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(2015 XG352)
Classification: Apollo [NEO]          SPK-ID: 3736682
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3963861285111911 0.0007498  
a 1.070593341030714 0.00065741 au
q .6462249913696878 0.00040616 au
i 12.66572995563818 0.026213 deg
node 249.8477989635945 0.0010124 deg
peri 75.92442793275862 0.01191 deg
M 77.76482837305231 1.4461 deg
tp 2458913.099090764944
(2020-Mar-04.59909076)
1.5447 TDB
period 404.6087155710035
1.11
0.37268
0.00102
d
yr
n .8897485055208227 0.00081954 deg/d
Q 1.49496169069174 0.000918 au
  Orbit Determination Parameters
   # obs. used (total)      14  
   data-arc span      11 days  
   first obs. used      2015-12-07  
   last obs. used      2015-12-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .22683  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:29:52  

Additional Information
 Earth MOID = .00594117 au 
 Jupiter MOID = 3.87567 au 
 T_jup = 5.673 
[ 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 25.5   n/a MPO358610  

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