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JPL Small-Body Database Browser
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(2015 VM64)
Classification: Apollo [NEO]          SPK-ID: 3733853
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6194522801786934 0.00050971  
a 1.887689880847014 0.0022815 au
q .7183560798860853 9.3941e-05 au
i 16.31577060873238 0.01136 deg
node 46.12337614608884 0.00038044 deg
peri 76.63218388445127 0.0051862 deg
M 102.746111903251 0.82917 deg
tp 2458330.130751375220
(2018-Jul-30.63075138)
1.6917 TDB
period 947.3149660064277
2.59
1.7175
0.004702
d
yr
n .3800214426228724 0.00068897 deg/d
Q 3.057023681807943 0.0036949 au
  Orbit Determination Parameters
   # obs. used (total)      91  
   data-arc span      4 days  
   first obs. used      2015-11-07  
   last obs. used      2015-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48181  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:53  

Additional Information
 Earth MOID = .0130105 au 
 Jupiter MOID = 2.30628 au 
 T_jup = 3.664 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457334.5 (2015-Nov-08.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6198617849577452 0.00051274  
q .7185178336645796 0.0001051 au
tp 2457383.106875210695
(2015-Dec-26.60687521)
0.015465 TDB
node 46.15057956409717 0.00024157 deg
peri 76.53699547815758 0.0050941 deg
i 16.34485085874185 0.011312 deg
  Orbit Determination Parameters
   # obs. used (total)      91  
   data-arc span      4 days  
   first obs. used      2015-11-07  
   last obs. used      2015-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48181  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:53  

Additional Information
 Jupiter MOID = 2.30628 au 
 T_jup = 3.664 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.629074204966006E-7 -5.388545454002853E-8 -7.929583951858824E-6 1.238490565391339E-7 -2.610135714338594E-6 5.800197994732995E-6
q -5.388545454002853E-8 1.104599324882287E-8 1.625168095097714E-6 -2.538616035368598E-8 5.347268961459339E-7 -1.188773394736709E-6
tp -7.929583951858824E-6 1.625168095097714E-6 .0002391689197167813 -3.735323479203019E-6 7.873635155758822E-5 -.0001749420310400609
node 1.238490565391339E-7 -2.538616035368598E-8 -3.735323479203019E-6 5.835551138532686E-8 -1.229262574840056E-6 2.732263417829871E-6
peri -2.610135714338594E-6 5.347268961459339E-7 7.873635155758822E-5 -1.229262574840056E-6 2.595027193994992E-5 -5.758914074278717E-5
i 5.800197994732995E-6 -1.188773394736709E-6 -.0001749420310400609 2.732263417829871E-6 -5.758914074278717E-5 .0001279653833797019

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 26.1   n/a MPO361299  

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