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JPL Small-Body Database Browser
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(2017 FV)
Classification: Apollo [NEO]          SPK-ID: 3771588
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 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5167236247790566 1.4797e-06  
a 1.5306745897617 4.09e-06 au
q .7397388673828389 3.395e-07 au
i 3.017488387005691 9.9555e-06 deg
node 13.40714023430823 1.759e-05 deg
peri 253.4856220941594 4.1451e-05 deg
M 7.189961407179828 0.0014451 deg
tp 2458586.685130257906
(2019-Apr-13.18513026)
0.0027213 TDB
period 691.7079001547231
1.89
0.0027724
7.59e-06
d
yr
n .5204509011961179 2.086e-06 deg/d
Q 2.321610312140561 6.2034e-06 au
  Orbit Determination Parameters
   # obs. used (total)      108  
   # delay obs. used      2  
   # Doppler obs. used      1  
   data-arc span      27 days  
   first obs. used      2017-03-05  
   last obs. used      2017-04-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .32814  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Nov-23 06:25:08  

Additional Information
 Earth MOID = .00248011 au 
 Jupiter MOID = 2.79505 au 
 T_jup = 4.327 
[ 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 24.6   n/a MPO413698  

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