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(2006 MV1)
Classification: Apollo [NEO]          SPK-ID: 3336903
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2418160033260484 0.00012842  
a 1.316978330695507 0.00026239 au
q .9985118942997088 2.9818e-05 au
i 4.27143745004016 0.015011 deg
node 264.5409028563479 0.006405 deg
peri 31.74357110997139 0.042041 deg
M 330.7913849151594 0.72293 deg
tp 2459441.289357802005
(2021-Aug-14.78935780)
1.1219 TDB
period 552.0346911993933
1.51
0.16498
0.0004517
d
yr
n .6521329288524171 0.0001949 deg/d
Q 1.635444767091306 0.00032584 au
  Orbit Determination Parameters
   # obs. used (total)      17  
   data-arc span      3 days  
   first obs. used      2006-06-19  
   last obs. used      2006-06-22  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .36416  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 23:44:06  

Additional Information
 Earth MOID = .00737522 au 
 Jupiter MOID = 3.54303 au 
 T_jup = 4.925 
[ 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 26.8   n/a MPO102376  
rotation period rot_per 0.0951 h n/a LCDB (Rev. 2020-October); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Hergenrother, C.W.; Whitely, R.J. (2011) Icarus 214, 194-209.]

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