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245174 (2004 TO135)
Classification: Main-belt Asteroid          SPK-ID: 2245174
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

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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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1882807019885023 6.1252e-08  
a 2.354823967865559 1.4876e-08 au
q 1.911456058136481 1.3831e-07 au
i 6.17905116349272 4.7418e-06 deg
node 234.500504067141 4.3591e-05 deg
peri 141.9626052034297 4.5948e-05 deg
M 123.4405809500901 1.7099e-05 deg
tp 2458547.923963900154
(2019-Mar-05.42396390)
6.022e-05 TDB
period 1319.885014651868
3.61
1.2507e-05
3.424e-08
d
yr
n .2727510321002874 2.5846e-09 deg/d
Q 2.798191877594637 1.7677e-08 au
  Orbit Determination Parameters
   # obs. used (total)      482  
   data-arc span      7206 days (19.73 yr)  
   first obs. used      2000-07-30  
   last obs. used      2020-04-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49942  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-21 13:03:25  

Additional Information
 Earth MOID = .917934 au 
 Jupiter MOID = 2.68109 au 
 T_jup = 3.523 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.4   n/a MPO454804  

245174 (2004 TO135)          Discovered 2004-Oct-08 by LONEOS at Anderson Mesa
Reference: 20100726/Numbers.arcLast Updated: 2010-07-28

Alternate Designations
 2004 TO135 = 2002 CE48 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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