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JPL Small-Body Database Browser
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(2020 DV3)
Classification: Apollo [NEO]          SPK-ID: 54005666
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4691035012237648 0.00033672  
a 1.481975542435798 0.00074367 au
q .786775626751177 0.00010422 au
i 1.086269652999826 0.00072021 deg
node 164.2341707110939 0.00048166 deg
peri 282.5453481728775 0.0012176 deg
M 78.24682880271494 0.06421 deg
tp 2458857.273220719248
(2020-Jan-08.77322072)
0.009725 TDB
period 658.9614087885133
1.80
0.49601
0.001358
d
yr
n .5463142381309589 0.00041122 deg/d
Q 2.177175458120418 0.0010925 au
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      6 days  
   first obs. used      2020-02-27  
   last obs. used      2020-03-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .5287  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-04 05:53:00  

Additional Information
 Earth MOID = .0027235 au 
 Jupiter MOID = 3.06516 au 
 T_jup = 4.454 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458907.5 (2020-Feb-28.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4695470461455016 0.00033617  
q .7865619695915046 0.00010385 au
tp 2458857.291128222362
(2020-Jan-08.79112822)
0.0097023 TDB
node 164.2387476995792 0.00047993 deg
peri 282.5355475208864 0.0011964 deg
i 1.085682386141208 0.00072101 deg
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      6 days  
   first obs. used      2020-02-27  
   last obs. used      2020-03-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .5287  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-04 05:53:00  

Additional Information
 Jupiter MOID = 3.06516 au 
 T_jup = 4.454 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.130128737807865E-7 -3.490532783225938E-8 3.261345430896519E-6 4.000545456794555E-8 -3.395798176222218E-7 2.383532244620092E-7
q -3.490532783225938E-8 1.078523946915356E-8 -1.007099020787212E-6 -1.2774510038034E-8 1.059546068154555E-7 -7.346001486618407E-8
tp 3.261345430896519E-6 -1.007099020787212E-6 9.413412699369226E-5 1.153616656758992E-6 -9.759944342010286E-6 6.878453021163731E-6
node 4.000545456794555E-8 -1.2774510038034E-8 1.153616656758992E-6 2.303345691911121E-7 -3.806368953239687E-7 2.759478175587292E-8
peri -3.395798176222218E-7 1.059546068154555E-7 -9.759944342010286E-6 -3.806368953239687E-7 1.431479221208208E-6 -6.430025269136443E-7
i 2.383532244620092E-7 -7.346001486618407E-8 6.878453021163731E-6 2.759478175587292E-8 -6.430025269136443E-7 5.198547758502308E-7

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 27.842   .38734 4 autocmod 2.8

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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