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JPL Small-Body Database Browser
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(2013 SW24)
Classification: Apollo [NEO, PHA]          SPK-ID: 3648716
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 31 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6515379410591567 9.3046e-06  
a 2.674623109856901 6.8575e-05 au
q .9320046757514968 1.0043e-06 au
i 6.14126680905098 5.4251e-05 deg
node 347.1643262766896 0.00012599 deg
peri 323.839220264394 0.00013166 deg
M 198.9493150772429 0.021374 deg
tp 2459715.247082667507
(2022-May-15.74708267)
0.12235 TDB
period 1597.689260891456
4.37
0.061445
0.0001682
d
yr
n .2253254176592088 8.6657e-06 deg/d
Q 4.417241543962304 0.00011325 au
  Orbit Determination Parameters
   # obs. used (total)      255  
   data-arc span      261 days  
   first obs. used      2013-04-16  
   last obs. used      2014-01-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .36801  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Feb-25 06:45:04  

Additional Information
 Earth MOID = .000840636 au 
 Jupiter MOID = .935228 au 
 T_jup = 3.027 
[ 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 21.0   n/a MPO473287  
rotation period rot_per 7.09 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Published Reference List:
[Warner, B.D. (2014) Minor Planet Bull. 41, 113-124.]

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