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JPL Small-Body Database Browser
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(2014 SC324)
Classification: Apollo [NEO]          SPK-ID: 3692282
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 55 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5254399271407821 9.0663e-08  
a 1.927515708534675 4.6719e-07 au
q .9147219950795022 5.1179e-08 au
i 1.655763111335704 3.8865e-06 deg
node 210.1401344439057 1.1567e-05 deg
peri 221.5098373826053 1.7213e-05 deg
M 234.5086183540251 0.00020889 deg
tp 2458941.227130737564
(2020-Apr-01.72713074)
0.00069105 TDB
period 977.4517218366864
2.68
0.00035537
9.73e-07
d
yr
n .3683046353670951 1.339e-07 deg/d
Q 2.940309421989848 7.1267e-07 au
  Orbit Determination Parameters
   # obs. used (total)      273  
   # delay obs. used      6  
   # Doppler obs. used      4  
   data-arc span      29 days  
   first obs. used      2014-09-30  
   last obs. used      2014-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .35333  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:38:19  

Additional Information
 Earth MOID = .000786963 au 
 Jupiter MOID = 2.378 au 
 T_jup = 3.735 
[ 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 24.3   n/a MPO315324  
rotation period rot_per 0.36156 h n/a LCDB (Rev. 2019-January); Warner et al., 2009 Published Reference List:
[Warner, B.D. (2015) Minor Planet Bull. 42, 115-127.]

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