. ] | ^ _ `  ^  a b  c d  e f  g h i  j k  l  m  n  o p  q r  s  t u  v w  x y  z {  | }  ~                                          L l    O                           O                                                                                                                    !  "  #  $  %  &  '  (  )  *  +  ,  -  .  /  0  1  2  3  4  5  6  7  8  9  :  ;  <  =  >  ?  @  A  B  C  D  E  F  G  H  I  J  K  L  M  N  O  P  Q  R S  T  U  V  W  X  Y  Z  [  \  ]  ^  _  `  a  b  c  d  e  f  g  h  i  j  k l  m n  o  p  q  r  s  t  u  v  w  x  y  z  {  |  }  ~                                                                                                                                                                                           !  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M [paneLjavax/swing/JPanel;title_b1Ljavax/swing/JButton;level_one_menu_b1level_one_menu_b2level_one_menu_b3level_one_menu_tf1Ljavax/swing/JTextField;level_one_menu_cl1Ljavax/swing/JComboBox;level_one_menu_cl2 add_mp_b1 add_mp_b2 add_mp_b3 delete_mp_b1 edit_mp_b1 edit_mp_b2 edit_mp_b3 edit_mp_b4 edit_mp_b5 edit_mp_b6 edit_mp_b7 edit_mp_b8 edit_mp_b9 edit_mp_b10 edit_mp_b11 edit_mp_b12 edit_mp_b13 add_obs_b1 add_obs_b2 add_obs_b3 add_obs_b4add_optical_obs_1_tf1add_optical_obs_1_tf2add_optical_obs_1_tf3add_optical_obs_1_tf4add_optical_obs_1_tf5add_optical_obs_1_tf6add_optical_obs_1_tf7add_optical_obs_1_tf8add_optical_obs_1_tf9add_optical_obs_1_tf10add_optical_obs_1_tf11add_optical_obs_1_tf12add_optical_obs_1_tf13add_optical_obs_1_tf14add_optical_obs_1_b1add_optical_obs_1_b2add_optical_obs_1_catalogLjava/awt/CheckboxGroup;add_optical_obs_1_FK5Ljava/awt/Checkbox;add_optical_obs_1_FK4add_optical_obs_1_epochadd_optical_obs_1_j2000add_optical_obs_1_b1950add_optical_obs_1_jadd_optical_obs_1_badd_optical_obs_2_tf1add_optical_obs_2_tf2add_optical_obs_2_tf3add_optical_obs_2_tf4add_optical_obs_2_tf5add_optical_obs_2_tf6add_optical_obs_2_tf7add_optical_obs_2_tf8add_optical_obs_2_observatoryadd_optical_obs_2_obscodeadd_optical_obs_2_latlongadd_optical_obs_2_EOPsadd_optical_obs_2_b1add_optical_obs_2_b2add_optical_obs_3_tf1add_optical_obs_3_tf2add_optical_obs_3_tf3add_optical_obs_3_tf4add_optical_obs_3_tf5add_optical_obs_3_tf6add_optical_obs_3_tf7add_optical_obs_3_tf8add_optical_obs_3_tf9add_optical_obs_3_tf10add_optical_obs_3_tf11add_optical_obs_3_tf12add_optical_obs_3_tf13add_optical_obs_3_tf14add_optical_obs_3_tf15add_optical_obs_3_tf16add_optical_obs_3_tf17add_optical_obs_3_tf18add_optical_obs_3_tf19add_optical_obs_3_tf20add_optical_obs_3_tf21add_optical_obs_3_tf22add_optical_obs_3_b1add_optical_obs_3_b2add_radar_obs_1_tf1add_radar_obs_1_tf2add_radar_obs_1_tf3add_radar_obs_1_tf4add_radar_obs_1_tf5add_radar_obs_1_tf6add_radar_obs_1_tf7add_radar_obs_1_tf8add_radar_obs_1_tf9add_radar_obs_1_tf10add_radar_obs_1_tf11add_radar_obs_1_tf12add_radar_obs_1_b1add_radar_obs_1_b2add_radar_obs_1_obstypeadd_radar_obs_1_Delayadd_radar_obs_1_Doppleradd_radar_obs_2_tf1add_radar_obs_2_tf2add_radar_obs_2_tf3add_radar_obs_2_tf4add_radar_obs_2_tf5add_radar_obs_2_tf6add_radar_obs_2_tf7add_radar_obs_2_tf8add_radar_obs_2_tf9add_radar_obs_2_tf10add_radar_obs_2_tf11add_radar_obs_2_tf12add_radar_obs_2_tf13add_radar_obs_2_tf14add_radar_obs_2_b1add_radar_obs_2_b2add_radar_obs_2_xmtradd_radar_obs_2_xmtr_Areciboadd_radar_obs_2_xmtr_DSS13add_radar_obs_2_xmtr_DSS14add_radar_obs_2_xmtr_otheradd_radar_