Asteroids

2022TR

Last update: 2023-09-29 23:50 UTC

Orbital Properties

Epoch

60200.0

MJD

Orbit type

Apollo

Perihelion (q)

0.847

Aphelion (Q)

2.619

Eccentricity (e)

0.511

Inclination (i)

2.4

deg

Orbit period (P)

833.3

Earth MOID

0.00975

U parameter

7.7

Next Earth close approach

Date

2038-09-24

Nominal distance (from Earth center)

0.18896

28268721

Maximum Brightness

26.6

mag

Risk

Object is not in risk list

Object is not in priority list

Physical Properties

Absolute Magnitude (H)

27.5

mag

Diameter

11*

Taxonomic type

Rotation period (T)

Discovery Information

Discovery Date

2022-10-02

Observatory

Pan-STARRS 1, Haleakala

Orbit Visualiser

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External links

Proper elements

Epoch

Near present day

Near middle of observation arc

Orbit properties

Epoch
Semimajor Axis
Eccentricity (e)
Inclination (i)
Ascending Node (Ω)
Arg. of Perihelion (ω)
Mean Anomaly (M)
Perihelion
Aphelion
Asc. Node-Earth Sep.
Desc. Node-Earth Sep.
MOID
Orbit Period
U parameter

Value

1-sigma variation

Unit

Epoch

Value

60200.0000

1-sigma variation

Unit

MJD

Semimajor Axis

Value

1.732954

1-sigma variation

0.001511

Unit

Eccentricity (e)

Value

0.511468

1-sigma variation

0.000479

Unit

Inclination (i)

Value

2.3891

1-sigma variation

0.0021

Unit

Ascending Node (Ω)

Value

1.9046

1-sigma variation

0.0007

Unit

Arg. of Perihelion (ω)

Value

70.3398

1-sigma variation

0.0010

Unit

Mean Anomaly (M)

Value

128.80176

1-sigma variation

0.16395

Unit

Perihelion

Value

0.846604

1-sigma variation

Unit

Aphelion

Value

2.619304

1-sigma variation

Unit

Asc. Node-Earth Sep.

Value

0.088775

1-sigma variation

Unit

Desc. Node-Earth Sep.

Value

0.547419

1-sigma variation

Unit

MOID

Value

0.009752

1-sigma variation

Unit

Orbit Period

Value

833.2572

1-sigma variation

Unit

U parameter

Value

7.7

1-sigma variation

Unit

Covariance Matrix

	a	e	i	Ω	ω	M
a	2.28221E-6	7.23377E-7	3.24520E-6	1.10992E-6	-1.50706E-6	-2.47685E-4
e	7.23377E-7	2.29284E-7	1.02860E-6	3.51784E-7	-4.77638E-7	-7.85069E-5
i	3.24520E-6	1.02860E-6	4.61565E-6	1.58182E-6	-2.14822E-6	-3.52197E-4
Ω	1.10992E-6	3.51784E-7	1.58182E-6	5.51699E-7	-7.50238E-7	-1.20457E-4
ω	-1.50706E-6	-4.77638E-7	-2.14822E-6	-7.50238E-7	1.02429E-6	1.63556E-4
M	-2.47685E-4	-7.85069E-5	-3.52197E-4	-1.20457E-4	1.63556E-4	2.68808E-2

Date of computation: 2023-08-01 23:50 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

27.476

Unit

mag

Source

[1]

Slope Parameter (G)

Value

0.15**

Unit

mag

Source

[1]

Albedo
Diameter

Size and albedo

Value

Unit

Source

Albedo

Value

Unit

Source

[-]

Diameter

Value

11*

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 ODIM	ESA orbit determination and impact monitoring system
[2]	Estimation	Estimated from absolute magnitude

Observational Information

Arc Length
Unobserved

Arc Information

Value

Unit

Source

Arc Length

Value

Unit

Source

[1]

Unobserved

Value

357

Unit

Source

[1]

Astrometry Summary

RMS of Residuals
First Observation
Last Observation
Total Optical Observations (Discarded)

Optical

Value

Unit

Source

RMS of Residuals

Value

0.495467

Unit

arcsec

Source

[1]

First Observation

Value

2022-10-02.29358

Unit

Source

[2]

Last Observation

Value

2022-10-07.876729

Unit

Source

[2]

Total Optical Observations (Discarded)

Value

29 (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

[3]

Last Observation

Value

Unit

Source

[3]

Delay (Discarded)

Value

0 (0)

Unit

Source

[1]

Doppler (Discarded)

Value

0 (0)

Unit

Source

[1]

Total Radar Observations (Discarded)

Value

0 (0)

Unit

Source

[1]

Note: The ASCII file is in a format suitable for Orbfit input.

Sources

No.	Name	Additional
[1]	ESA ODIM	ESA orbit determination and impact monitoring system
[2]	MPC	Minor Planet Center: https://www.minorplanetcenter.net
[3]	JPL Radar Observations	Jet Propulsion Laboratory: https://ssd.jpl.nasa.gov/dat/radar_data_ast.txt

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 2022TR from 1950 to 2123

Body	Date in UTC	Time uncert. in min	Nominal distance in au	Min. possibile distance in au	Distance uncert. in au
EARTH	1952-01-10 17:45	> 1 mo	0.0913084	0.0360995	0.4528818
EARTH	1968-01-26 14:14	> 1 w	0.0357779	0.0357738	0.0010454
EARTH	1984-02-05 12:01	246.4	0.1123449	0.1108283	0.0005062
EARTH	1990-09-22 19:23	> 1 d	0.1994909	0.0755366	0.0413559
EARTH	2006-10-01 06:29	> 1 w	0.0766684	0.0085922	0.1204162
EARTH	2022-10-08 14:28	< 1 s	0.0102707	0.0102440	0.0000089
EARTH	2038-09-24 03:16	> 1 d	0.1889647	0.0077397	0.1218060
EARTH	2048-02-03 02:08	> 1 w	0.0713731	0.0332591	0.1408043
MARS	2057-06-17 08:02	> 1 d	0.0470265	0.0428504	0.0365569
EARTH	2064-01-23 12:13	> 1 w	0.0473546	0.0332106	0.0649691
EARTH	2079-12-10 01:10	> 1 w	0.1424138	0.1267503	0.0054625
EARTH	2095-10-18 14:18	658.6	0.0582348	0.0493174	0.0029769
EARTH	2111-10-05 19:52	> 1 d	0.0539238	0.0109199	0.0667514
EARTH	2121-02-12 01:13	240.7	0.1808582	0.1752323	0.0018767

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