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(2015 VD105)
Classification: Apollo [NEO]          SPK-ID: 3734470
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6482905724440614 0.00055067  
a 2.475861551078959 0.0036172 au
q .870783848837739 9.1196e-05 au
i 1.131132180710779 0.00072429 deg
node 124.3187177019491 0.021675 deg
peri 335.7058962274081 0.020199 deg
M 51.1981004003494 0.90531 deg
tp 2458798.133180088311
(2019-Nov-10.63318009)		 3.1349 TDB
period 1422.944495958507
3.90		 3.1183
0.008537		 d
yr
n .2529965160429544 0.00055443 deg/d
Q 4.080939253320179 0.0059622 au
   Orbit Determination Parameters
   # obs. used (total)      68  
   data-arc span      26 days  
   first obs. used      2015-10-18  
   last obs. used      2015-11-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .54256  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Apr-18 07:27:05  

Additional Information
 Earth MOID = .007106 au 
 Jupiter MOID = 1.12249 au 
 T_jup = 3.152 
[ 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 24.7   n/a MPO466771  

[ 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
2015-Nov-16 23:50 < 00:01 Earth 0.0185539333223663 0.0185106056373515 0.018597260660605 12.7404189411322 12.7291421665379 2457343.492875776 0.274063333075508 2156.85879982049 4.64951173254329 -0.400346578703255 1419.65624677833 T 7 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:11 2019-Apr-18 07:27
2063-Feb-25 16:25 8_05:27 Mars 0.0902024756516488 0.00509815775333222 0.214221315144991 15.8198448695528 15.8196442430684 2474611.183697638 11847.3868892538 6188490.43494189 31.354774508805 3.24086678511532 24383.5181642012 T 7 CATAB v2.0e-lin.ifort 2019-Apr-18 07:27:11 2019-Apr-18 07:27
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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