obs_2_rcvradd_radar_obs_2_rcvr_Areciboadd_radar_obs_2_rcvr_DSS13add_radar_obs_2_rcvr_DSS14add_radar_obs_2_rcvr_otheradd_radar_obs_3_tf1add_radar_obs_3_tf2add_radar_obs_3_tf3add_radar_obs_3_tf4add_radar_obs_3_tf5add_radar_obs_3_tf6add_radar_obs_3_tf7add_radar_obs_3_tf8add_radar_obs_3_tf9add_radar_obs_3_tf10add_radar_obs_3_tf11add_radar_obs_3_tf12add_radar_obs_3_tf13add_radar_obs_3_tf14add_radar_obs_3_tf15add_radar_obs_3_tf16add_radar_obs_3_tf17add_radar_obs_3_tf18add_radar_obs_3_tf19add_radar_obs_3_tf20add_radar_obs_3_tf21add_radar_obs_3_tf22add_radar_obs_3_b1add_radar_obs_3_b2input_state_vector_tf0input_state_vector_tf1input_state_vector_tf2input_state_vector_tf3input_state_vector_tf4input_state_vector_tf5input_state_vector_tf6input_state_vector_tf7input_state_vector_tf8input_state_vector_tf9input_state_vector_tf10input_state_vector_tf11input_state_vector_tf12input_state_vector_tf13input_state_vector_tf14input_state_vector_tf15input_state_vector_tf16input_state_vector_tf17input_state_vector_b1input_state_vector_b2input_orbital_elements_tf0input_orbital_elements_tf1input_orbital_elements_tf2input_orbital_elements_tf3input_orbital_elements_tf4input_orbital_elements_tf5input_orbital_elements_tf6input_orbital_elements_tf7input_orbital_elements_tf8input_orbital_elements_tf9input_orbital_elements_tf10input_orbital_elements_tf11input_orbital_elements_tf12input_orbital_elements_tf13input_orbital_elements_tf14input_orbital_elements_tf15input_orbital_elements_tf16input_orbital_elements_tf17input_orbital_elements_b1input_orbital_elements_b2input_orbit_b1input_orbit_b2input_orbit_b3display_orbit_b1display_orbit_b2display_orbit_b3display_orbital_elements_tf0display_orbital_elements_tf1display_orbital_elements_tf2display_orbital_elements_tf3display_orbital_elements_tf4display_orbital_elements_tf5display_orbital_elements_tf6display_orbital_elements_tf7display_orbital_elements_tf8display_orbital_elements_tf9display_orbital_elements_tf10display_orbital_elements_tf11display_orbital_elements_tf12display_orbital_elements_tf13display_orbital_elements_tf14display_orbital_elements_tf15display_orbital_elements_tf16display_orbital_elements_tf17display_orbital_elements_b1display_orbital_elements_b2display_state_vector_tf0display_state_vector_tf1display_state_vector_tf2display_state_vector_tf3display_state_vector_tf4display_state_vector_tf5display_state_vector_tf6display_state_vector_tf7display_state_vector_tf8display_state_vector_tf9display_state_vector_tf10display_state_vector_tf11display_state_vector_tf12display_state_vector_tf13display_state_vector_tf14display_state_vector_tf15display_state_vector_tf16display_state_vector_tf17display_state_vector_b1display_state_vector_b2set_perturbers_choicesset_perturbers_oneset_perturbers_twoset_perturbers_threeset_perturbers_b1set_radius_tf1set_radius_tf2set_radius_tf3 set_radius_b1 set_radius_b2delete_observation_cb1delete_observation_cb2delete_observation_cb3delete_observation_cb4delete_observation_cb5delete_observation_b1delete_observation_b2delete_observation_b3delete_observation_b4check_for_collision_tf1check_for_collision_tf2check_for_collision_tf3check_for_collision_tf4check_for_collision_tf5check_for_collision_tf6check_for_collision_tf7check_for_collision_b1check_for_collision_b2display_ephemeris_1_tf1display_ephemeris_1_tf2display_ephemeris_1_tf3display_ephemeris_1_tf4display_ephemeris_1_tf5display_ephemeris_1_tf6display