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(2014 DX110)
Classification: Apollo [NEO]          SPK-ID: 3662876
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6243617121672551 0.00025773  
a 2.199980341717023 0.0014054 au
q .8263968488282797 3.909e-05 au
i 5.732504072947512 0.0020667 deg
node 163.78591393908 0.00018827 deg
peri 56.58242301225293 0.0018829 deg
M 76.19755757885767 0.75403 deg
tp 2459144.230249848760
(2020-Oct-21.73024985)
2.2547 TDB
period 1191.863793802825
3.26
1.142
0.003127
d
yr
n .3020479369134662 0.00028942 deg/d
Q 3.573563834605767 0.0022828 au
  Orbit Determination Parameters
   # obs. used (total)      63  
   data-arc span      5 days  
   first obs. used      2014-02-28  
   last obs. used      2014-03-05  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .41704  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:25:37  

Additional Information
 Earth MOID = .00190158 au 
 Jupiter MOID = 1.4278 au 
 T_jup = 3.376 
[ 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 E2014E24  
rotation period rot_per 0.12041 h n/a LCDB (Rev. 2020-October); 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:
[Warner, B.D. (2014) Minor Planet Bull. 41, 157-168.]

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2014-Mar-05 21:00 < 00:01 Earth 0.00232849143568535 0.00232592488876792 0.0023310579236683 14.8428300684481 14.7655347333073 2456722.374669519 0.0203404820855908 126.634698138708 0.703368199447138 -0.173178488484204 1968.91918983806 T 9 CATAB v2.0g-lin.ifort 2021-Apr-15 09:25:38 2021-Apr-15 09:25
2014-Mar-05 22:22 < 00:01 Moon 0.00249975903708217 0.00249858841750325 0.00250093177851348 15.8147955214754 15.8139664949413 2456722.431814775 0.0858758670963988 128.863121566035 0.71990003387547 63.0461993985916 458118.699441683 T 9 CATAB v2.0g-lin.ifort 2021-Apr-15 09:25:38 2021-Apr-15 09:25
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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