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(2017 BP30)
Classification: Apollo [NEO]          SPK-ID: 3767163
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2671625231531963 0.00025226  
a 1.305366722953185 0.00038045 au
q .9566216556087925 5.0574e-05 au
i 8.757219317282514 0.0076912 deg
node 309.2770975054123 0.0027149 deg
peri 232.3519724116124 0.012751 deg
M 52.78363978326415 0.42143 deg
tp 2458920.628090656727
(2020-Mar-12.12809066)
0.60279 TDB
period 544.7499922636086
1.49
0.23815
0.000652
d
yr
n .6608536119552495 0.00028891 deg/d
Q 1.654111790297577 0.00048209 au
  Orbit Determination Parameters
   # obs. used (total)      28  
   data-arc span      7 days  
   first obs. used      2017-01-28  
   last obs. used      2017-02-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .49911  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:20:40  

Additional Information
 Earth MOID = .036911 au 
 Jupiter MOID = 3.33016 au 
 T_jup = 4.940 
[ 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 MPO399711  

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