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(2007 CS5)
Classification: Aten [NEO]          SPK-ID: 3367721
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1727708206108013 0.00052923  
a .980459968558993 3.0945e-05 au
q .8110650952150154 0.00054448 au
i .7513296706328119 0.0017776 deg
node 125.2640471927109 0.022412 deg
peri 261.420329629568 0.013228 deg
M 188.3681653781352 0.11104 deg
tp 2459369.559106984318
(2021-Jun-04.05910698)		 0.10165 TDB
period 354.6036703997407
0.97		 0.016788
4.596e-05		 d
yr
n 1.015217918060961 4.8063e-05 deg/d
Q 1.149854841902971 3.6292e-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 = .000651749 au 
 Jupiter MOID = 4.13317 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 = 4.13317 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  

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