Asteroids

2024GF2 help

Last update: 2024-05-09 00:35 UTC

Orbital Properties

Epoch

60400.0

MJD

Orbit type

Apollo

Perihelion (q)

0.832

Aphelion (Q)

4.834

Eccentricity (e)

0.706

Inclination (i)

12.0

deg

Orbit period (P)

1741.8

Earth MOID

0.05070

U parameter

8.6

Next Earth close approach

Date

2043-03-15

Nominal distance (from Earth center)

0.1446

21631187

Maximum Brightness

20.2

mag

Risk

Object is in risk list

Object is in priority list

Physical Properties

Absolute Magnitude (H)

21.8

mag

Diameter

120 - 260*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2024-04-08

Observatory

Mt. Lemmon Survey

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)
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

60400.0000

1-sigma variation

Unit

MJD

Semimajor Axis

Value

2.833159

1-sigma variation

0.019334

Unit

Eccentricity (e)

Value

0.706382

1-sigma variation

0.001936

Unit

Inclination (i)

Value

11.9869

1-sigma variation

0.0160

Unit

Long. of Ascending Node (Ω)

Value

174.7012

1-sigma variation

0.0206

Unit

Arg. of Perihelion (ω)

Value

291.9257

1-sigma variation

0.0606

Unit

Mean Anomaly (M)

Value

11.28922

1-sigma variation

0.12662

Unit

Perihelion distance

Value

0.831865

1-sigma variation

Unit

Aphelion distance

Value

4.834453

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

0.128826

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

0.923626

1-sigma variation

Unit

MOID

Value

0.050700

1-sigma variation

Unit

Orbit Period

Value

1741.8262

1-sigma variation

Unit

U parameter

Value

8.6

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	3.73787E-4	3.74184E-5	3.09781E-4	-3.98088E-4	1.16555E-3	-2.44808E-3
e	3.74184E-5	3.74619E-6	3.10249E-5	-3.98357E-5	1.16560E-4	-2.45064E-4
i	3.09781E-4	3.10249E-5	2.57257E-4	-3.29349E-4	9.61624E-4	-2.02874E-3
Ω	-3.98088E-4	-3.98357E-5	-3.29349E-4	4.24596E-4	-1.24607E-3	2.60737E-3
ω	1.16555E-3	1.16560E-4	9.61624E-4	-1.24607E-3	3.67132E-3	-7.63478E-3
M	-2.44808E-3	-2.45064E-4	-2.02874E-3	2.60737E-3	-7.63478E-3	1.60334E-2

Date of computation: 2024-05-01 11:58 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

21.792

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

120 - 260*

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
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

0.57675

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2024-04-08.240125

Unit

Source

[2]

Last Observation

Value

2024-04-17.373609

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

41 (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 2024GF2 from 1950 to 2124

Body	Date in UTC	Time uncert. in min	Nominal distance in au	Min. possibile distance in au	Distance uncert. in au
EARTH	2005-03-05 11:37	> 1 mo	0.0733196	0.0573000	0.6904850
EARTH	2024-03-15 17:36	2.7	0.1990847	0.1978454	0.0004131
EARTH	2043-03-15 06:15	> 1 mo	0.1445956	0.0343828	1.0934047
EARTH	2062-02-19 15:25	> 1 mo	0.1346160	0.0119438	1.0680974
EARTH	2080-11-04 08:51	> 1 w	0.1852391	0.1790167	0.1101077
EARTH	2095-03-10 12:24	> 1 w	0.0674098	0.0253779	0.2978380
EARTH	2113-11-14 15:50	> 1 mo	0.1905534	0.1829239	0.1498469

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2024GF2

Date in UTC	MJD	σ	σ_imp	Distance ± Width in RE	Stretching in RE/σ	IP	Exp. energy	PS	TS
2087-03-01.546	83380.546	2.603	0.000	0.84 ± 0.154	1.26E5	1.73E-7	4.81E-5	-5.08	0


Based on 41 optical observations (of which 0 are rejected as outliers) from 2024/04/08.240 to 2024/04/17.374.
Coordinates are given on the Target Plane.
Unit is one Earth radius, but impact cross section has radius between 1.20 and 1.20 Earth radii.
Coordinates for LOV = EQU scaled= 1 second= F.
Aegis software version= 4.0, Date of computation=20240501 130925.462 UTC.

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