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159928 (2005 CV69)
Classification: Apollo [NEO]          SPK-ID: 2159928
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 102 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4193681521072808 2.293e-08  
a 1.654141514162554 2.4844e-09 au
q .960447244044264 3.8002e-08 au
i 27.75253706586831 1.0002e-05 deg
node 157.4811987764861 7.7668e-06 deg
peri 95.65030300875237 1.3516e-05 deg
M 106.7969119366606 8.5546e-06 deg
tp 2458969.977344807482
(2020-Apr-30.47734481)
1.8132e-05 TDB
period 777.0651263636271
2.13
1.7507e-06
4.793e-09
d
yr
n .4632816321132113 1.0437e-09 deg/d
Q 2.347835784280843 3.5263e-09 au
  Orbit Determination Parameters
   # obs. used (total)      679  
   data-arc span      11875 days (32.51 yr)  
   first obs. used      1988-03-20  
   last obs. used      2020-09-23  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .4363  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-18 06:26:37  

Additional Information
 Earth MOID = .21799 au 
 Jupiter MOID = 3.13246 au 
 T_jup = 4.052 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 17.99   n/a E2021B55  

159928 (2005 CV69)          Discovered 2005-Feb-03 by NEAT at Palomar
Reference: 20070630/Numbers.arcLast Updated: 2007-07-05

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