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JPL Small-Body Database Browser
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(2016 VN3)
Classification: Apollo [NEO]          SPK-ID: 3763477
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 2457701.5 (2016-Nov-09.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6412165481762826 0.0010298  
a 1.999602402414374 0.0050565 au
q .7174242522132271 0.00024505 au
i 10.22783422517296 0.014624 deg
node 46.11207545999903 6.5926e-05 deg
peri 78.13888184525939 0.0029163 deg
M 343.0604456432975 0.073801 deg
tp 2457750.097438818694
(2016-Dec-27.59743882)
0.027391 TDB
period 1032.794464737944
2.83
3.9175
0.01073
d
yr
n .3485688704686703 0.0013222 deg/d
Q 3.281780552615521 0.0082988 au
  Orbit Determination Parameters
   # obs. used (total)      37  
   data-arc span      3 days  
   first obs. used      2016-11-08  
   last obs. used      2016-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .56519  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:22:19  

Additional Information
 Earth MOID = .0156186 au 
 Jupiter MOID = 1.94412 au 
 T_jup = 3.538 
[ 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 MPO389567  

[ 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
1949-Apr-20 17:40 3_15:31 Earth 0.194202467182094 0.103065629545293 0.297661383631998 22.540799478525 22.5401907913349 2433027.235904936 5250.71082217064 5439243.63266882 580.182717855512 -23.0308774370242 18997.0371352453 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 15:16:06 2018-Dec-11 17:05
2016-Nov-12 21:39 < 00:01 Earth 0.0157161375779147 0.0156461026017768 0.0157861718695431 17.6009205540653 17.5912855913691 2457705.402168937 0.150266935019033 3488.50994721201 13.1046632866026 -0.00347043410378743 522.012760524129 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 15:16:06 2018-Dec-11 17:05
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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