Asteroids

2023RB15 help

Last update: 2025-02-19 13:28 UTC

Orbital Properties

Epoch

60800.0

MJD

Orbit type

Amor

Perihelion (q)

1.043

Aphelion (Q)

4.216

Eccentricity (e)

0.603

Inclination (i)

6.8

deg

Orbit period (P)

1557.2

Earth MOID

0.03764

U parameter

8.7

Next Earth close approach

Date

2104-08-23

Nominal distance (from Earth center)

0.09966

14909308

Maximum Brightness

23.1

mag

Risk

Object is not in risk list

Object is not in priority list

Physical Properties

Absolute Magnitude (H)

25.9

mag

Diameter

18 - 40*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2023-09-12

Observatory

JPL SynTrack Robotic Telescope, Auberry

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

2.629288

1-sigma variation

0.017304

Unit

Eccentricity (e)

Value

0.603463

1-sigma variation

0.002562

Unit

Inclination (i)

Value

6.7759

1-sigma variation

0.0196

Unit

Long. of Ascending Node (Ω)

Value

174.6686

1-sigma variation

0.0004

Unit

Arg. of Perihelion (ω)

Value

178.1379

1-sigma variation

0.0083

Unit

Mean Anomaly (M)

Value

137.93744

1-sigma variation

1.36039

Unit

Perihelion distance

Value

1.042610

1-sigma variation

Unit

Aphelion distance

Value

4.215967

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

3.217821

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

0.038155

1-sigma variation

Unit

MOID

Value

0.037636

1-sigma variation

Unit

Orbit Period

Value

1557.2408

1-sigma variation

Unit

U parameter

Value

8.7

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	2.99424E-4	4.43370E-5	3.39024E-4	6.91726E-6	-1.44181E-4	-2.35400E-2
e	4.43370E-5	6.56516E-6	5.02006E-5	1.02427E-6	-2.13494E-5	-3.48566E-3
i	3.39024E-4	5.02006E-5	3.83861E-4	7.83196E-6	-1.63248E-4	-2.66532E-2
Ω	6.91726E-6	1.02427E-6	7.83196E-6	1.59931E-7	-3.33071E-6	-5.43817E-4
ω	-1.44181E-4	-2.13494E-5	-1.63248E-4	-3.33071E-6	6.94604E-5	1.13351E-2
M	-2.35400E-2	-3.48566E-3	-2.66532E-2	-5.43817E-4	1.13351E-2	1.85065E0

Date of computation: 2025-02-19 13:28 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

25.873

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

18 - 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

600

Unit

Source

[1]

Normalized RMS of residuals

Value

0.737976

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2023-09-12.251072

Unit

Source

[2]

Last Observation

Value

2023-09-20.329083

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

32 (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 2023RB15 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	2006-08-23 09:08	> 1 mo	0.0890767	0.0161297	0.7534302
EARTH	2023-09-16 20:42	< 1 min	0.0374106	0.0370063	0.0001348
EARTH	2104-08-23 16:45	> 1 mo	0.0996626	0.0148913	2.1947338
EARTH	2121-08-08 18:55	> 1 w	0.1985160	0.0462723	0.1343905

Download as:

Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
359.86737764	251.60112495	0.03777029	MINIMUM
358.82072557	69.48890672	2.03631144	SADDLE
179.70439614	70.61126335	3.22338128	SADDLE
179.71941101	250.61620803	5.22243890	MAXIMUM

Download:

MOID Plots

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