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(2019 CS5)
Classification: Apollo [NEO]          SPK-ID: 3838783
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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3744156453058629 9.8114e-05  
a 1.54222350579349 0.00022878 au
q .9647908966659504 8.2364e-06 au
i 3.571021165981776 0.0006112 deg
node 147.9831977581752 0.00018688 deg
peri 20.88784684049022 0.0018557 deg
M 335.3536226876544 0.075091 deg
tp 2459248.392774393616
(2021-Feb-02.89277439)
0.15657 TDB
period 699.5510359676772
1.92
0.15566
0.0004262
d
yr
n .5146157771062665 0.00011451 deg/d
Q 2.11965611492103 0.00031444 au
  Orbit Determination Parameters
   # obs. used (total)      99  
   data-arc span      1 day  
   first obs. used      2019-02-13  
   last obs. used      2019-02-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .57953  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Mar-04 07:17:32  

Additional Information
 Earth MOID = .00280793 au 
 Jupiter MOID = 2.85028 au 
 T_jup = 4.382 
[ 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 25.9   .33106 MPO467467 autocmod 2.6q

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