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(2017 SQ10)
Classification: Amor [NEO]          SPK-ID: 3781646
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5755671018414121 0.0017486  
a 2.42584600474742 0.010195 au
q 1.029608850281379 8.5456e-05 au
i .8169441820986071 0.0018032 deg
node 218.1862218983979 0.016387 deg
peri 159.7945279339431 0.017828 deg
M 355.7623529158649 0.028782 deg
tp 2458034.744844307421
(2017-Oct-08.24484431)
0.007935 TDB
period 1380.045066179733
3.78
8.7
0.02382
d
yr
n .2608610463689849 0.0016445 deg/d
Q 3.822083159213461 0.016063 au
  Orbit Determination Parameters
   # obs. used (total)      31  
   data-arc span      9 days  
   first obs. used      2017-09-21  
   last obs. used      2017-09-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .47783  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Oct-01 06:50:13  

Additional Information
 Earth MOID = .0314614 au 
 Jupiter MOID = 1.6387 au 
 T_jup = 3.262 
[ 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 26.2   n/a MPO416678  

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