_ephemeris_1_tf7display_ephemeris_1_tf8display_ephemeris_1_tf9display_ephemeris_1_tf10display_ephemeris_1_tf11display_ephemeris_1_tf12display_ephemeris_1_tf13display_ephemeris_1_tf14display_ephemeris_1_tf15display_ephemeris_1_tf16display_ephemeris_1_tf17display_ephemeris_1_tf18display_ephemeris_1_tf19display_ephemeris_1_tf20display_ephemeris_1_tf21display_ephemeris_1_tf22display_ephemeris_1_tf23display_ephemeris_1_tf24display_ephemeris_1_b1display_ephemeris_1_b2display_ephemeris_1_cb1#display_ephemeris_1_ObservatoryCodedisplay_ephemeris_1_Geocentricdisplay_ephemeris_1_LatLongAltdisplay_ephemeris_2_b1display_ephemeris_2_b2compute_orbit_b1compute_orbit_b2compute_orbit_b3compute_orbit_b4compute_orbit_b5compute_orbit_b6compute_orbit_b7propogate_epoch_1_tf1propogate_epoch_1_tf2propogate_epoch_1_b1propogate_epoch_1_b2compute_residuals_1_b1compute_residuals_1_b2compute_residuals_2_b1compute_residuals_2_b2compute_residuals_2_b3compute_residuals_2_b4compute_best_fit_1_b1compute_best_fit_1_b2compute_best_fit_1_thrustcompute_best_fit_1_thrust_nocompute_best_fit_1_thrust_yescompute_best_fit_1_selection compute_best_fit_1_selection_all compute_best_fit_1_selection_chi%compute_best_fit_1_selection_residualcompute_best_fit_1_tf1compute_best_fit_1_tf2compute_best_fit_1_tf3compute_best_fit_1_tf4select_observations_cl1select_observations_cl2select_observations_cl3select_observations_b1select_observations_b2display_initial_orbit_tf0display_initial_orbit_tf1display_initial_orbit_tf2display_initial_orbit_tf3display_initial_orbit_tf4display_initial_orbit_tf5display_initial_orbit_tf6display_initial_orbit_tf7display_initial_orbit_tf8display_initial_orbit_tf9display_initial_orbit_tf10display_initial_orbit_tf11display_initial_orbit_tf12display_initial_orbit_b1display_initial_orbit_b2display_initial_orbit_b3display_initial_orbit_b4display_initial_orbit_b5display_initial_orbit_b6select_method_b1select_method_b2select_method_b3select_method_b4 set_a_tf1set_a_b1set_a_b2 no_events_b1 read_MPEC_b1 read_MPEC_b2read_neodys_b1read_neodys_b2designate_mp_b1designate_mp_groupdesignate_mp_1designate_mp_2display_physical_properties_tf1display_physical_properties_tf2display_physical_properties_tf3display_physical_properties_tf4display_physical_properties_tf5display_physical_properties_b1display_physical_properties_b2select_duration_b1select_duration_b2select_duration_b3select_duration_b4select_duration_b5select_duration_b6select_duration_b7compare_observations_1_b1compare_observations_1_b2display_candidates_b1display_candidates_b2display_candidates_b3compare_observations_1_choices"compare_observations_1_twobody_com!compare_observations_1_twobody_ascompare_observations_1_nbody compare_observations_1_nbody_all compare_observations_1_nbody_NEAcompare_observations_1_nbody_MB compare_observations_1_nbody_TNOselect_duration_tf1&compare_observations_1_nbody_singleNEA"compare_observations_1_nbody_NEA18"compare_observations_1_nbody_NEA20"compare_observations_1_nbody_NEA30$compare_observations_1_nbody_NEALT20$compare_observations_1_nbody_NEA1830select_duration_groupselect_duration_nominalselect_duration_VIselect_duration_tf2select_duration_group3select_duration_normalselect_duration_weakselect_duration_SR select_mp_cl1 select_mp_b1 select_mp_b2select_duration_group2select_duration_highselect_duration_mediumselect_duration_group4select_duration_normal_filterselect_duration_narrow_filtercompare_observations_1_accuracycompare_observations_1_highcompare_observations_1_medium