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(2015 JC1)
Classification: Apollo [NEO]          SPK-ID: 3719182
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5189100992940539 0.00055089  
a 1.393878307438805 0.0011106 au
q .6705807765219068 0.00023359 au
i 6.376842419589049 0.0071204 deg
node 231.769550200001 6.1401e-05 deg
peri 266.8700347429045 0.0017149 deg
M 60.36573226131299 1.4072 deg
tp 2458899.708551112929
(2020-Feb-20.20855111)
2.2291 TDB
period 601.0847585228377
1.65
0.71837
0.001967
d
yr
n .5989171991063256 0.00071578 deg/d
Q 2.117175838355703 0.0016869 au
  Orbit Determination Parameters
   # obs. used (total)      48  
   data-arc span      10 days  
   first obs. used      2015-05-12  
   last obs. used      2015-05-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .50428  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:33:49  

Additional Information
 Earth MOID = .000328495 au 
 Jupiter MOID = 2.95209 au 
 T_jup = 4.612 
[ 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 27.1   n/a MPO337172  

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