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(2016 CV193)
Classification: Apollo [NEO]          SPK-ID: 3743607
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2777276371942487 7.7257e-06  
a 1.376306237560107 1.4416e-05 au
q .9940679581468318 2.3368e-07 au
i 9.387882330395733 0.00023563 deg
node 133.2794518347218 5.6954e-05 deg
peri 87.16531320114305 5.8798e-05 deg
M 186.9690051422086 0.014339 deg
tp 2459283.960434261914
(2021-Mar-10.46043426)
0.027945 TDB
period 589.7542022350221
1.61
0.009266
2.537e-05
d
yr
n .6104237979749687 9.5907e-06 deg/d
Q 1.758544516973382 1.842e-05 au
  Orbit Determination Parameters
   # obs. used (total)      92  
   data-arc span      143 days  
   first obs. used      2016-02-10  
   last obs. used      2016-07-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .42562  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:28:24  

Additional Information
 Earth MOID = .131003 au 
 Jupiter MOID = 3.24113 au 
 T_jup = 4.756 
[ 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 22.6   n/a MPO409560  

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