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(2016 LB)
Classification: Apollo [NEO]          SPK-ID: 3753623
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .146105443284731 7.5264e-07  
a 1.011909955245253 3.9568e-08 au
q .8640644026699129 7.6715e-07 au
i 32.18210676746048 8.6305e-05 deg
node 72.95475657852322 2.8701e-06 deg
peri 76.47967458983311 3.3975e-05 deg
M 57.99784405039161 0.00010976 deg
tp 2458940.600861140533
(2020-Apr-01.10086114)
0.00011045 TDB
period 371.8015788771802
1.02
2.1808e-05
5.971e-08
d
yr
n .9682583949406017 5.6792e-08 deg/d
Q 1.159755507820593 4.535e-08 au
  Orbit Determination Parameters
   # obs. used (total)      134  
   data-arc span      742 days (2.03 yr)  
   first obs. used      2016-05-30  
   last obs. used      2018-06-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .40807  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Jun-12 06:23:10  

Additional Information
 Earth MOID = .0105689 au 
 Jupiter MOID = 3.98314 au 
 T_jup = 5.881 
[ 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 22.8   n/a MPO381207  
diameter diameter 0.060 km 0.016 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  
geometric albedo albedo 0.526   0.121 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  

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