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(2002 MN)
Classification: Apollo [NEO]          SPK-ID: 3127411
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2457000.5 (2014-Dec-09.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .498048372346704 0.00019245  
a 1.814921148681023 0.00079644 AU
q .911002624642829 5.0565e-05 AU
i 1.048994985402677 0.00055797 deg
node 85.27713704052159 0.044835 deg
peri 131.4853330740436 0.059765 deg
M 52.72558921191636 0.80617 deg
tp 2456869.701124634424
(2014-Jul-31.20112463)
1.9138 JED
period 893.0691118946294
2.45
0.58786
0.001609
d
yr
n .4031043008936528 0.00026534 deg/d
Q 2.718839672719216 0.0011931 AU
  Orbit Determination Parameters
   # obs. used (total)      86  
   data-arc span      53 days  
   first obs. used      2002-06-17  
   last obs. used      2002-08-09  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-BIG16  
   condition code      6  
   fit RMS      .52838  
   data source      ORB  
   producer      Otto Matic  
   solution date      2014-Jun-13 02:43:20  

Additional Information
 Earth MOID = .000775993 AU 
 T_jup = 3.891 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 23.6 mag n/a MPO34019  

[ 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
1904-Aug-23 03:56 2_03:03 Mars 0.0448803911804098 0.0445305433938208 0.118704462399698 13.9259094658916 13.9254513945429 2416715.663874884 3062.65672832342 4817585.84815953 164.825606957994 -83.1818239991426 38043.0604733486 T 17 CATAB v2.0c-linF95 2014-Jun-13 02:43:22 2014-Jun-13 02:43
1938-Feb-22 11:04 19:34 Earth 0.298816352597956 0.243850080638219 0.353091151155124 19.3501911401998 19.3497303238194 2428951.961294336 1174.31126097096 2598909.50998815 222.505985011493 -0.432052843131277 1284.07737128451 T 17 CATAB v2.0c-linF95 2014-Jun-13 02:43:22 2014-Jun-13 02:43
1943-Jun-20 06:24 16:29 Earth 0.0471328056781434 0.0303125478755526 0.0634151677300943 11.7039465746042 11.699115470728 2430895.766334509 989.119976059193 629233.497409479 4.26454162192272 -0.517428055053647 9310.73229483801 T 17 CATAB v2.0c-linF95 2014-Jun-13 02:43:22 2014-Jun-13 02:43
1997-Feb-15 14:16 11:49 Earth 0.437387592483494 0.39624350695724 0.478439897796866 23.510492304493 23.5102331930651 2450495.094481418 709.321622293053 2023655.57700679 233.510185778981 -0.176064015252869 751.167065587134 T 17 CATAB v2.0c-linF95 2014-Jun-13 02:43:22 2014-Jun-13 02:43
2002-Jun-13 15:46 < 00:01 Moon 0.000768699215110893 0.000767529072957208 0.000769869387776417 10.3294668308171 10.3253385310748 2452439.156767636 0.672688824305491 59.1293804013853 37.8605582850169 12.1548072445638 1924.20710821578 T 17 CATAB v2.0c-linF95 2014-Jun-13 02:43:22 2014-Jun-13 02:43
2002-Jun-14 02:03 < 00:01 Earth 0.000801907674944537 0.000801173109157139 0.000802642215569571 10.5732148934938 10.2541465419596 2452439.585651664 0.650509438131799 35.9214669938873 4.85850890028536 2.17211177203655 2169.85379482506 T 17 CATAB v2.0c-linF95 2014-Jun-13 02:43:22 2014-Jun-13 02:43
2007-Feb-21 03:23 14:44 Earth 0.288215830726987 0.246962643298849 0.32907203480532 18.9911089051016 18.990622106001 2454152.640770926 883.902470956412 1951893.36851313 34.6109676717527 -3.3825784829963 63210.7166961203 T 17 CATAB v2.0c-linF95 2014-Jun-13 02:43:22 2014-Jun-13 02:43
2014-Oct-30 22:38 1_09:42 Mars 0.0267893767647932 0.0265420267562399 0.0923609425130366 13.8382915325034 13.8375192552925 2456961.442962323 2021.62194220081 4021134.79808819 35.096158835453 -81.9912845743876 106244.010624926 T 17 CATAB v2.0c-linF95 2014-Jun-13 02:43:22 2014-Jun-13 02:43
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Close-Approach Data ]
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