Asteroids

2025NO1 help

Last update: 2025-07-09 20:00 UTC

Orbital Properties

Epoch

60800.0

MJD

Orbit type

Apollo

Perihelion (q)

1.003

Aphelion (Q)

3.616

Eccentricity (e)

0.566

Inclination (i)

6.7

deg

Orbit period (P)

1282.2

Earth MOID

0.00196

U parameter

8.5

Next Earth close approach

Date

2064-05-24

Nominal distance (from Earth center)

0.08948

13386588

Maximum Brightness

28.7

mag

Risk

Object is in risk list

Object is not in priority list

Physical Properties

Absolute Magnitude (H)

31.1

mag

Diameter

1.6 - 4*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2025-07-02

Observatory

Space Surveillance Telescope, HEH Station

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

2.309796

1-sigma variation

0.008001

Unit

Eccentricity (e)

Value

0.565667

1-sigma variation

0.001512

Unit

Inclination (i)

Value

6.7050

1-sigma variation

0.0138

Unit

Long. of Ascending Node (Ω)

Value

101.1123

1-sigma variation

0.0003

Unit

Arg. of Perihelion (ω)

Value

163.1660

1-sigma variation

0.0033

Unit

Mean Anomaly (M)

Value

347.31473

1-sigma variation

0.06342

Unit

Perihelion distance

Value

1.003220

1-sigma variation

Unit

Aphelion distance

Value

3.616371

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

2.442407

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

0.002619

1-sigma variation

Unit

MOID

Value

0.001957

1-sigma variation

Unit

Orbit Period

Value

1282.2090

1-sigma variation

Unit

U parameter

Value

8.5

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	6.40226E-5	1.20978E-5	1.10041E-4	-2.05069E-6	2.40379E-5	5.07415E-4
e	1.20978E-5	2.28602E-6	2.07932E-5	-3.87494E-7	4.54061E-6	9.58822E-5
i	1.10041E-4	2.07932E-5	1.89235E-4	-3.52708E-6	4.17188E-5	8.72048E-4
Ω	-2.05069E-6	-3.87494E-7	-3.52708E-6	6.57515E-8	-7.79096E-7	-1.62509E-5
ω	2.40379E-5	4.54061E-6	4.17188E-5	-7.79096E-7	1.10447E-5	1.90064E-4
M	5.07415E-4	9.58822E-5	8.72048E-4	-1.62509E-5	1.90064E-4	4.02165E-3

Date of computation: 2025-07-09 20:00 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

31.117

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

1.6 - 4*

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

[-]

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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

0.2

Unit

Source

[1]

Unobserved

Value

Unit

Source

[1]

Normalized RMS of residuals

Value

0.172254

Unit

Source

[1]

Astrometry Summary

First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

First Observation

Value

2025-07-02.697956

Unit

Source

[2]

Last Observation

Value

2025-07-02.911389

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

4 (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 2025NO1 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	2018-05-27 05:58	> 1 mo	0.0773205	0.0505764	0.1191585
EARTH	2025-07-02 14:30	< 1 s	0.0017126	0.0017013	0.0000038
1 Ceres	2026-04-10 03:38	> 1 d	0.0106625	0.0102957	0.0008548
EARTH	2064-05-24 07:41	> 1 mo	0.0894838	0.0564393	0.7087332
EARTH	2071-08-01 07:38	> 1 mo	0.1843090	0.0274287	1.1033192
1 Ceres	2072-04-23 19:59	> 1 w	0.0071657	0.0032340	0.5409482
EARTH	2110-06-17 03:31	> 1 mo	0.0372444	0.0042555	0.0691036
1 Ceres	2118-05-11 09:07	> 1 d	0.0118407	0.0047650	0.1335587

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Stationary Points

Ecc. an. ast.	Ecc. an. Earth	Distance in au	Classification
8.56018876	178.19320874	0.00195658	MINIMUM
0.25141094	342.35027833	1.98735290	SADDLE
179.99473195	342.22934679	2.63272863	SADDLE
180.18434624	162.33065063	4.63144036	MAXIMUM

Download:

MOID Plots

Click on the images to zoom-in and zoom-out

Level lines of the squared distance function

2025NO1

Date in UTC	MJD	σ	σ_imp	Distance ± Width in RE	Stretching in RE/σ	IP	Exp. energy	PS	TS
2071-07-03.150	77660.150	0.143	0.000	0.62 ± 0.008	9.99E5	1.19E-6	3.85E-10	-8.86	0
2093-07-02.371	85695.371	1.382	0.000	1.33 ± 0.016	8.46E4	3.14E-6	1.04E-9	-8.60	0


Based on 4 optical observations (of which 0 are rejected as outliers) from 2025/07/02.698 to 2025/07/02.911.
Coordinates are given on the Target Plane.
Unit is one Earth radius, but impact cross section has radius between 1.58 and 1.58 Earth radii.
Coordinates for LOV = EQU scaled= 1 second= F.
Aegis software version= 5.0, Date of computation=20250709 200626.315 UTC.

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Download Impactor Table as: