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(2014 TT35)
Classification: Apollo [NEO]          SPK-ID: 3693239
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 2456945.5 (2014-Oct-15.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4693906393213668 0.00072291  
a 1.570438558831579 0.0018018 au
q .8332893996866984 0.0001794 au
i 3.234470123319829 0.0044932 deg
node 200.3388808755237 0.0019585 deg
peri 247.0898147893626 0.0029861 deg
M 334.8682478500951 0.051691 deg
tp 2456995.682248766425
(2014-Dec-04.18224877)
0.016869 TDB
period 718.836054412599
1.97
1.2371
0.003387
d
yr
n .5008096043459813 0.0008619 deg/d
Q 2.30758771797646 0.0026476 au
  Orbit Determination Parameters
   # obs. used (total)      29  
   data-arc span      3 days  
   first obs. used      2014-10-14  
   last obs. used      2014-10-17  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .61785  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 11:29:11  

Additional Information
 Earth MOID = .00612785 au 
 Jupiter MOID = 2.9487 au 
 T_jup = 4.282 
[ 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 26.0   n/a MPO313339  

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