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(2015 FC34)
Classification: Apollo [NEO]          SPK-ID: 3713948
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 2457103.5 (2015-Mar-22.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5822310488292919 0.0020023  
a 1.695087429332993 0.0064503 au
q .7081548974950962 0.00069935 au
i 11.16411539651434 0.035727 deg
node 185.5325241605553 0.011905 deg
peri 79.97744672609458 0.011543 deg
M 333.8103522822115 0.17574 deg
tp 2457162.142670278098
(2015-May-19.64267028)
0.058786 TDB
period 806.0956576279592
2.21
4.6011
0.0126
d
yr
n .446597121065441 0.0025492 deg/d
Q 2.682019961170889 0.010206 au
  Orbit Determination Parameters
   # obs. used (total)      49  
   data-arc span      10 days  
   first obs. used      2015-03-20  
   last obs. used      2015-03-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .42113  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Feb-10 07:06:23  

Additional Information
 Earth MOID = .006718 au 
 Jupiter MOID = 2.50686 au 
 T_jup = 3.980 
[ 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 23.0   n/a MPO332798  

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