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JPL Small-Body Database Browser
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(2007 CS5)
Classification: Aten [NEO]          SPK-ID: 3367721
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 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1727278376689307 0.00052971  
a .9803891460546401 3.0516e-05 au
q .8110486487825326 0.00054455 au
i .7512335923611535 0.0017784 deg
node 125.2628340919921 0.02247 deg
peri 261.4295172949098 0.013159 deg
M 299.2120664753015 0.13919 deg
tp 2458660.370246705418
(2019-Jun-25.87024671)
0.13435 TDB
period 354.5652494535459
0.97
0.016555
4.533e-05
d
yr
n 1.015327927806885 4.7405e-05 deg/d
Q 1.149729643326748 3.5787e-05 au
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      16 days  
   first obs. used      2007-02-07  
   last obs. used      2007-02-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .6012  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:07:06  

Additional Information
 Earth MOID = .000678574 au 
 Jupiter MOID = 4.13561 au 
 T_jup = 6.162 
[ hide covariance matrix ]
Orbital Elements at Epoch 2454145.5 (2007-Feb-14.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1732167192196253 0.00050544  
q .8103260177443921 0.00042383 au
tp 2454051.829425427434
(2006-Nov-12.32942543)
0.050775 TDB
node 125.7452410299967 0.0081175 deg
peri 261.6057242401723 0.0043506 deg
i .746755511946066 0.002333 deg
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      16 days  
   first obs. used      2007-02-07  
   last obs. used      2007-02-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .6012  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:07:06  

Additional Information
 Jupiter MOID = 4.13561 au 
 T_jup = 6.162 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.55471046877437E-7 -2.142013395716915E-7 2.565666527272743E-5 -4.091885815864058E-6 1.855036103016189E-6 1.179143655863152E-6
q -2.142013395716915E-7 1.79629033847083E-7 -2.150531584877726E-5 3.428671183037701E-6 -1.54268686250288E-6 -9.886309419339915E-7
tp 2.565666527272743E-5 -2.150531584877726E-5 .002578131619156424 -.0004114226727443317 .000189072491753234 .000118426492381443
node -4.091885815864058E-6 3.428671183037701E-6 -.0004114226727443317 6.589327271899715E-5 -3.081803632892697E-5 -1.887900619127068E-5
peri 1.855036103016189E-6 -1.54268686250288E-6 .000189072491753234 -3.081803632892697E-5 1.892796399542605E-5 8.564801390758449E-6
i 1.179143655863152E-6 -9.886309419339915E-7 .000118426492381443 -1.887900619127068E-5 8.564801390758449E-6 5.443001298585963E-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 24.6   n/a MPO116391  

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