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(2015 VM64)
Classification: Apollo [NEO]          SPK-ID: 3733853
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6202772846134578 0.00051717  
a 1.886717604451484 0.0022752 au
q .7164295319299098 0.00011181 au
i 16.3097170978266 0.01115 deg
node 46.03832624100892 0.0011396 deg
peri 76.71960033620101 0.0037971 deg
M 254.7839226452676 1.1061 deg
tp 2459277.154911812656
(2021-Mar-03.65491181)		 3.4087 TDB
period 946.583172044822
2.59		 1.7122
0.004688		 d
yr
n .380315233390768 0.00068794 deg/d
Q 3.057005676973059 0.0036865 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 = .0124379 au 
 Jupiter MOID = 2.30516 au 
 T_jup = 3.665 
[ 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 = 2.30516 au 
 T_jup = 3.665 
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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