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(2015 VC2)
Classification: Apollo [NEO]          SPK-ID: 3733264
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 36 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07441545637252053 7.9969e-08  
a 1.05308683643572 8.5967e-08 au
q .9747208989024618 6.4091e-09 au
i .8678029081284628 5.456e-07 deg
node 186.1706486881762 2.9507e-05 deg
peri 288.2107000019306 2.5393e-05 deg
M 16.97357529829234 0.00019369 deg
tp 2458981.889178932800
(2020-May-12.38917893)
0.0002101 TDB
period 394.7250633086231
1.08
4.8334e-05
1.323e-07
d
yr
n .9120272145438288 1.1168e-07 deg/d
Q 1.131452773968978 9.2364e-08 au
  Orbit Determination Parameters
   # obs. used (total)      110  
   data-arc span      189 days  
   first obs. used      2015-11-03  
   last obs. used      2016-05-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .73382  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-18 07:24:06  

Additional Information
 Earth MOID = .00779483 au 
 Jupiter MOID = 3.87742 au 
 T_jup = 5.838 
[ 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 27.4   n/a MPO361296  

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