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(2007 RU17)
Classification: Apollo [NEO, PHA]          SPK-ID: 3384406
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 65 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .827939052220925 1.3955e-07  
a 2.039821618268603 1.053e-07 au
q .3509736409395424 2.7532e-07 au
i 9.081004922556202 2.117e-05 deg
node 17.39855595870724 2.2415e-05 deg
peri 129.8869581263566 3.3496e-05 deg
M 89.62532038394899 1.2323e-05 deg
tp 2458735.579886451323
(2019-Sep-09.07988645)
1.6477e-05 TDB
period 1064.110459733472
2.91
8.2397e-05
2.256e-07
d
yr
n .3383107427495536 2.6196e-08 deg/d
Q 3.728669595597665 1.9248e-07 au
  Orbit Determination Parameters
   # obs. used (total)      389  
   # delay obs. used      1  
   # Doppler obs. used      0  
   data-arc span      2213 days (6.06 yr)  
   first obs. used      2007-09-13  
   last obs. used      2013-10-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .40958  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Dec-02 06:16:59  

Additional Information
 Earth MOID = .0391667 au 
 Jupiter MOID = 1.36751 au 
 T_jup = 3.244 
[ 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 18.1   n/a E2013R61  

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