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JPL Small-Body Database Browser
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(2016 LV)
Classification: Apollo [NEO]          SPK-ID: 3753664
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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5360975410533484 0.00020367  
a 2.005831086352748 0.0008378 au
q .9305099731906731 1.9885e-05 au
i 2.128185707786705 0.00064208 deg
node 83.73309408685232 0.00030286 deg
peri 126.7555060175775 0.00039708 deg
M 18.45483056698647 0.24016 deg
tp 2458547.307852406247
(2019-Mar-04.80785241)
0.6589 TDB
period 1037.623892792969
2.84
0.65009
0.00178
d
yr
n .3469465212785232 0.00021737 deg/d
Q 3.081152199514822 0.0012869 au
  Orbit Determination Parameters
   # obs. used (total)      188  
   data-arc span      14 days  
   first obs. used      2016-06-03  
   last obs. used      2016-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .3072  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:37  

Additional Information
 Earth MOID = .00832246 au 
 Jupiter MOID = 1.8847 au 
 T_jup = 3.642 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457544.5 (2016-Jun-05.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5366456793972226 0.00020537  
q .9302852022308417 2.0609e-05 au
tp 2457509.455165608083
(2016-Apr-30.95516561)
0.0027152 TDB
node 83.74948320249908 0.00034878 deg
peri 126.6823164959047 0.00042749 deg
i 2.125840513540338 0.00064351 deg
  Orbit Determination Parameters
   # obs. used (total)      188  
   data-arc span      14 days  
   first obs. used      2016-06-03  
   last obs. used      2016-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .3072  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:37  

Additional Information
 Jupiter MOID = 1.8847 au 
 T_jup = 3.642 
Orbit Covariance (6×6)
  e q tp node peri i
e 4.217875326955195E-8 -4.230951119826715E-9 5.57424654699058E-7 6.598619919968746E-8 -7.479834640174479E-8 1.318891045964773E-7
q -4.230951119826715E-9 4.247211027792857E-10 -5.587489023808865E-8 -6.666200273264893E-9 7.614733417437282E-9 -1.321309138842097E-8
tp 5.57424654699058E-7 -5.587489023808865E-8 7.372126960579717E-6 8.66519153202107E-7 -9.745290340730939E-7 1.744936719762616E-6
node 6.598619919968746E-8 -6.666200273264893E-9 8.66519153202107E-7 1.216479705908775E-7 -1.445608146366915E-7 2.009538861759086E-7
peri -7.479834640174479E-8 7.614733417437282E-9 -9.745290340730939E-7 -1.445608146366915E-7 1.827464386984727E-7 -2.25317341982841E-7
i 1.318891045964773E-7 -1.321309138842097E-8 1.744936719762616E-6 2.009538861759086E-7 -2.25317341982841E-7 4.141056163461118E-7

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 23.1   n/a MPO386982  

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