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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | .06180722406721374 | 4.4576e-08 | |
a | 3.051599061394506 | 1.5679e-08 | au |
q | 2.862988194443596 | 1.3989e-07 | au |
i | 8.976481588293634 | 4.4687e-06 | deg |
node | 201.2126445952236 | 2.3946e-05 | deg |
peri | 318.6174799610991 | 3.7847e-05 | deg |
M | 8.408809810994184 | 2.821e-05 | deg |
tp | 2458955.019873407551 (2020-Apr-15.51987341) | 0.00015262 | TDB |
period | 1947.106182836327 5.33 | 1.5006e-05 4.108e-08 | d yr |
n | .1848897626505361 | 1.4249e-09 | deg/d |
Q | 3.240209928345415 | 1.6648e-08 | au |
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| | Orbit Determination Parameters
Additional Information
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Orbital Elements at Epoch 2456852.5 (2014-Jul-14.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | .06425857631101341 | 4.4395e-08 | |
q | 2.858088562413448 | 1.4003e-07 | au |
tp | 2457007.814232779864 (2014-Dec-16.31423278) | 0.0001493 | TDB |
node | 201.2936266642898 | 2.3973e-05 | deg |
peri | 318.6084791345826 | 3.704e-05 | deg |
i | 8.969426151071882 | 4.4654e-06 | deg |
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| | Orbit Determination Parameters
Additional Information
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Orbit Covariance (6×6)
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|
e |
q |
tp |
node |
peri |
i |
e |
1.970923675379122E-15 |
-6.184286013544621E-15 |
1.50835811810058E-12 |
-5.227745431216691E-15 |
3.206713160125752E-13 |
-8.536691094881566E-16 |
q |
-6.184286013544621E-15 |
1.960922616326886E-14 |
-5.042142819924763E-12 |
1.802488280549083E-14 |
-1.068491826127954E-12 |
1.855189153824721E-15 |
tp |
1.50835811810058E-12 |
-5.042142819924763E-12 |
2.228995121549167E-8 |
-1.833566872011804E-11 |
4.232404027260696E-9 |
7.857451461604064E-13 |
node |
-5.227745431216691E-15 |
1.802488280549083E-14 |
-1.833566872011804E-11 |
5.74712249988103E-10 |
-5.707866786166507E-10 |
-3.151071664481923E-11 |
peri |
3.206713160125752E-13 |
-1.068491826127954E-12 |
4.232404027260696E-9 |
-5.707866786166507E-10 |
1.371977148053058E-9 |
3.128172567661678E-11 |
i |
-8.536691094881566E-16 |
1.855189153824721E-15 |
7.857451461604064E-13 |
-3.151071664481923E-11 |
3.128172567661678E-11 |
1.993945597820513E-11 |
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Physical Parameter Table
Parameter |
Symbol |
Value |
Units |
Sigma |
Reference |
Notes |
absolute magnitude |
H |
12.9 |
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n/a |
MPO250479 |
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diameter |
diameter |
9.997 |
km |
0.101 |
urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M) |
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rotation period |
rot_per |
1110.58 |
h |
n/a |
LCDB (Rev. 2020-October); Warner et al., 2009 |
Result based on less than full coverage, so that the period may be wrong by 30 percent or so. Published Reference List: [Pal, A.; Szakats, R.; Kiss, C.; Bodi, A.; et al. (2019) Ap. J. Supl. Ser. 247, id.26.] |
geometric albedo |
albedo |
0.121 |
|
0.020 |
urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M) |
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27922 Mascheroni | Discovered 1996 Dec. 8 by P. G. Comba at Prescott. |
Lorenzo Mascheroni (1750-1800), professor at the University of Pavia and author of a treatise on statics, proved that all plane construction problems that can be solved with ruler and compass can also be solved with compass alone. |
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character) |
Reference: 20020427/MPCPages.arc | Last Updated: 2003-10-02 |
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Alternate Designations
1996 XW8 = 1978 GY3 = 2000 LO5 |
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