Asteroids

2024GC6 help

Last update: 2025-01-22 06:31 UTC

Orbital Properties

Epoch

60600.0

MJD

Orbit type

Apollo

Perihelion (q)

0.929

Aphelion (Q)

3.274

Eccentricity (e)

0.558

Inclination (i)

12.4

deg

Orbit period (P)

1112.7

Earth MOID

0.02211

U parameter

7.7

Next Earth close approach

Date

2082-02-09

Nominal distance (from Earth center)

0.19872

29728362

Maximum Brightness

25.5

mag

Risk

Object is not in risk list

Object is not in priority list

Physical Properties

Absolute Magnitude (H)

25.7

mag

Diameter

19 - 40*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2024-04-14

Observatory

Catalina Sky 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

60600.0000

1-sigma variation

Unit

MJD

Semimajor Axis

Value

2.101406

1-sigma variation

0.002351

Unit

Eccentricity (e)

Value

0.557890

1-sigma variation

0.000510

Unit

Inclination (i)

Value

12.3611

1-sigma variation

0.0079

Unit

Long. of Ascending Node (Ω)

Value

204.7988

1-sigma variation

0.0002

Unit

Arg. of Perihelion (ω)

Value

315.4486

1-sigma variation

0.0025

Unit

Mean Anomaly (M)

Value

71.18591

1-sigma variation

0.12193

Unit

Perihelion distance

Value

0.929054

1-sigma variation

Unit

Aphelion distance

Value

3.273759

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

0.034400

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

1.406002

1-sigma variation

Unit

MOID

Value

0.022112

1-sigma variation

Unit

Orbit Period

Value

1112.6625

1-sigma variation

Unit

U parameter

Value

7.7

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	5.52600E-6	1.19798E-6	1.86578E-5	-4.90214E-7	4.61939E-6	-2.86625E-4
e	1.19798E-6	2.59721E-7	4.04473E-6	-1.06269E-7	9.95995E-7	-6.21361E-5
i	1.86578E-5	4.04473E-6	6.30072E-5	-1.65529E-6	1.56236E-5	-9.67753E-4
Ω	-4.90214E-7	-1.06269E-7	-1.65529E-6	4.35075E-8	-4.11420E-7	2.54269E-5
ω	4.61939E-6	9.95995E-7	1.56236E-5	-4.11420E-7	6.13409E-6	-2.40044E-4
M	-2.86625E-4	-6.21361E-5	-9.67753E-4	2.54269E-5	-2.40044E-4	1.48669E-2

Date of computation: 2024-12-09 13:46 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

25.676

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

19 - 40*

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

281

Unit

Source

[1]

Normalized RMS of residuals

Value

0.578054

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2024-04-14.303528

Unit

Source

[2]

Last Observation

Value

2024-04-16.91835

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

54 (4)

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 2024GC6 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	2021-02-23 13:11	> 1 w	0.1789481	0.1475510	0.0129710
EARTH	2024-04-11 20:37	< 1 min	0.0242096	0.0241553	0.0000181
EARTH	2082-02-09 04:50	> 1 mo	0.1987218	0.1798920	0.1691264
EARTH	2085-04-07 02:00	> 1 mo	0.0349490	0.0161014	0.4305224

Download as:

Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
22.24122921	97.93284420	0.02091120	MINIMUM
0.31348868	238.64200343	1.93170512	SADDLE
179.49961601	238.96271508	2.27741527	SADDLE
180.83723588	59.67262475	4.25146780	MAXIMUM

Download:

MOID Plots

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