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(2019 GM1)
Classification: Apollo [NEO]          SPK-ID: 3840791
[ 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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07119724677873042 5.5674e-06  
a 1.002640385073979 3.3186e-08 au
q .9312551501475457 5.5561e-06 au
i 6.753064415138286 0.00016415 deg
node 187.992406271033 0.00016329 deg
peri 110.4261185432004 0.00026905 deg
M 319.2911968365834 0.00094979 deg
tp 2459041.966945946727
(2020-Jul-11.46694595)		 0.00096556 TDB
period 366.704481114222
1.00		 1.8206e-05
4.985e-08		 d
yr
n .9817169370446454 4.874e-08 deg/d
Q 1.074025620000413 3.5548e-08 au
   Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      364 days  
   first obs. used      2019-04-03  
   last obs. used      2020-04-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .25691  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-02 06:04:34  

Additional Information
 Earth MOID = .0196834 au 
 Jupiter MOID = 3.96382 au 
 T_jup = 6.059 
[ 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 27.0   .6466 MPO477913 autocmod 2.6q

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