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JPL Small-Body Database Browser
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(2015 BC)
Classification: Apollo [NEO]          SPK-ID: 3703786
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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5763112868657446 0.00039594  
a 1.255132235960438 0.00075229 au
q .5317853618673984 0.00017826 au
i 13.1213344084475 0.010491 deg
node 119.5696055622842 0.00013565 deg
peri 105.0663618602379 0.0034969 deg
M 334.5235458598006 0.94089 deg
tp 2458636.847047106163
(2019-Jun-02.34704711)
1.375 TDB
period 513.6090323327954
1.41
0.46176
0.001264
d
yr
n .7009222527977979 0.00063017 deg/d
Q 1.978479110053477 0.0011858 au
  Orbit Determination Parameters
   # obs. used (total)      91  
   data-arc span      3 days  
   first obs. used      2015-01-16  
   last obs. used      2015-01-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .25875  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:36:19  

Additional Information
 Earth MOID = .000834336 au 
 Jupiter MOID = 3.07445 au 
 T_jup = 4.927 
[ 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 24.0   n/a MPCxxxxx  

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