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(2020 CC)
Classification: Apollo [NEO]          SPK-ID: 3989356
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5840135164024566 0.00062119  
a 2.22433313262491 0.0032092 au
q .9252925181901447 4.6769e-05 au
i 3.287429415588263 0.0026699 deg
node 134.025611962945 7.1735e-05 deg
peri 35.84321208291475 0.0020436 deg
M 26.81510806163143 0.056662 deg
tp 2458910.244178395777
(2020-Mar-01.74417840)		 0.0046093 TDB
period 1211.708552612983
3.32		 2.6223
0.007179		 d
yr
n .2971011463306749 0.00064297 deg/d
Q 3.523373747059676 0.0050834 au
   Orbit Determination Parameters
   # obs. used (total)      49  
   data-arc span      4 days  
   first obs. used      2020-02-01  
   last obs. used      2020-02-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .39159  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-05 05:05:02  

Additional Information
 Earth MOID = .00217668 au 
 Jupiter MOID = 1.44959 au 
 T_jup = 3.399 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458881.5 (2020-Feb-02.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .589023908424674 0.00061286  
q .9267420376303336 4.9709e-05 au
tp 2458909.876642967997
(2020-Mar-01.37664297)		 0.0035106 TDB
node 134.0712785249382 5.5615e-05 deg
peri 35.30978987293405 0.003508 deg
i 3.335545636027184 0.0025657 deg
   Orbit Determination Parameters
   # obs. used (total)      49  
   data-arc span      4 days  
   first obs. used      2020-02-01  
   last obs. used      2020-02-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .39159  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-05 05:05:02  

Additional Information
 Jupiter MOID = 1.44959 au 
 T_jup = 3.399 
Orbit Covariance (6×6)
  e q tp node peri i
e 3.755919008974437E-7 -3.046395671598402E-8 -2.15120546084409E-6 -3.379390618941185E-8 2.14927441699095E-6 1.57239745661771E-6
q -3.046395671598402E-8 2.471024301995695E-9 1.744626463488515E-7 2.740114895413496E-9 -1.743550773633096E-7 -1.275348993900964E-7
tp -2.15120546084409E-6 1.744626463488515E-7 1.232444728589873E-5 1.937085411816746E-7 -1.230501277194058E-5 -9.006078548746441E-6
node -3.379390618941185E-8 2.740114895413496E-9 1.937085411816746E-7 3.093023753761888E-9 -1.932037848475021E-7 -1.414990130797417E-7
peri 2.14927441699095E-6 -1.743550773633096E-7 -1.230501277194058E-5 -1.932037848475021E-7 1.230625771434348E-5 8.997612593924769E-6
i 1.57239745661771E-6 -1.275348993900964E-7 -9.006078548746441E-6 -1.414990130797417E-7 8.997612593924769E-6 6.582938033653061E-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 28.057   .49501 6 autocmod 2.8

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