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JPL Small-Body Database Browser
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(2016 RO17)
Classification: Apollo [NEO]          SPK-ID: 3759005
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6318367492491426 0.00045932  
a 2.05541976015008 0.0022653 au
q .7567300205544012 0.00011009 au
i 6.67464365942197 0.0035875 deg
node 167.7230620062884 0.0043041 deg
peri 246.5024329000659 0.0045483 deg
M 305.8820869921353 0.50707 deg
tp 2458762.303442512974
(2019-Oct-05.80344251)
1.7835 TDB
period 1076.339349897056
2.95
1.7794
0.004872
d
yr
n .3344670061857641 0.00055293 deg/d
Q 3.354109499745759 0.0036966 au
  Orbit Determination Parameters
   # obs. used (total)      76  
   data-arc span      2 days  
   first obs. used      2016-09-05  
   last obs. used      2016-09-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .62246  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:24:07  

Additional Information
 Earth MOID = .00515081 au 
 Jupiter MOID = 2.07114 au 
 T_jup = 3.499 
[ 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 26.3   n/a E2016R87  

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