= F.
Aegis software version= 5.0, Date of computation=20250223 154939.933 UTC.

Download this part as:

Download Impactor Table as: