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(2017 BG30)
Classification: Apollo [NEO]          SPK-ID: 3767154
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 .1069611974649504 7.0685e-05  
a 1.055363651735642 5.6354e-05 au
q .942480691785015 2.4306e-05 au
i 1.630946368071903 0.0016608 deg
node 304.5189731480737 0.0066388 deg
peri 250.3804987090391 0.0068612 deg
M 332.4362718478947 0.082143 deg
tp 2459030.820550541062
(2020-Jun-30.32055054)
0.092787 TDB
period 396.005871721984
1.08
0.031719
8.684e-05
d
yr
n .9090774296718968 7.2814e-05 deg/d
Q 1.168246611686269 6.2382e-05 au
  Orbit Determination Parameters
   # obs. used (total)      39  
   data-arc span      5 days  
   first obs. used      2017-01-28  
   last obs. used      2017-02-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .61416  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:20:42  

Additional Information
 Earth MOID = .00609771 au 
 Jupiter MOID = 3.78838 au 
 T_jup = 5.826 
[ 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 29.4   n/a MPO399708  

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