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JPL Small-Body Database Browser
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(2014 LL26)
Classification: Amor [NEO]          SPK-ID: 3673787
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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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.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1018956818918404 0.00012874  
a 1.142982679876849 0.00017362 au
q 1.026517680320234 8.783e-06 au
i 9.189951498982104 0.0075826 deg
node 258.1973275858404 0.00025702 deg
peri 13.48833396884741 0.0016808 deg
M 346.9229981271174 0.32478 deg
tp 2458616.713007594055
(2019-May-13.21300759)
0.40636 TDB
period 446.3318725956065
1.22
0.1017
0.0002784
d
yr
n .8065747084259285 0.00018378 deg/d
Q 1.259447679433464 0.00019131 au
  Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      12 days  
   first obs. used      2014-06-09  
   last obs. used      2014-06-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .42738  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:04  

Additional Information
 Earth MOID = .0135454 au 
 Jupiter MOID = 3.78004 au 
 T_jup = 5.473 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456824.5 (2014-Jun-16.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1024305018017868 0.00012846  
q 1.026347923071754 9.2042e-06 au
tp 2456831.372032384128
(2014-Jun-22.87203238)
0.0017429 TDB
node 258.323692415166 4.0011e-05 deg
peri 13.23711824319483 0.0012406 deg
i 9.228735753989426 0.0075128 deg
  Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      12 days  
   first obs. used      2014-06-09  
   last obs. used      2014-06-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .42738  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:04  

Additional Information
 Jupiter MOID = 3.78004 au 
 T_jup = 5.473 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.65025014225428E-8 1.182293780107769E-9 -2.17729938092066E-7 -4.642209474553562E-9 -1.504298841357561E-7 9.650828502902156E-7
q 1.182293780107769E-9 8.471719743880861E-11 -1.563820462257782E-8 -3.322430757173536E-10 -1.081676535040908E-8 6.914637118973977E-8
tp -2.17729938092066E-7 -1.563820462257782E-8 3.037658184545551E-6 5.926339289838626E-8 2.150961719226038E-6 -1.273977484266095E-5
node -4.642209474553562E-9 -3.322430757173536E-10 5.926339289838626E-8 1.600842712485033E-9 4.004900111444857E-8 -2.710691076766047E-7
peri -1.504298841357561E-7 -1.081676535040908E-8 2.150961719226038E-6 4.004900111444857E-8 1.539000803990139E-6 -8.8043708128577E-6
i 9.650828502902156E-7 6.914637118973977E-8 -1.273977484266095E-5 -2.710691076766047E-7 -8.8043708128577E-6 5.64422472308211E-5

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 25.3   n/a E2014M12  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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