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JPL Small-Body Database Browser
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(2017 UV7)
Classification: Apollo [NEO]          SPK-ID: 3788086
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4460730923696458 0.00021497  
a 1.548755573518413 0.0005399 au
q .8578973855143299 3.3935e-05 au
i 13.20236091850305 0.0051078 deg
node 32.86124042269986 2.5521e-05 deg
peri 60.87325191402673 0.0023981 deg
M 256.3970436266178 0.13102 deg
tp 2458803.101379433057
(2019-Nov-15.60137943)
0.36215 TDB
period 704.0001477664343
1.93
0.36812
0.001008
d
yr
n .511363529030731 0.00026739 deg/d
Q 2.239613761522496 0.00078073 au
  Orbit Determination Parameters
   # obs. used (total)      37  
   data-arc span      3 days  
   first obs. used      2017-10-27  
   last obs. used      2017-10-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .29205  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Oct-31 06:19:37  

Additional Information
 Earth MOID = .0152299 au 
 Jupiter MOID = 3.05936 au 
 T_jup = 4.310 
[ 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 MPO421551  

[ 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
1960-Mar-04 17:23 11:26 Earth 0.219819381411932 0.219653971955222 0.220004305575459 13.9925964009769 13.9917301145466 2436998.224277623 685.499653046581 104533.351639759 1127.7176418405 -85.2482712654772 24921.541809403 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
1961-Nov-16 16:28 4_08:49 Earth 0.142042203986042 0.119926268228084 0.164371525821309 9.71146004013518 9.70952827811618 2437620.186088755 6288.75857452397 1141671.95300034 105.532054021477 -13.7213119660488 50916.5316890327 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
1962-Mar-12 13:03 6_16:03 Earth 0.406476999997398 0.387589045568727 0.427205975915331 6.90362046398166 6.90267088882947 2437736.043801919 9602.77219087822 1684893.59650113 278.023829649923 54.0027306736713 140062.316664195 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
1963-Oct-11 16:22 2_04:22 Earth 0.287472622122938 0.233314417316741 0.341642288932967 19.9560311823092 19.9555667239897 2438314.181746436 3141.97454617498 2702452.8849299 17.318023550628 1.91590853117409 77257.7032456521 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2010-Aug-03 20:49 2_14:14 Mars 0.0149418481253844 0.0147315311438496 0.0616028078418357 13.1713929956306 13.1699382262709 2455412.367244024 3734.08895841389 2860181.00533245 341.259152992957 -80.5338022276268 6438.01117207864 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2014-Mar-20 07:01 1_05:29 Earth 0.442226937655594 0.408316324057481 0.47677510752585 22.7402793313307 22.7400143752456 2456736.792404620 1768.56030645106 1901260.63111284 377.751618207156 -26.0517067846466 71857.5747145691 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2016-Feb-25 15:42 1_04:24 Earth 0.204835969068142 0.200209310221205 0.211115246710519 9.78685836917124 9.78552916307212 2457444.154039049 1704.31203105707 957868.65095271 445.58824393297 73.4316411132337 76300.8164284135 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2017-Oct-29 03:56 < 00:01 Earth 0.0156930001639341 0.015673166833156 0.0157128333852941 12.4937325995803 12.4801353658852 2458055.664131655 0.0786013077451272 986.84197554851 4.53088032499758 -0.0170998468789961 1639.67012078918 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2019-Oct-03 05:22 15:58 Earth 0.45458960994953 0.435999138557079 0.473181598348005 24.638388303185 24.638150409643 2458759.723912172 957.874544089725 927993.870742131 19.5997111960952 2.56786661095326 145715.020146137 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2041-Mar-17 12:09 7_08:27 Earth 0.386411719775233 0.223936147705314 0.586290219377426 20.9469314888041 20.9466022999917 2466596.006574737 10586.5787727432 10882653.2710393 377.904871021338 -29.5013184614252 70318.7674816548 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2068-Mar-09 07:20 4_00:55 Earth 0.248329235491241 0.202229871958585 0.31743298493242 15.871361857037 15.8706858058783 2476449.805603870 5815.36397725193 4773375.76861053 408.047256824909 -50.9805856861865 67190.087711617 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2071-Oct-12 21:26 2_21:59 Earth 0.276214052619726 0.21103543631161 0.341392090383506 19.673246396787 19.6727560583168 2477762.392860696 4199.22547566415 3250118.51393491 20.1002279720057 -0.0655442518447005 1789.02376939771 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2089-Aug-06 09:39 2_20:45 Mars 0.0865698157459019 0.0251793846751268 0.156128968630873 14.4559434767154 14.455714707971 2484269.902243574 4125.02376995676 3529862.20095726 309.891278713974 14.3981896943672 10245.8086500161 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2093-Mar-23 14:19 3_12:39 Earth 0.49208096198514 0.383100605464719 0.605478249809022 24.4068612034729 24.406639350202 2485595.096289969 5078.97073168103 6013209.29850516 366.736807860502 -22.1518507710248 70778.3384124993 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2095-Mar-01 09:26 6_19:50 Earth 0.194174421114027 0.193612133015091 0.247285404327577 11.0063224266656 11.0050756096917 2486302.893020449 9830.15482347577 6939957.30349291 431.177949101317 85.6667007534651 71912.087614712 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2098-Oct-05 13:35 5_01:47 Earth 0.415660721788889 0.279310382536289 0.552057422727549 23.5374394135333 23.5371670702513 2487617.065695386 7306.7882434906 6803918.53254493 21.3902977336063 1.76301232477913 83398.9058640861 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2122-Mar-06 21:56 2_17:42 Earth 0.204430170612539 0.194389979656212 0.228704967937246 13.4178137742105 13.4168423669913 2496169.414139154 3942.17052389114 2845081.6213911 454.759313106517 -71.8723262580415 63017.9938257428 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2125-Oct-11 17:01 3_19:07 Earth 0.313566360119905 0.223558099514705 0.403574237803839 20.7076364622855 20.7072261101828 2497484.208944245 5466.58388855748 4488305.23418099 22.5134054213388 0.24445203953224 7862.63775217316 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2149-Mar-15 21:48 9_06:43 Earth 0.320660867049064 0.189811102937962 0.542872863416674 18.8242169004467 18.8237754778431 2506040.408537148 13363.2462503019 12471109.3546277 396.212401565456 -36.2543664741027 66983.0642238905 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2162-Dec-10 18:40 8_02:10 Mars 0.0262806714185766 0.0260492715122315 0.176848011698712 13.1730074069191 13.1721804204062 2511058.277807232 11649.7479149428 8551601.98243425 346.449313836073 -82.5063892087164 11192.9610450717 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
2176-Mar-21 15:23 9_02:44 Earth 0.424383685949339 0.21744808060917 0.67704926009503 22.3357903231354 22.335509226864 2515908.140721837 13123.9749928211 13448858.7508603 387.037531931895 -26.1095231247734 67419.1373792162 T 3 CATAB v2.0e-lin.ifort 2017-Nov-30 18:28:27 2018-Dec-11 17:17
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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