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(2014 XB6)
Classification: Apollo [NEO]          SPK-ID: 3701712
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3934948274545352 0.00030502  
a 1.598765738586775 0.0008055 au
q .9696596901413495 1.2738e-05 au
i 6.092320316304315 0.0066198 deg
node 76.32842575403016 0.01561 deg
peri 32.49935606151839 0.0094678 deg
M 242.6268962648654 0.79866 deg
tp 2459241.236401368506
(2021-Jan-26.73640137)
1.82 TDB
period 738.3727765113169
2.02
0.55802
0.001528
d
yr
n .4875586038002883 0.00036847 deg/d
Q 2.2278717870322 0.0011225 au
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      1 day  
   first obs. used      2014-12-10  
   last obs. used      2014-12-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .54681  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:36:58  

Additional Information
 Earth MOID = .018344 au 
 Jupiter MOID = 2.92231 au 
 T_jup = 4.268 
[ 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 26.5   n/a MPO319047  

[ 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
1931-Nov-11 18:41 9_07:44 Earth 0.372150100899855 0.131499804077391 0.613209559999345 17.7469514734869 17.7465480367986 2426657.278183068 13423.8360559315 12026215.5062365 89.3415023205859 2.27186717213588 25858.4416020321 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 22:31:20 2018-Dec-11 16:28
2008-Nov-05 23:28 2_19:42 Earth 0.475663647100211 0.382240571612178 0.569095089700009 20.8071754129499 20.8069061962003 2454776.478104228 4062.21492709742 4659901.69447218 43.927345953905 1.24154805236444 31174.8831793596 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 22:31:20 2018-Dec-11 16:28
2010-Nov-15 18:25 2_15:07 Earth 0.313729596352694 0.249475195732401 0.377990248329154 16.0152950593609 16.0147647502212 2455516.267096775 3786.72800436506 3205023.96293116 119.039568503013 1.3098819681678 8414.0512001385 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 22:31:20 2018-Dec-11 16:28
2012-Nov-25 23:59 2_07:13 Earth 0.153563006251498 0.120821199028673 0.186304796456005 11.2963921490056 11.2948560630458 2456257.499113496 3313.19686380537 1632699.11793775 194.110298352455 -0.788700161425823 1297.68434234981 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 22:31:20 2018-Dec-11 16:28
2014-Dec-14 07:17 00:01 Earth 0.0194027215424436 0.019355006189209 0.0194504356345213 7.18754835546467 7.16841693124132 2457005.803731118 1.09688417457258 2366.48648239443 45.6582735031251 0.138085941304396 708.913190135394 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 22:31:20 2018-Dec-11 16:28
2019-Feb-14 10:29 7_11:54 Earth 0.134877570206812 0.0994833311445187 0.185560196050169 8.8453331471909 8.8430995067382 2458528.936881008 10793.5753230034 3143215.40156716 262.640884715786 -43.8391260438836 31862.3925771541 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 22:31:20 2018-Dec-11 16:28
2021-Feb-28 00:59 5_01:02 Earth 0.250260311870168 0.169330719020718 0.338627762251662 13.121057557133 13.1202461011548 2459273.540958049 7262.19009242051 4741380.87829476 404.522321647714 -25.3871116709548 34885.7938222732 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 22:31:20 2018-Dec-11 16:28
2023-Mar-09 15:40 4_08:14 Earth 0.383194225216691 0.270004848281001 0.500304044852826 17.3623773172061 17.3619768294714 2460013.153120108 6254.30113807031 6059399.0833718 545.655716379581 -17.7403594514364 27908.2955095043 T 6 CATAB v2.0e-lin.ifort 2017-Nov-29 22:31:20 2018-Dec-11 16:28
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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