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(2016 GE135)
Classification: Apollo [NEO]          SPK-ID: 3750672
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 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3315318667546887 0.00050897  
a 1.401604367413949 0.00099794 au
q .9369278550336777 4.7956e-05 au
i 13.99250991721 0.025032 deg
node 21.56633588879643 0.0043357 deg
peri 78.19764258243003 0.0096772 deg
M 238.4861666597528 1.0222 deg
tp 2459205.078415602886
(2020-Dec-21.57841560)
1.9395 TDB
period 606.0892623708014
1.66
0.6473
0.001772
d
yr
n .593971915278305 0.00063436 deg/d
Q 1.86628087979422 0.0013288 au
  Orbit Determination Parameters
   # obs. used (total)      39  
   data-arc span      16 days  
   first obs. used      2016-03-30  
   last obs. used      2016-04-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .37261  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:26:41  

Additional Information
 Earth MOID = .110349 au 
 Jupiter MOID = 3.3749 au 
 T_jup = 4.663 
[ 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 22.9   n/a MPO374806  

[ 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
2006-Mar-08 22:10 4_22:03 Earth 0.229926264888719 0.183661387539984 0.391913462941528 12.815474911351 12.8145706283014 2453803.423538093 7083.40498747409 10367742.1904172 1823.01539445157 -53.0299973068367 14396.50062954 T 5 CATAB v2.0e-lin.ifort 2017-Nov-30 12:34:06 2018-Dec-11 16:58
2010-Oct-31 06:13 9_00:01 Earth 0.266612505850266 0.21649723182069 0.375958368977495 7.23609148887278 7.23471024856911 2455500.759081936 12960.9881695034 7567306.01689863 326.207621371703 54.2817563527019 54731.928258645 T 5 CATAB v2.0e-lin.ifort 2017-Nov-30 12:34:06 2018-Dec-11 16:58
2011-Mar-06 11:54 < 00:01 Earth 0.183432082891195 0.182927466845911 0.218923949089375 9.36430100297175 9.36274969627021 2455626.995999958 0.862781186071063 5340385.65799581 1711.06237917406 85.8888571662279 16304.7461594513 T 5 CATAB v2.0e-lin.ifort 2017-Nov-30 12:34:06 2018-Dec-11 16:58
2015-Nov-05 04:40 00:11 Earth 0.148976139041398 0.148217727349328 0.149734557792747 8.35063884779357 8.34849678772383 2457331.694416088 10.5272648174983 37855.4707700224 6840.39279598465 -3.16920303882354 379.297108664445 T 5 CATAB v2.0e-lin.ifort 2017-Nov-30 12:34:06 2018-Dec-11 16:58
2016-Mar-10 07:39 00:13 Earth 0.237038587928988 0.23595642007989 0.238120752571213 7.63072412039274 7.62925089404091 2457457.818889099 12.9794092920351 53945.7390189719 1306.14731054934 -0.8484008542644 436.283896349754 T 5 CATAB v2.0e-lin.ifort 2017-Nov-30 12:34:06 2018-Dec-11 16:58
2020-Oct-31 21:51 3_10:20 Earth 0.117448853074159 0.110086352264891 0.180873354392279 11.0008358298512 10.9987734027562 2459154.410092990 4939.99044822998 5118835.65459544 1702.98843515724 -69.6553102179614 9385.40802358055 T 5 CATAB v2.0e-lin.ifort 2017-Nov-30 12:34:06 2018-Dec-11 16:58
2025-Oct-26 08:38 7_01:56 Earth 0.227501157919537 0.105599160692656 0.426162032801807 14.7580591077452 14.7572654903524 2460974.859861320 10196.357480084 10539953.5032113 1610.42066500072 -27.6633024141857 9051.03100430813 T 5 CATAB v2.0e-lin.ifort 2017-Nov-30 12:34:06 2018-Dec-11 16:58
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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