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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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5698028553276323 1.1397e-06  
a 1.72600509066482 2.5206e-07 au
q .7425224616939766 2.0755e-06 au
i 1.221196126861813 2.1446e-05 deg
node 253.6070929003529 0.00046484 deg
peri 73.59593570331377 0.00055547 deg
M 301.2681339284139 0.00049002 deg
tp 2459335.624106216435
(2021-May-01.12410622)
0.001157 TDB
period 828.2501730598048
2.27
0.00018143
4.967e-07
d
yr
n .4346512825588094 9.5213e-08 deg/d
Q 2.709487719635663 3.9569e-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 = .000583766 au 
 Jupiter MOID = 2.66489 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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