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JPL Small-Body Database Browser
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(2015 EG)
Classification: Aten [NEO]          SPK-ID: 3712904
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3563152448381607 3.103e-07  
a .862611753633058 1.258e-08 au
q .5552500354370198 2.6523e-07 au
i 2.493144364914744 5.8259e-06 deg
node 167.6536182510624 7.7182e-06 deg
peri 223.5327270884517 1.1171e-05 deg
M 161.747044518061 4.7516e-05 deg
tp 2458469.021319456333
(2018-Dec-16.52131946)
3.7524e-05 TDB
period 292.6317765913491
0.80
6.4013e-06
1.753e-08
d
yr
n 1.230214996448347 2.6911e-08 deg/d
Q 1.169973471829096 1.7062e-08 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] -1.995793564230984E-13 3.127E-14
ALN [SET] 1. n/a
NK [SET] 0. n/a
NM [SET] 2. n/a
R0 [SET] 1. n/a
  Orbit Determination Parameters
   # obs. used (total)      146  
   # delay obs. used      2  
   # Doppler obs. used      1  
   data-arc span      2899 days (7.94 yr)  
   first obs. used      2011-04-02  
   last obs. used      2019-03-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .34421  
   source      ORB  
   producer      Giorgini  
   solution date      2019-Jul-13 12:44:43  

Additional Information
 Earth MOID = .00299215 au 
 Jupiter MOID = 4.25794 au 
 T_jup = 6.792 
[ 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 25.7   n/a E2015L43  
rotation period rot_per 1.29 h n/a LCDB (Rev. 2019-January); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Thirouin, A.; Moskovitz, N.; Binzel, R.P.; Christensen, E.; et al. (2016) Astron. J. 152, A163.]

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