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(2016 BV)
Classification: Apollo [NEO]          SPK-ID: 3740669
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 2457407.5 (2016-Jan-20.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5081231408756123 0.001613  
a 1.793600869892915 0.0053569 au
q .8822307624056965 0.00025823 au
i 3.692838989969944 0.0093697 deg
node 111.5423339272996 0.0010754 deg
peri 316.8333434483249 0.0094416 deg
M 16.17385628802797 0.079868 deg
tp 2457368.081670559324
(2015-Dec-11.58167056)
0.018062 TDB
period 877.3787985953211
2.40
3.9307
0.01076
d
yr
n .4103130832160045 0.0018382 deg/d
Q 2.704970977380134 0.0080789 au
  Orbit Determination Parameters
   # obs. used (total)      27  
   data-arc span      12 days  
   first obs. used      2016-01-18  
   last obs. used      2016-01-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .37625  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:28:59  

Additional Information
 Earth MOID = .0031223 au 
 Jupiter MOID = 2.63187 au 
 T_jup = 3.910 
[ 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 26.0   n/a MPO365063  

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