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(2017 NT5)
Classification: Apollo [NEO]          SPK-ID: 3776550
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6759574888889958 0.00025612  
a 1.86811796140058 0.0012197 au
q .6053496352638139 8.3217e-05 au
i 6.03933881945618 0.0019738 deg
node 293.5692124638206 0.00010464 deg
peri 88.9389402695779 0.0012282 deg
M 26.9454967219054 0.37431 deg
tp 2458930.694673277179
(2020-Mar-22.19467328)
0.90132 TDB
period 932.6203142429366
2.55
0.9134
0.002501
d
yr
n .3860091770488973 0.00037805 deg/d
Q 3.130886287537345 0.0020442 au
  Orbit Determination Parameters
   # obs. used (total)      86  
   data-arc span      21 days  
   first obs. used      2017-06-23  
   last obs. used      2017-07-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .22404  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Jul-15 06:18:59  

Additional Information
 Earth MOID = .00224189 au 
 Jupiter MOID = 2.38672 au 
 T_jup = 3.664 
[ 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 22.9   n/a MPO416462  

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