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(2019 QP1)
Classification: Apollo [NEO]          SPK-ID: 3843602
[ 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.


Orbital Elements at Epoch 2458719.5 (2019-Aug-24.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4027414565147551 0.0012728  
a 1.559106706881262 0.0030847 au
q .9311898008899789 0.00014214 au
i 6.838036430465129 0.018054 deg
node 325.9727813780844 0.0014001 deg
peri 57.72397804206102 0.0061489 deg
M 337.1164389697245 0.081917 deg
tp 2458764.699464960465
(2019-Oct-08.19946496)		 0.027663 TDB
period 711.0697222446893
1.95		 2.1103
0.005778		 d
yr
n .506279467031109 0.0015025 deg/d
Q 2.187023612872544 0.004327 au
   Orbit Determination Parameters
   # obs. used (total)      13  
   data-arc span      4 days  
   first obs. used      2019-08-23  
   last obs. used      2019-08-27  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .47024  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 21:36:37  

Additional Information
 Earth MOID = .026887 au 
 Jupiter MOID = 3.2956 au 
 T_jup = 4.332 
[ 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 26.5   .28336 MPO492667 autocmod 2.8

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