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(2019 VT3)
Classification: Apollo [NEO]          SPK-ID: 3892702
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1317033945984103 0.00010827  
a 1.037217262985267 6.6069e-05 au
q .900612228514035 5.617e-05 au
i 7.814221717352615 0.0071416 deg
node 40.73350703644434 0.00064147 deg
peri 92.13657355409303 0.0051541 deg
M 305.0755168285566 0.020139 deg
tp 2459259.366268857001
(2021-Feb-13.86626886)
0.027207 TDB
period 385.8362530671656
1.06
0.036866
0.0001009
d
yr
n .9330382957490827 8.915e-05 deg/d
Q 1.173822297456498 7.4771e-05 au
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      3 days  
   first obs. used      2019-11-05  
   last obs. used      2019-11-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .6386  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-08 05:49:44  

Additional Information
 Earth MOID = .00411164 au 
 Jupiter MOID = 3.83528 au 
 T_jup = 5.894 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458793.5 (2019-Nov-06.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1313782286815041 0.00010892  
q .9011438766353896 5.6836e-05 au
tp 2458873.663368654739
(2020-Jan-25.16336865)
0.010255 TDB
node 40.90090781987077 0.00020686 deg
peri 92.02099762208213 0.0050679 deg
i 7.870890589223838 0.0070424 deg
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      3 days  
   first obs. used      2019-11-05  
   last obs. used      2019-11-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .6386  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-08 05:49:44  

Additional Information
 Jupiter MOID = 3.83528 au 
 T_jup = 5.894 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.186455052259299E-8 -6.123498263696763E-9 -1.102111219208849E-6 1.986402477672317E-8 -4.680906801460467E-7 7.532398527921044E-7
q -6.123498263696763E-9 3.23032315829789E-9 5.557950067424531E-7 -9.513948088688854E-9 2.196080147651748E-7 -3.783889081758141E-7
tp -1.102111219208849E-6 5.557950067424531E-7 .0001051622489998376 -1.963232196885906E-6 4.790681269660707E-5 -7.16188654843968E-5
node 1.986402477672317E-8 -9.513948088688854E-9 -1.963232196885906E-6 4.279024276052366E-8 -9.986690715944553E-7 1.388752479334241E-6
peri -4.680906801460467E-7 2.196080147651748E-7 4.790681269660707E-5 -9.986690715944553E-7 2.568384303910996E-5 -3.272293948156787E-5
i 7.532398527921044E-7 -3.783889081758141E-7 -7.16188654843968E-5 1.388752479334241E-6 -3.272293948156787E-5 4.959478938945234E-5

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 28.2   .32818 E2019-VC6 autocmod 2.8

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