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JPL Small-Body Database Browser
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(2019 VD)
Classification: Apollo [NEO]          SPK-ID: 3892193
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6468714774783925 0.00071707  
a 2.541147399866165 0.0049579 au
q .8973516268243635 7.1401e-05 au
i .09614451557469124 8.6642e-05 deg
node 11.3392014150887 0.0086307 deg
peri 70.73515903631733 0.009541 deg
M 306.3006538845377 0.15888 deg
tp 2458821.203748409249
(2019-Dec-03.70374841)		 0.0070891 TDB
period 1479.596218108357
4.05		 4.3302
0.01186		 d
yr
n .2433096243380879 0.00071207 deg/d
Q 4.184943172907967 0.0081651 au
   Orbit Determination Parameters
   # obs. used (total)      35  
   data-arc span      6 days  
   first obs. used      2019-10-28  
   last obs. used      2019-11-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .49048  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-04 08:43:34  

Additional Information
 Earth MOID = .000867335 au 
 Jupiter MOID = 1.09768 au 
 T_jup = 3.113 
[ 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 27.419   .40234 3 autocmod 2.8

[ 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
1907-Jul-28 07:16 8_23:10 Venus 0.106079269423556 0.0136564378261726 0.216362823803872 9.61035964539286 9.60822931519871 2417784.802491408 12910.2993195158 5521661.4501308 294.938844540356 -7.4164875562168 7084.8711358056 T 3 CATAB v2.0f-lin.ifort 2019-Nov-04 08:44:32 2019-Nov-04 08:44
2019-Nov-04 05:17 < 00:01 Moon 0.00177278316049732 0.00177196194842373 0.00177361160079047 12.8043791931978 12.8029353198045 2458791.720471265 0.743317145780802 183.280523977681 1.31768838555602 -77.0204807773603 187923.969406237 T 3 CATAB v2.0f-lin.ifort 2019-Nov-04 08:44:32 2019-Nov-04 08:44
2019-Nov-04 09:56 < 00:01 Earth 0.00116504286978668 0.00116141158566869 0.00116867348096283 12.0033612296879 11.8112927180457 2458791.913861702 0.0678024670019335 175.500689860897 1.42881709608568 1.67561797097044 651.374701571962 T 3 CATAB v2.0f-lin.ifort 2019-Nov-04 08:44:32 2019-Nov-04 08:44
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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