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(2017 SP10)
Classification: Amor [NEO]          SPK-ID: 3781648
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 2458018.5 (2017-Sep-22.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5142979466079661 0.00088975  
a 2.108173913238922 0.0039389 au
q 1.023944398567664 3.7363e-05 au
i 11.24747692223477 0.013229 deg
node 181.5700536752415 0.00039207 deg
peri 194.1379656198922 0.0033482 deg
M 355.31466067322 0.014977 deg
tp 2458033.051126891679
(2017-Oct-06.55112689)
0.0057347 TDB
period 1118.041899561754
3.06
3.1334
0.008579
d
yr
n .3219915104622746 0.0009024 deg/d
Q 3.192403427910181 0.0059646 au
  Orbit Determination Parameters
   # obs. used (total)      39  
   data-arc span      11 days  
   first obs. used      2017-09-19  
   last obs. used      2017-09-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .50372  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Oct-01 06:50:13  

Additional Information
 Earth MOID = .0300769 au 
 Jupiter MOID = 2.26652 au 
 T_jup = 3.539 
[ 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 26.1   n/a MPO416678  

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