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JPL Small-Body Database Browser
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172722 (2004 BV102)
Classification: Apollo [NEO]          SPK-ID: 2172722
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 105 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6992870797348716 9.3615e-08  
a 1.543712163041411 1.6299e-08 au
q .4642141925969809 1.4813e-07 au
i 7.217552366046497 8.871e-06 deg
node 341.3096892840285 4.0569e-05 deg
peri 17.1902206772427 4.2865e-05 deg
M 6.417333090972472 4.6543e-05 deg
tp 2458588.011795640100
(2019-Apr-14.51179564)
9.038e-05 TDB
period 700.5641605059361
1.92
1.1095e-05
3.038e-08
d
yr
n .513871562798779 8.1385e-09 deg/d
Q 2.623210133485842 2.7697e-08 au
  Orbit Determination Parameters
   # obs. used (total)      457  
   data-arc span      5161 days (14.13 yr)  
   first obs. used      2004-01-31  
   last obs. used      2018-03-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50858  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Mar-20 07:00:58  

Additional Information
 Earth MOID = .103034 au 
 Jupiter MOID = 2.83477 au 
 T_jup = 4.143 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 17.5   n/a MPO439991  

172722 (2004 BV102)          Discovered 2004-Jan-31 by LINEAR at Socorro
Reference: 20071224/Numbers.arcLast Updated: 2007-12-22

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