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JPL Small-Body Database Browser
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(2007 VK184)
Classification: Apollo [NEO]          SPK-ID: 3394541
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 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5695223788192517 1.1403e-06  
a 1.726269599692054 2.5167e-07 au
q .7431204307920781 2.0768e-06 au
i 1.22119994341257 2.1446e-05 deg
node 253.6197260455058 0.00046469 deg
peri 73.57221807145235 0.00055539 deg
M 40.54808467023186 0.00043306 deg
tp 2458507.189781897388
(2019-Jan-23.68978190)
0.00097618 TDB
period 828.4405734607097
2.27
0.00018116
4.96e-07
d
yr
n .4345513867049556 9.5028e-08 deg/d
Q 2.70941876859203 3.95e-07 au
  Orbit Determination Parameters
   # obs. used (total)      107  
   data-arc span      2327 days (6.37 yr)  
   first obs. used      2007-11-12  
   last obs. used      2014-03-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .57621  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:05:12  

Additional Information
 Earth MOID = .000516615 au 
 Jupiter MOID = 2.66122 au 
 T_jup = 3.961 
[ 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 22.0   n/a MPO131999  

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