Asteroids

2025DS2 help

Last update: 2025-02-23 10:01 UTC

Orbital Properties

Epoch

60800.0

MJD

Orbit type

Apollo

Perihelion (q)

0.960

Aphelion (Q)

1.872

Eccentricity (e)

0.322

Inclination (i)

17.3

deg

Orbit period (P)

615.6

Earth MOID

0.02377

U parameter

7.2

Next Earth close approach

Date

2052-02-07

Nominal distance (from Earth center)

0.18577

27790218

Maximum Brightness

23.6

mag

Risk

Object is not in risk list

Object is in priority list

Physical Properties

Absolute Magnitude (H)

24.3

mag

Diameter

40 - 80*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2025-02-21

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

60800.0000

1-sigma variation

Unit

MJD

Semimajor Axis

Value

1.416218

1-sigma variation

0.000396

Unit

Eccentricity (e)

Value

0.321840

1-sigma variation

0.000191

Unit

Inclination (i)

Value

17.2778

1-sigma variation

0.0071

Unit

Long. of Ascending Node (Ω)

Value

336.5130

1-sigma variation

0.0001

Unit

Arg. of Perihelion (ω)

Value

140.5367

1-sigma variation

0.0051

Unit

Mean Anomaly (M)

Value

60.22043

1-sigma variation

0.02886

Unit

Perihelion distance

Value

0.960422

1-sigma variation

Unit

Aphelion distance

Value

1.872014

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

0.679857

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

0.026623

1-sigma variation

Unit

MOID

Value

0.023769

1-sigma variation

Unit

Orbit Period

Value

615.5928

1-sigma variation

Unit

U parameter

Value

7.2

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	1.57037E-7	7.55939E-8	2.81622E-6	2.61107E-8	1.77362E-6	-1.14289E-5
e	7.55939E-8	3.64085E-8	1.35382E-6	1.29818E-8	8.43195E-7	-5.49706E-6
i	2.81622E-6	1.35382E-6	5.07062E-5	4.26974E-7	3.28021E-5	-2.05388E-4
Ω	2.61107E-8	1.29818E-8	4.26974E-7	1.34656E-8	7.01075E-8	-1.80361E-6
ω	1.77362E-6	8.43195E-7	3.28021E-5	7.01075E-8	2.57953E-5	-1.31565E-4
M	-1.14289E-5	-5.49706E-6	-2.05388E-4	-1.80361E-6	-1.31565E-4	8.32854E-4

Date of computation: 2025-02-22 18:30 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

24.347

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 - 80*

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

0.9

Unit

Source

[1]

Normalized RMS of residuals

Value

0.666766

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2025-02-21.358335

Unit

Source

[2]

Last Observation

Value

2025-02-22.73002

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

82 (3)

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 2025DS2 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	1966-02-22 15:10	> 1 d	0.0270364	0.0245722	0.0327677
EARTH	1993-02-07 09:21	> 1 d	0.1773339	0.0131968	0.0746433
EARTH	1998-03-06 14:18	> 1 d	0.1766922	0.0099193	0.0698070
EARTH	2025-02-23 04:41	< 1 min	0.0240829	0.0240498	0.0000110
EARTH	2052-02-07 04:59	> 1 d	0.1857661	0.0183172	0.0658488
EARTH	2057-03-06 00:00	> 1 d	0.1671765	0.0101636	0.0765729
EARTH	2084-02-22 11:45	> 1 d	0.0330109	0.0230074	0.0565514
EARTH	2116-02-15 22:50	> 1 w	0.1163522	0.0092169	0.1083043
EARTH	2121-03-08 08:08	> 1 d	0.1859341	0.0070174	0.0978582

Download as:

Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
27.29457899	51.63453948	0.02376926	MINIMUM
171.36276987	190.03493768	0.90025949	SADDLE
356.61410423	191.21207754	1.96646617	SADDLE
182.97759934	18.37108261	2.84527609	MAXIMUM

Download:

MOID Plots

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