add_obs_b5select_method_b5 set_rhos_tf1 set_rhos_tf2 set_rhos_b1 set_rhos_b2set_rhos_lschoice set_rhos_lsdisplay_herget_orbit_tf0display_herget_orbit_tf1display_herget_orbit_tf2display_herget_orbit_tf3display_herget_orbit_tf4display_herget_orbit_tf5display_herget_orbit_tf6display_herget_orbit_tf7display_herget_orbit_tf8display_herget_orbit_tf9display_herget_orbit_tf10display_herget_orbit_tf11display_herget_orbit_tf12display_herget_orbit_b1display_herget_orbit_b2display_herget_orbit_b3display_herget_orbit_b4display_herget_orbit_b5display_herget_orbit_b6sample_obs_MC_1_b1sample_obs_MC_1_b2display_obs_MC_1_b1display_obs_MC_1_b2display_obs_MC_1_b3display_obs_MC_1_b4display_obs_MC_1_b5display_obs_MC_1_b6display_ephemeris_1_b3MC_ephem_toggle_display_b1MC_ephem_toggle_display_b2stat_ranging_inputs_tf1stat_ranging_inputs_tf2stat_ranging_inputs_tf4stat_ranging_inputs_tf5stat_ranging_inputs_prograde stat_ranging_inputs_eccentricitystat_ranging_inputs_residualsstat_ranging_orbit4stat_ranging_inputs_2bodystat_ranging_inputs_nbodystat_ranging_inputs_b1stat_ranging_inputs_b2mp LMinorPlanet;gp LGraphing; input_juldateDclassical_elements[Dclassical_elements_uncertainty collision[[Dobservation_counterI event_counterdisplay_ephemeris_timedisplay_ephemeris_intervaldisplay_ephemeris_endtimedisplay_ephemeris_starttimeformatted_ephemerides[Ljava/lang/String;ephemeris_radecephemeris_magnitudesephemeris_support_dataephemeris_counter residuals rms_residualsformatted_observationsformatted_residualsformatted_rms_residualsresidual_counterreset_residual_counter two_body_Lx two_body_Ly two_body_Lz two_body_x two_body_y two_body_z two_body_rtwo_body_rprimepointer[Itwo_body_residualstwo_body_time1two_body_time2two_body_time3two_body_epoch_timetwo_body_recipatwo_body_methodLjava/lang/String; kgaussfailbarycentric_two_body_rbarycentric_two_body_rprimetwo_body_error_messagePHAZobscodeobslongobslatobsalt code_countercollision_durationcandidate_residuals candidatescandidate_sunrcandidate_countercandidate_pointerMonte_Carlo_indexvirtual_impactors[[[Dformatted_collisionsnon_event_counternon_event_arraynominal_eigenvector elapsed_timeimport_designation_arrayimport_elements_arrayimport_counter two_body_rho1 two_body_rho2two_body_times mjd_stringx_stringy_string ut1utc_string lod_string dPsi_stringdEpsilon_string eop_counterMC_state_vectorsMC_orbital_elementsMC_ephemeris_radec MC_counterMC_ephem_counterMC_ephem_display_counterSR_totalSR_flag()VCodeLineNumberTablemain([Ljava/lang/String;)VactionPerformed(Ljava/awt/event/ActionEvent;)VbuildConstraints((Ljava/awt/GridBagConstraints;IIIIIIII)Vlevel_one_menuadd_mp(Ljava/lang/String;)V delete_mpedit_mpadd_obsadd_optical_obs_1cancel_optical_obs_1add_optical_obs_2cancel_optical_obs_2add_optical_obs_3add_radar_obs_1cancel_radar_obs_1add_radar_obs_2cancel_radar_obs_2add_radar_obs_3process_optical_obs_1process_optical_obs_2process_optical_obs_3process_optical_obs_2aprocess_radar_obs_1process_radar_obs_2process_radar_obs_3input_state_vectorinput_orbital_elements input_orbitprocess_input_state_vectorprocess_input_orbital_elements display_orbitdisplay_orbital_elementsdisplay_state_vectorset_perturbersprocess_set_perturbers set_radiusprocess_set_radiuspreprocess_delete_observationback5_delete_observationprocess_delete_observationdelete_observationcheck_for_collisionpreprocess_check_for_collision