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(2007 XB10)
Classification: Apollo [NEO]          SPK-ID: 3397575
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 29 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5997765838198598 1.3673e-07  
a 2.209763025277374 9.9793e-08 au
q .8843989069250723 2.9835e-07 au
i 41.32789358668052 5.4674e-05 deg
node 261.1390500001662 1.8653e-05 deg
peri 37.24486939890006 2.7994e-05 deg
M 3.986206561523977 7.0696e-05 deg
tp 2458987.214610867587
(2020-May-17.71461087)
0.00023473 TDB
period 1199.822441173261
3.28
8.1276e-05
2.225e-07
d
yr
n .3000443962758102 2.0325e-08 deg/d
Q 3.535127143629676 1.5965e-07 au
  Orbit Determination Parameters
   # obs. used (total)      76  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      4610 days (12.62 yr)  
   first obs. used      2007-12-05  
   last obs. used      2020-07-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .67563  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jul-20 06:28:52  

Additional Information
 Earth MOID = .0540851 au 
 Jupiter MOID = 2.06949 au 
 T_jup = 3.138 
[ 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 17.7   n/a MPO264973  

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