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JPL Small-Body Database Browser
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(2015 VV105)
Classification: Apollo [NEO]          SPK-ID: 3734613
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2832561135701964 0.00025979  
a 1.409829879587489 0.00053594 au
q 1.010486947100399 1.787e-05 au
i 7.758617350151848 0.0057853 deg
node 230.5351584817006 0.00038205 deg
peri 188.3722409104431 0.0032338 deg
M 253.3849143572339 0.55257 deg
tp 2459181.577567676400
(2020-Nov-28.07756768)
1.0417 TDB
period 611.4324625872212
1.67
0.34865
0.0009546
d
yr
n .5887812996985677 0.00033573 deg/d
Q 1.809172812074579 0.00068774 au
  Orbit Determination Parameters
   # obs. used (total)      36  
   data-arc span      8 days  
   first obs. used      2015-11-12  
   last obs. used      2015-11-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .62823  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:39  

Additional Information
 Earth MOID = .023551 au 
 Jupiter MOID = 3.5282 au 
 T_jup = 4.680 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457339.5 (2015-Nov-13.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2842912023551771 0.0002579  
q 1.010375370749685 1.8529e-05 au
tp 2457347.235023164654
(2015-Nov-20.73502316)
0.0027601 TDB
node 230.6137460189846 0.00014606 deg
peri 188.0812946299005 0.0024552 deg
i 7.781157070547854 0.0057371 deg
  Orbit Determination Parameters
   # obs. used (total)      36  
   data-arc span      8 days  
   first obs. used      2015-11-12  
   last obs. used      2015-11-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .62823  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:39  

Additional Information
 Jupiter MOID = 3.5282 au 
 T_jup = 4.680 
Orbit Covariance (6×6)
  e q tp node peri i
e 6.651329086485661E-8 4.778447315773756E-9 -7.068648456218723E-7 3.764639402060142E-8 -6.264829290599392E-7 1.479572634242673E-6
q 4.778447315773756E-9 3.433203729367137E-10 -5.082536342996556E-8 2.704426071716989E-9 -4.50547627505475E-8 1.062970093017037E-7
tp -7.068648456218723E-7 -5.082536342996556E-8 7.618250608514766E-6 -3.994303093374381E-7 6.774031650214768E-6 -1.572268427811681E-5
node 3.764639402060142E-8 2.704426071716989E-9 -3.994303093374381E-7 2.133492638891848E-8 -3.538966109480531E-7 8.374508117618484E-7
peri -6.264829290599392E-7 -4.50547627505475E-8 6.774031650214768E-6 -3.538966109480531E-7 6.027929646974343E-6 -1.3934496727511E-5
i 1.479572634242673E-6 1.062970093017037E-7 -1.572268427811681E-5 8.374508117618484E-7 -1.3934496727511E-5 3.29141568413409E-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 28.3   n/a MPO361302  

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