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(2016 CY135)
Classification: Apollo [NEO]          SPK-ID: 3742333
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 33 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3534619958837394 8.0174e-06  
a 1.475081133061978 1.6806e-05 au
q .9536960116794433 9.6048e-07 au
i 1.10374712867583 2.1032e-05 deg
node 173.4902546844873 6.1526e-05 deg
peri 26.54235538971641 0.00015012 deg
M 113.2784770475396 0.01425 deg
tp 2458794.594859047999
(2019-Nov-07.09485905)
0.022383 TDB
period 654.368355531581
1.79
0.011183
3.062e-05
d
yr
n .5501488526405763 9.4023e-06 deg/d
Q 1.996466254444513 2.2747e-05 au
  Orbit Determination Parameters
   # obs. used (total)      87  
   data-arc span      164 days  
   first obs. used      2016-01-31  
   last obs. used      2016-07-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .37376  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:28:31  

Additional Information
 Earth MOID = .00178157 au 
 Jupiter MOID = 2.96002 au 
 T_jup = 4.523 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457472.5 (2016-Mar-25.0) TDB
Reference: JPL 33 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3541397695880647 8.0215e-06  
q .9535905769534928 1.0076e-06 au
tp 2457485.835778868252
(2016-Apr-07.33577887)
2.6881e-05 TDB
node 173.5771261281765 6.5496e-05 deg
peri 26.53614398779843 0.00014563 deg
i 1.106041664141068 2.0927e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      87  
   data-arc span      164 days  
   first obs. used      2016-01-31  
   last obs. used      2016-07-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .37376  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:28:31  

Additional Information
 Jupiter MOID = 2.96002 au 
 T_jup = 4.523 
Orbit Covariance (6×6)
  e q tp node peri i
e 6.434424821986827E-11 -8.08099223477774E-12 2.105669324637727E-10 -4.314790837430119E-10 1.12827056565335E-9 1.671087377908232E-10
q -8.08099223477774E-12 1.015181184677022E-12 -2.651114549845588E-11 5.419633343307345E-11 -1.417804792070041E-10 -2.098870357411681E-11
tp 2.105669324637727E-10 -2.651114549845588E-11 7.225975774785742E-10 -1.404047342849563E-9 3.716730921467742E-9 5.471694924820767E-10
node -4.314790837430119E-10 5.419633343307345E-11 -1.404047342849563E-9 4.289736554633842E-9 -8.958460660347545E-9 -1.149898214579593E-9
peri 1.12827056565335E-9 -1.417804792070041E-10 3.716730921467742E-9 -8.958460660347545E-9 2.120748733639253E-8 2.959966936378167E-9
i 1.671087377908232E-10 -2.098870357411681E-11 5.471694924820767E-10 -1.149898214579593E-9 2.959966936378167E-9 4.379350153922481E-10

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 24.5   n/a MPO373615  

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