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(2016 JT28)
Classification: Apollo [NEO]          SPK-ID: 3753290
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2457521.5 (2016-May-13.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .497361285428798 0.0015838  
a 1.037525235534767 0.0010886 au
q .5215003507243787 0.0010961 au
i 10.34131986696223 0.045979 deg
node 231.7349350314989 0.0066344 deg
peri 124.5407776732231 0.0050621 deg
M 291.5586356256271 0.2116 deg
tp 2457594.885893764229
(2016-Jul-25.38589376)
0.11139 TDB
period 386.0081106889021
1.06
0.60749
0.001663
d
yr
n .9326228906369717 0.0014677 deg/d
Q 1.553550120345155 0.00163 au
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      14 days  
   first obs. used      2016-05-10  
   last obs. used      2016-05-24  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .49301  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 17:06:41  

Additional Information
 Earth MOID = .0218733 au 
 Jupiter MOID = 3.91771 au 
 T_jup = 5.777 
[ 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 23.7   n/a MPO382824  

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