Asteroids

2022SJ48 help

Last update: 2025-09-10 00:30 UTC

Orbital Properties

Epoch

61000.0

MJD

Orbit type

Apollo

Perihelion (q)

1.016

Aphelion (Q)

4.126

Eccentricity (e)

0.605

Inclination (i)

25.2

deg

Orbit period (P)

1505.8

Earth MOID

0.04964

U parameter

8.5

Next Earth close approach

Date

2121-10-02

Nominal distance (from Earth center)

0.07337

10976090

Maximum Brightness

20.6

mag

Risk

Object is not in risk list

Physical Properties

Absolute Magnitude (H)

24.2

mag

Diameter

40 - 90*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2022-09-30

Observatory

Pan-STARRS 1, Haleakala

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

61000.0000

1-sigma variation

Unit

MJD

Semimajor Axis

Value

2.571064

1-sigma variation

0.012165

Unit

Eccentricity (e)

Value

0.604872

1-sigma variation

0.001832

Unit

Inclination (i)

Value

25.2264

1-sigma variation

0.0403

Unit

Long. of Ascending Node (Ω)

Value

3.2680

1-sigma variation

0.0046

Unit

Arg. of Perihelion (ω)

Value

25.8526

1-sigma variation

0.0145

Unit

Mean Anomaly (M)

Value

269.49993

1-sigma variation

1.90601

Unit

Perihelion distance

Value

1.015899

1-sigma variation

Unit

Aphelion distance

Value

4.126230

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

0.052744

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

2.579855

1-sigma variation

Unit

MOID

Value

0.049644

1-sigma variation

Unit

Orbit Period

Value

1505.8019

1-sigma variation

Unit

U parameter

Value

8.5

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	1.47990E-4	2.22907E-5	4.89464E-4	-5.54334E-5	-1.74455E-4	-2.31868E-2
e	2.22907E-5	3.35752E-6	7.37168E-5	-8.34934E-6	-2.62689E-5	-3.49247E-3
i	4.89464E-4	7.37168E-5	1.62383E-3	-1.83489E-4	-5.81979E-4	-7.66874E-2
Ω	-5.54334E-5	-8.34934E-6	-1.83489E-4	2.07687E-5	6.54928E-5	8.68518E-3
ω	-1.74455E-4	-2.62689E-5	-5.81979E-4	6.54928E-5	2.10791E-4	2.73323E-2
M	-2.31868E-2	-3.49247E-3	-7.66874E-2	8.68518E-3	2.73323E-2	3.63286E0

Date of computation: 2025-09-10 00:30 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

24.163

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

1078

Unit

Source

[1]

Normalized RMS of residuals

Value

0.794098

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2022-09-30.341372

Unit

Source

[2]

Last Observation

Value

2022-10-02.060952

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

35 (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 2022SJ48 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	1989-09-18 11:10	> 1 mo	0.1850862	0.0495993	1.3277822
EARTH	2022-10-01 13:01	< 1 min	0.0642879	0.0638998	0.0001294
EARTH	2121-10-02 15:39	> 1 mo	0.0733706	0.0375493	1.7933405

Download as:

Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
348.10546964	263.85704222	0.04992867	MINIMUM
1.95102942	109.30549570	2.01008899	SADDLE
181.52454132	105.19347144	3.14591038	SADDLE
178.68542621	283.87434391	5.10846510	MAXIMUM

Download:

MOID Plots

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