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(2004 FY15)
Classification: Apollo [NEO]          SPK-ID: 3177224
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4790789576633023 0.00016707  
a 1.854591985290145 0.00051349 au
q .9660959900866278 4.2361e-05 au
i 3.493576161100876 0.0025151 deg
node 6.034366077120925 0.029467 deg
peri 207.3622620730341 0.032627 deg
M 138.0493688006054 1.1037 deg
tp 2458646.744729257865
(2019-Jun-12.24472926)
2.6814 TDB
period 922.5098135081804
2.53
0.38313
0.001049
d
yr
n .3902397510883581 0.00016207 deg/d
Q 2.743087980493662 0.00075949 au
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      1 day  
   first obs. used      2004-03-26  
   last obs. used      2004-03-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .65541  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:13:01  

Additional Information
 Earth MOID = .0015405 au 
 Jupiter MOID = 2.23162 au 
 T_jup = 3.852 
[ 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 26.1   n/a MPO62539  

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