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(2016 TO11)
Classification: Apollo [NEO]          SPK-ID: 3760526
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2457668.5 (2016-Oct-07.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5470512818890449 0.0010214  
a 2.069345027185258 0.0045088 au
q .9373071773928422 7.1447e-05 au
i 4.361044208463734 0.0062264 deg
node 196.1684466762755 0.00074389 deg
peri 218.4947728796621 0.00085653 deg
M 349.139376465435 0.038999 deg
tp 2457701.301979100012
(2016-Nov-08.80197910)
0.010584 TDB
period 1087.295995337832
2.98
3.5536
0.009729
d
yr
n .3310965933321082 0.0010821 deg/d
Q 3.201382876977674 0.0069753 au
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      5 days  
   first obs. used      2016-10-06  
   last obs. used      2016-10-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .58306  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:23:17  

Additional Information
 Earth MOID = .00559097 au 
 Jupiter MOID = 2.18972 au 
 T_jup = 3.567 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 1.043311229514889E-6 -7.297507584533005E-8 -1.081013960348324E-5 -7.595331506229636E-7 8.67483377722512E-7 6.359691425778931E-6
q -7.297507584533005E-8 5.104614340831981E-9 7.56076757582681E-7 5.311681568812246E-8 -6.07387566539121E-8 -4.448151550455997E-7
tp -1.081013960348324E-5 7.56076757582681E-7 .0001120144293622381 7.871025473823083E-6 -8.97941007298614E-6 -6.589741729372129E-5
node -7.595331506229636E-7 5.311681568812246E-8 7.871025473823083E-6 5.533795033828215E-7 -6.300223417557871E-7 -4.630503688469157E-6
peri 8.67483377722512E-7 -6.07387566539121E-8 -8.97941007298614E-6 -6.300223417557871E-7 7.336363284251753E-7 5.284883908522527E-6
i 6.359691425778931E-6 -4.448151550455997E-7 -6.589741729372129E-5 -4.630503688469157E-6 5.284883908522527E-6 3.876820067760381E-5

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 27.3   n/a E2016U05  

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