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(2016 YC8)
Classification: Apollo [NEO]          SPK-ID: 3766164
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 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2236975948456223 6.5229e-07  
a 1.086187121596653 6.5766e-07 au
q .8432096749431923 2.8158e-07 au
i 6.063991293708477 1.7831e-05 deg
node 295.6558731514741 2.3708e-05 deg
peri 258.1667665273376 6.2905e-05 deg
M 110.8048902606378 0.0010153 deg
tp 2459073.234165975285
(2020-Aug-11.73416598)
0.0010505 TDB
period 413.4808503589388
1.13
0.00037553
1.028e-06
d
yr
n .8706570079061399 7.9075e-07 deg/d
Q 1.329164568250114 8.0478e-07 au
  Orbit Determination Parameters
   # obs. used (total)      88  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      22 days  
   first obs. used      2016-12-27  
   last obs. used      2017-01-18  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      3  
   norm. resid. RMS      .4491  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 18:20:39  

Additional Information
 Earth MOID = .00125361 au 
 Jupiter MOID = 3.63888 au 
 T_jup = 5.676 
[ 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 24.6   n/a E2017B01  

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