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JPL Small-Body Database Browser
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(2019 VM1)
Classification: Apollo [NEO]          SPK-ID: 3892315
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 2458791.5 (2019-Nov-04.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3082817088964946 0.0019531  
a 1.464453067077118 0.0042789 au
q 1.012988972959871 0.00014327 au
i 8.463767391646071 0.068025 deg
node 49.66570738486399 0.03513 deg
peri 1.200088957973974 0.21358 deg
M 355.2370622220332 0.087967 deg
tp 2458800.064145182772
(2019-Nov-12.56414518)
0.16 TDB
period 647.3089529030157
1.77
2.837
0.007767
d
yr
n .5561486495521061 0.0024375 deg/d
Q 1.915917161194364 0.005598 au
  Orbit Determination Parameters
   # obs. used (total)      11  
   data-arc span      1 day  
   first obs. used      2019-11-03  
   last obs. used      2019-11-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .43344  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-04 09:12:03  

Additional Information
 Earth MOID = .0232246 au 
 Jupiter MOID = 3.46182 au 
 T_jup = 4.551 
[ 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 26.309   .50486 1 autocmod 2.8

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