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(2015 SV6)
Classification: Apollo [NEO]          SPK-ID: 3728645
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 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 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457289.5 (2015-Sep-24.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6424899686801774 0.00038572  
q .6645830569030711 0.00011842 au
tp 2457338.836597398707
(2015-Nov-12.33659740)
0.01237 TDB
node 358.4869045355662 6.4837e-05 deg
peri 85.75461118352385 0.00079716 deg
i 5.162500641551424 0.0029764 deg
  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
 Jupiter MOID = 2.25238 au 
 T_jup = 3.717 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.487804734340781E-7 -4.567339451444158E-8 -4.771228200337427E-6 1.748901792587727E-8 -2.874176056238017E-7 1.146317606707262E-6
q -4.567339451444158E-8 1.402411773806398E-8 1.464604543509973E-6 -5.301821190654131E-9 8.773895315520394E-8 -3.516490505089104E-7
tp -4.771228200337427E-6 1.464604543509973E-6 .0001530108820005279 -5.628024306311582E-7 9.231922944896807E-6 -3.676843030571843E-5
node 1.748901792587727E-8 -5.301821190654131E-9 -5.628024306311582E-7 4.203776324503976E-9 -4.521002446525529E-8 1.420599187719004E-7
peri -2.874176056238017E-7 8.773895315520394E-8 9.231922944896807E-6 -4.521002446525529E-8 6.35466506508269E-7 -2.256754191612869E-6
i 1.146317606707262E-6 -3.516490505089104E-7 -3.676843030571843E-5 1.420599187719004E-7 -2.256754191612869E-6 8.858850552524497E-6

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.]

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