Asteroids

2024FN help

Last update: 2024-04-26 23:50 UTC

Orbital Properties

Epoch

60400.0

MJD

Orbit type

Apollo

Perihelion (q)

0.991

Aphelion (Q)

4.005

Eccentricity (e)

0.603

Inclination (i)

2.9

deg

Orbit period (P)

1442.2

Earth MOID

0.04826

U parameter

6.3

Next Earth close approach

Date

2028-08-05

Nominal distance (from Earth center)

0.09806

14669221

Maximum Brightness

17.9

mag

Risk

Object is not in risk list

Object is in priority list

Physical Properties

Absolute Magnitude (H)

20.7

mag

Diameter

190 - 400*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2024-03-17

Observatory

Pan-STARRS 1, Haleakala

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

2.498161

1-sigma variation

0.000374

Unit

Eccentricity (e)

Value

0.603341

1-sigma variation

0.000092

Unit

Inclination (i)

Value

2.9339

1-sigma variation

0.0017

Unit

Long. of Ascending Node (Ω)

Value

7.0081

1-sigma variation

0.0045

Unit

Arg. of Perihelion (ω)

Value

270.3851

1-sigma variation

0.0204

Unit

Mean Anomaly (M)

Value

331.26665

1-sigma variation

0.00484

Unit

Perihelion distance

Value

0.990918

1-sigma variation

Unit

Aphelion distance

Value

4.005403

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

0.581282

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

0.597582

1-sigma variation

Unit

MOID

Value

0.048265

1-sigma variation

Unit

Orbit Period

Value

1442.2116

1-sigma variation

Unit

U parameter

Value

6.3

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	1.39972E-7	3.39366E-8	5.33252E-7	-1.40295E-6	6.04236E-6	2.99652E-7
e	3.39366E-8	8.52705E-9	1.45200E-7	-3.82993E-7	1.67980E-6	-9.77062E-9
i	5.33252E-7	1.45200E-7	2.88756E-6	-7.65054E-6	3.45031E-5	-3.26259E-6
Ω	-1.40295E-6	-3.82993E-7	-7.65054E-6	2.02882E-5	-9.15019E-5	8.85574E-6
ω	6.04236E-6	1.67980E-6	3.45031E-5	-9.15019E-5	4.15597E-4	-4.64668E-5
M	2.99652E-7	-9.77062E-9	-3.26259E-6	8.85574E-6	-4.64668E-5	2.34569E-5

Date of computation: 2024-04-23 11:53 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

20.735

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

190 - 400*

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 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

0.522742

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2024-03-17.425686

Unit

Source

[2]

Last Observation

Value

2024-04-17.26593

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

49 (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 2024FN 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	1977-07-04 20:59	> 1 w	0.0832784	0.0668126	0.0057686
EARTH	2028-08-05 04:52	948.7	0.0980577	0.0854922	0.0042936
EARTH	2032-06-30 14:18	> 1 d	0.0537902	0.0533928	0.0001338
EARTH	2036-05-23 03:22	> 1 d	0.1024447	0.0706162	0.0114951
EARTH	2100-05-28 10:43	581.8	0.1630794	0.1528667	0.0034182
EARTH	2104-06-10 14:23	> 1 d	0.0880566	0.0797751	0.0028599
EARTH	2108-06-16 14:48	> 1 d	0.0747222	0.0681076	0.0023510
EARTH	2112-06-21 01:01	> 1 d	0.0717397	0.0651060	0.0023994
EARTH	2116-06-30 00:12	> 1 d	0.0668304	0.0653425	0.0004967
EARTH	2120-06-27 13:42	> 1 w	0.0666524	0.0589096	0.0028688
EARTH	2124-06-25 20:27	> 1 w	0.0689676	0.0527038	0.0092637

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