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(2013 LR6)
Classification: Apollo [NEO]          SPK-ID: 3639547
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5218809038161129 9.1717e-05  
a 2.015056125092568 0.00037402 au
q .9634368132890643 6.0343e-06 au
i 2.524762720858704 0.00082956 deg
node 76.37764030003764 5.9032e-05 deg
peri 213.5097178244426 0.0010147 deg
M 149.1892278817625 0.24274 deg
tp 2458567.523711924873
(2019-Mar-25.02371192)
0.58393 TDB
period 1044.790337212409
2.86
0.29089
0.0007964
d
yr
n .3445667395436594 9.5934e-05 deg/d
Q 3.066675436896071 0.00056921 au
  Orbit Determination Parameters
   # obs. used (total)      61  
   data-arc span      1 day  
   first obs. used      2013-06-06  
   last obs. used      2013-06-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .36113  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:45:39  

Additional Information
 Earth MOID = .00148851 au 
 Jupiter MOID = 2.14861 au 
 T_jup = 3.643 
[ show covariance matrix ]

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 27.8   n/a MPO263326  

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
1975-Sep-21 18:57 8_08:30 Earth 0.447534037858761 0.222644316447763 0.676822692118742 22.550896536449 22.5506325236297 2442677.289462503 12029.7216468429 11538665.1784351 253.360299156916 9.52653678855072 39796.5528865402 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
1986-May-05 23:21 6_03:53 Earth 0.395830232745403 0.239348404589967 0.552314000976494 21.212198228272 21.2118808910857 2446556.473156333 8872.52988185655 7803286.82808128 58.2336021547567 -0.424892416535916 6703.40724787625 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2013-Jun-08 04:42 < 00:01 Earth 0.000742427917160166 0.000742031110141263 0.000742824702368411 9.88192141358922 9.51181503598531 2456451.695511959 0.253551142364782 18.7063011208893 1.64634443693792 0.816393343764374 3759.03956624335 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2013-Jun-08 13:16 < 00:01 Moon 0.00173626357584418 0.00173613352636125 0.00173639371511879 10.264903313444 10.2630642904528 2456452.052786098 0.362882924157508 29.4083973989724 4.72276779552896 -81.1991190594404 63939.7878772827 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2045-Mar-24 13:23 6_21:13 Mars 0.0885721840599484 0.0283967161966663 0.193934196910934 12.772266700364 12.7720136277465 2468064.057656194 9913.42746928763 5382982.58596751 713.901662084576 18.7067767626044 5857.51618870531 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2056-May-03 17:12 4_10:28 Earth 0.437900461122083 0.319833583241236 0.555975949865653 22.5302492509962 22.5299791827272 2472122.216950467 6388.43444902797 5888528.7510545 144.112507192843 0.94928069021508 6832.67519620673 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2073-Sep-13 01:55 1_17:48 Earth 0.296456817242914 0.260615603060111 0.332417590488206 18.4442111915085 18.4437238913352 2478463.579911812 2507.5229191664 1814689.20578594 612.258254239525 9.35398195825912 10611.6982031795 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2076-May-12 15:33 1_01:37 Earth 0.273858807642249 0.252557113913182 0.295160646564001 17.8068289429468 17.8062825492003 2479436.148221404 1536.51095140852 1062279.50178359 138.367968757441 0.666355941192729 3053.53148722551 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2087-Jul-29 09:31 2_15:15 Mars 0.0665968531641813 0.0428659356850793 0.0935076759575573 10.5317910275449 10.5313828410221 2483530.896735502 3794.89515498193 1458487.59186249 872.150853704374 27.575720063842 5363.2155580091 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2093-Sep-19 06:33 2_15:04 Earth 0.412924941639541 0.345418626705928 0.480608833374754 21.7773758986925 21.7770795939193 2485774.772858356 3783.71285520063 3397636.91286874 609.62136877897 7.12846188133923 11421.4445873671 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2096-May-19 23:10 5_12:25 Earth 0.167563158378535 0.0877501644027308 0.247371879128779 14.63729001318 14.6362036144268 2486748.465492430 7944.81725119718 3979621.05307295 103.24761626405 -0.00104160305900055 5.68626161640846 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
2111-Jan-12 03:23 8_01:56 Mars 0.0803850688252258 0.0277221243043448 0.178433809144299 10.0220874757012 10.0217321060716 2492097.641073914 11635.9780867223 5027300.69326296 710.138205000529 -20.1816768364416 5990.9528848585 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 11:34:59 2018-Dec-11 16:03
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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