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(2015 SV6)
Classification: Apollo [NEO]          SPK-ID: 3728645
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6419965765811244 0.00037143  
a 1.854992325395321 0.0016926 au
q .6640936029072656 8.3082e-05 au
i 5.073677644248015 0.0030465 deg
node 357.9659053987556 0.0024933 deg
peri 86.49085560470749 0.001666 deg
M 287.9652884568909 0.87369 deg
tp 2459185.150685070250
(2020-Dec-01.65068507)
2.4923 TDB
period 922.8085349589888
2.53
1.263
0.003458
d
yr
n .390113426959146 0.00053393 deg/d
Q 3.045891047883376 0.0027792 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      2 days  
   first obs. used      2015-09-23  
   last obs. used      2015-09-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .39464  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:31:46  

Additional Information
 Earth MOID = .00669434 au 
 Jupiter MOID = 2.25238 au 
 T_jup = 3.717 
[ 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 27.7   n/a MPO347506  
rotation period rot_per 0.00490 h n/a LCDB (Rev. 2019-August); 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:
[Thirouin, A.; Moskovitz, N.; Binzel, R.P.; Christensen, E.; et al. (2016) Astron. J. 152, A163.]

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