(2011 CL50) |
Classification: Aten [NEO] SPK-ID: 3557536 |
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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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | .1459654425742445 | 4.4008e-08 | |
a | .8849179501697163 | 2.0286e-09 | au |
q | .7557505099313004 | 3.8264e-08 | au |
i | .1854206398826393 | 4.7668e-07 | deg |
node | 9.115842810022306 | 0.00095026 | deg |
peri | 296.1065059837813 | 0.00094762 | deg |
M | 129.9863557285085 | 3.4849e-05 | deg |
tp | 2459090.713686747852 (2020-Aug-29.21368675) | 2.9148e-05 | TDB |
period | 304.0555491325698 0.83 | 1.0455e-06 2.862e-09 | d yr |
n | 1.183994178126439 | 4.0714e-09 | deg/d |
Q | 1.014085390408132 | 2.3247e-09 | au |
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Additional Model Parameters
Parameter | Value | Uncertainty (1-sigma) |
A2 [EST] | 4.36257230382443E-12 | 3.548E-13 |
ALN [SET] | 1. | n/a |
NK [SET] | 0. | n/a |
NM [SET] | 2. | n/a |
R0 [SET] | 1. | n/a |
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| | Orbit Determination Parameters
Additional Information
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[ hide covariance matrix ]
Orbital Elements at Epoch 2458722.5 (2019-Aug-27.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | .1446635952342707 | 4.4743e-08 | |
q | .7576577186961364 | 4.4103e-08 | au |
tp | 2458786.217878843947 (2019-Oct-29.71787884) | 3.0021e-05 | TDB |
node | 10.37707106224867 | 0.00093377 | deg |
peri | 295.0989327248448 | 0.0009305 | deg |
i | .1870581014977314 | 4.5052e-07 | deg |
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Additional Model Parameters
Parameter | Value | Uncertainty (1-sigma) |
A2 [EST] | 4.36257230382443E-12 | 3.548E-13 |
ALN [SET] | 1. | n/a |
NK [SET] | 0. | n/a |
NM [SET] | 2. | n/a |
R0 [SET] | 1. | n/a |
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| | Orbit Determination Parameters
Additional Information
Jupiter MOID = 4.0935 au |
T_jup = 6.696 |
Nongravitational accels. using nonstandard g(r) = (1 au/ r)^2 |
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Orbit Covariance (7×7)
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|
e |
q |
tp |
node |
peri |
i |
A2 |
e |
2.001961924297702E-15 |
-1.776916691342938E-15 |
1.156936300241902E-12 |
7.851410324546563E-12 |
-6.894411776112626E-12 |
1.543874342048723E-15 |
1.588823057410195E-24 |
q |
-1.776916691342938E-15 |
1.945033536664681E-15 |
-1.182611499687015E-12 |
9.21839192362177E-12 |
-1.009343704534056E-11 |
-4.536309379373334E-15 |
-6.798660255161573E-21 |
tp |
1.156936300241902E-12 |
-1.182611499687015E-12 |
9.012480691370931E-10 |
-1.555354320387771E-9 |
2.276237995717057E-9 |
7.51752460569538E-13 |
3.081438125203585E-18 |
node |
7.851410324546563E-12 |
9.21839192362177E-12 |
-1.555354320387771E-9 |
8.719257072936367E-7 |
-8.685742356259342E-7 |
-2.130381499870001E-10 |
-2.976470196171073E-16 |
peri |
-6.894411776112626E-12 |
-1.009343704534056E-11 |
2.276237995717057E-9 |
-8.685742356259342E-7 |
8.658299962405507E-7 |
2.125875960254425E-10 |
2.983112617355926E-16 |
i |
1.543874342048723E-15 |
-4.536309379373334E-15 |
7.51752460569538E-13 |
-2.130381499870001E-10 |
2.125875960254425E-10 |
2.029718994184435E-13 |
5.58819097062408E-20 |
A2 |
1.588823057410195E-24 |
-6.798660255161573E-21 |
3.081438125203585E-18 |
-2.976470196171073E-16 |
2.983112617355926E-16 |
5.58819097062408E-20 |
1.258666812606349E-25 |
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Physical Parameter Table
Parameter |
Symbol |
Value |
Units |
Sigma |
Reference |
Notes |
absolute magnitude |
H |
27.34 |
|
n/a |
E2021B69 |
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