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(2015 FL290)
Classification: Apollo [NEO]          SPK-ID: 3715300
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 33 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5476270835238289 1.559e-05  
a 2.03977240509045 6.5455e-05 au
q .9227377918383807 2.1924e-06 au
i 5.705672654086983 0.00012123 deg
node 37.42945100947021 8.0926e-05 deg
peri 213.9941529125751 0.00015257 deg
M 259.4875763897219 0.029897 deg
tp 2459297.590140675406
(2021-Mar-24.09014068)
0.10267 TDB
period 1064.071950526615
2.91
0.051218
0.0001402
d
yr
n .3383229863561707 1.6285e-05 deg/d
Q 3.156807018342519 0.0001013 au
  Orbit Determination Parameters
   # obs. used (total)      163  
   data-arc span      150 days  
   first obs. used      2015-03-24  
   last obs. used      2015-08-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .40827  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:38  

Additional Information
 Earth MOID = .00946472 au 
 Jupiter MOID = 1.91963 au 
 T_jup = 3.594 
[ 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 22.2   n/a MPO336943  

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