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(2016 TO11)
Classification: Apollo [NEO]          SPK-ID: 3760526
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.


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 
[ 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 27.3   n/a E2016U05  

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2016-Oct-12 10:55 00:02 Moon 0.00586024735649458 0.0058308252775937 0.00588967301997478 9.97217596697292 9.97161514489463 2457673.954673226 2.31919022812973 1484.94425114466 3.54729483417915 -8.89404305021235 35542.7971081513 T 6 CATAB v2.0e-lin.ifort 2017-Nov-30 14:25:15 2018-Dec-11 17:03
2016-Oct-12 19:01 < 00:01 Earth 0.00599207275291651 0.00596136590639896 0.00602277673451921 9.79758421206788 9.75209319158006 2457674.292328012 0.0928701948274017 1517.08484741183 3.70754965641016 -0.286581597354936 374.595745214811 T 6 CATAB v2.0e-lin.ifort 2017-Nov-30 14:25:15 2018-Dec-11 17:03
2019-Sep-18 05:45 9_23:01 Earth 0.253844521639776 0.0716813928766158 0.436384111676334 17.4635146347431 17.4629135712055 2458744.739317129 14340.9770339157 9106186.52823425 14.0386802290138 -2.17337816263951 94661.7658131263 T 6 CATAB v2.0e-lin.ifort 2017-Nov-30 14:25:15 2018-Dec-11 17:03
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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