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(2016 OV)
Classification: Apollo [NEO]          SPK-ID: 3756107
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 2457600.5 (2016-Jul-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6538003399440255 0.0011175  
a 2.702747118773513 0.0084756 au
q .9356901337366548 8.5954e-05 au
i 10.47556528700547 0.01204 deg
node 133.2127202299409 0.0017821 deg
peri 213.9854885244756 0.00050906 deg
M 352.8669759033157 0.03587 deg
tp 2457632.657163725642
(2016-Sep-01.15716373)
0.010446 TDB
period 1622.955254926487
4.44
7.6342
0.0209
d
yr
n .2218175756276821 0.0010434 deg/d
Q 4.469804103810372 0.014017 au
  Orbit Determination Parameters
   # obs. used (total)      34  
   data-arc span      7 days  
   first obs. used      2016-07-28  
   last obs. used      2016-08-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .33484  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:24:49  

Additional Information
 Earth MOID = .00670624 au 
 Jupiter MOID = 1.02518 au 
 T_jup = 2.998 
[ 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 24.6   n/a MPO384702  

[ 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
1920-Nov-11 00:14 4_06:52 Jupiter 1.82505024542553 1.72930405379317 1.92100559575542 7.28457652234534 7.22058424315015 2422639.509881226 6171.65596362695 4880024.29613634 663.591201183153 -6.04047787684115 60247.7786464694 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 13:26:28 2018-Dec-11 17:01
1922-Oct-30 13:33 5_09:10 Earth 0.351563241107098 0.317737842385888 0.38661580042951 19.2915530508941 19.291160183372 2423358.064797568 7750.38868597591 2005735.58711277 121.798580745739 30.9418394744317 210101.022117153 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 13:26:28 2018-Dec-11 17:01
2016-Aug-07 10:42 < 00:01 Earth 0.0232356377311185 0.0231343453192965 0.0233369288485726 12.4703784240559 12.461179472355 2457607.946108750 0.129627822089733 5043.59674835004 5.38513575661169 -0.0116001977252531 476.785301814073 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 13:26:28 2018-Dec-11 17:01
2098-Nov-23 04:45 4_13:26 Jupiter 1.96279869008458 1.9309734973156 1.99470163020256 8.10297663090527 8.04954371257926 2487665.698071267 6565.99568660756 1705293.81224555 930.935598217287 -18.5857180190237 160372.154374435 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 13:26:28 2018-Dec-11 17:01
2100-Jul-19 03:54 8_07:23 Earth 0.0681215629546651 0.0278861289965849 0.126306619442 16.3141950015067 16.311797306056 2488268.662384593 11963.1089334703 3043473.05882543 56.0699046533877 -24.1513027560319 89066.0678183902 T 9 CATAB v2.0e-lin.ifort 2017-Nov-30 13:26:28 2018-Dec-11 17:01
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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