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JPL Small-Body Database Browser
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(2015 OV)
Classification: Apollo [NEO]          SPK-ID: 3724242
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 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1654396872535454 1.0376e-06  
a 1.121887300082748 9.3978e-07 au
q .9362826160233337 3.8317e-07 au
i 7.648815134697171 3.7732e-05 deg
node 135.9718345799533 3.2329e-05 deg
peri 270.479995411765 4.8042e-05 deg
M 309.3219850437026 0.0016845 deg
tp 2459061.599740976676
(2020-Jul-31.09974098)
0.0021076 TDB
period 434.0325241738819
1.19
0.00054537
1.493e-06
d
yr
n .8294309295949835 1.0422e-06 deg/d
Q 1.307491984142162 1.0953e-06 au
  Orbit Determination Parameters
   # obs. used (total)      50  
   data-arc span      261 days  
   first obs. used      2015-07-19  
   last obs. used      2016-04-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .67984  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-21 11:40:01  

Additional Information
 Earth MOID = .0512122 au 
 Jupiter MOID = 3.95565 au 
 T_jup = 5.546 
[ 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 23.6   n/a MPO373589  
rotation period rot_per 1.17 h n/a LCDB (Rev. 2019-August); 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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