Asteroids

2025EK1 help

Last update: 2025-03-13 15:55 UTC

Orbital Properties

Epoch

60800.0

MJD

Orbit type

Apollo

Perihelion (q)

0.982

Aphelion (Q)

2.117

Eccentricity (e)

0.366

Inclination (i)

11.0

deg

Orbit period (P)

704.5

Earth MOID

0.05434

U parameter

8.0

Next Earth close approach

Date

2052-03-06

Nominal distance (from Earth center)

0.0761

11384522

Maximum Brightness

20.8

mag

Risk

Object is not in risk list

Object is in priority list

Physical Properties

Absolute Magnitude (H)

24.4

mag

Diameter

40 - 80*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2025-03-03

Observatory

Pan-STARRS 2, 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

60800.0000

1-sigma variation

Unit

MJD

Semimajor Axis

Value

1.549540

1-sigma variation

0.001821

Unit

Eccentricity (e)

Value

0.366026

1-sigma variation

0.000744

Unit

Inclination (i)

Value

11.0467

1-sigma variation

0.0163

Unit

Long. of Ascending Node (Ω)

Value

159.5587

1-sigma variation

0.0041

Unit

Arg. of Perihelion (ω)

Value

46.3440

1-sigma variation

0.0044

Unit

Mean Anomaly (M)

Value

13.73641

1-sigma variation

0.01858

Unit

Perihelion distance

Value

0.982368

1-sigma variation

Unit

Aphelion distance

Value

2.116713

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

0.080341

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

0.786925

1-sigma variation

Unit

MOID

Value

0.054341

1-sigma variation

Unit

Orbit Period

Value

704.5353

1-sigma variation

Unit

U parameter

Value

8.0

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	3.31537E-6	1.35385E-6	2.96193E-5	7.45237E-6	-6.91397E-6	-3.37963E-5
e	1.35385E-6	5.52873E-7	1.20959E-5	3.04340E-6	-2.81390E-6	-1.38047E-5
i	2.96193E-5	1.20959E-5	2.64648E-4	6.65881E-5	-6.14108E-5	-3.02077E-4
Ω	7.45237E-6	3.04340E-6	6.65881E-5	1.67546E-5	-1.54486E-5	-7.60056E-5
ω	-6.91397E-6	-2.81390E-6	-6.14108E-5	-1.54486E-5	1.93070E-5	6.85302E-5
M	-3.37963E-5	-1.38047E-5	-3.02077E-4	-7.60056E-5	6.85302E-5	3.45290E-4

Date of computation: 2025-03-05 11:58 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

24.362

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

Unit

Source

[1]

Normalized RMS of residuals

Value

0.424698

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2025-02-27.508158

Unit

Source

[2]

Last Observation

Value

2025-03-05.37856

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

28 (2)

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 2025EK1 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	1969-03-28 08:28	> 1 mo	0.1257501	0.0148911	0.3116615
EARTH	1998-02-26 18:26	> 1 w	0.1961849	0.0400816	0.2880692
EARTH	2025-03-07 06:10	< 1 min	0.0743138	0.0739566	0.0001191
EARTH	2052-03-06 23:32	> 1 w	0.0761008	0.0529498	0.2054015
EARTH	2079-02-27 17:10	> 1 w	0.1953816	0.0425057	0.3327827
EARTH	2104-04-03 09:56	> 1 mo	0.1414567	0.0023837	0.1378775

Download as:

Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
335.67345661	67.51652364	0.05434057	MINIMUM
183.40835149	285.88872958	1.13965541	SADDLE
3.63706124	287.57197608	1.97268435	SADDLE
180.22389407	103.72281768	3.11375901	MAXIMUM

Download:

MOID Plots

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