wait_screenfile_output_check_for_collisiondisplay_ephemeris_2preprocess_display_ephemerisdisplay_ephemeris_1file_output_display_ephemerisformat_ephemeris!preprocess_input_orbital_elements compute_orbitpropogate_epoch_1preprocess_propogate_epochfile_output_propogate_epochfile_output_compute_residualscompute_residuals_1compute_residuals_2preprocess_compute_best_fitfile_output_compute_best_fitcompute_best_fit_1select_observationspostprocess_select_observationspreprocess_two_body select_methodpostprocess_set_aset_apostprocess_initial_orbit accept_orbitdisplay_initial_orbit no_events evaluate_PHA read_MPEC MPEC_readerread_obscode_list neodys_reader read_neodys designate_mpprocess_designate_mpdisplay_physical_propertiesprocess_recalculate_abs_magselect_durationcompare_observations_1mpc_catalog_reader(I)Vmpc_candidate_finder(Ljava/lang/String;[D)V mpc_candidate_apparent_magnitude(D[DDD)D&mpc_candidate_comet_apparent_magnitudefile_output_MPC_comparempc_nbody_candidate_findermpc_get_observed_radec([D[DDZDDDD[D[DD[D[D[D)Vdisplay_candidatesformat_observations_residualserase_observationfind_virtual_impactorscreate_normal_variant([D[D[[D[D[D)V within_VI ([D[DDI)Zformat_collision select_mpinitialize_imported_mpget_covariance_eigenvector([D[[D)Vtrail_file_output(D[[D)Vexpedited_comparisonpreprocess_herget([D[D[D[D[D[D[D)Vpostprocess_set_rhosset_rhos"preprocess_compute_herget_best_fitpostprocess_herget_orbitdisplay_herget_orbitcreate_MC_variant ([D[D[[D)Vsecond_eigenvalue ([D[[[D[[DI)Descape_velocity(I)Deop_file_readerread_optical_eop_parmsread_radar_eop_parmssample_obs_MC_1preprocess_MC_orbitcreate_MC_orbit_variant ([D[D[[D[D)Vdisplay_obs_MC_1qvseqvsiqvswqvsomegaqvsmpreprocess_MC_ephemerisMC_ephem_toggle_displayravsdecstat_ranging_inputspreprocess_SR_orbitcreate_SR_orbit_variant_2 ([D[D[D[D)Vcreate_SR_orbit_variant_nSR_find_virtual_impactors SourceFileGUI.java9Comet/Asteroid Orbit Determination and Ephemeris Software javax/swing/JButtonBegin Create Edit Delete javax/swing/JTextField  javax/swing/JComboBox   Return Exp Comp  Add Rev/Del Compute Display Specify Generate Check Change    Designate Compare Import Optical Radar MPC NEODyS               Submit Cancel java/awt/CheckboxGroup java/awt/Checkbox ICRF or FK5  FK4  J2000 B1950 J B          4Enter the MPC observatory code of the observing site AEnter the latitude, longitude, and altitude of the observing site (Use Default Earth Orientation Parameters                                           Delay Doppler                   Arecibo  DSS13  DSS14  other - enter coords below                                    ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H ISelect J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` aDone bDisplay State Vector c d e f g h i j k l m n o p q r s t u vDisplay Orbital Elements w x# All nine planets and Earth's Moon y- Planets, Moon, plus Ceres, Pallas, and Vesta z! Planets, Moon, and 300 asteroids {Set | } ~   Recalculate      Delete Checked Next 5  Prev 5         Next Event                             Observatory Code  Geocentric Geodetic Latitude: Next 10  Initial Best-Fit  Residuals  Propogate  Obs MC Stat Rng          Phys Props     .Do Not Use Non-Gravitational Thrust Parameters 'Use Non-Gravitational Thrust Parameters  Use all observations 0Exclude observations where chi exceeds threshold 5Exclude observations where residuals exceed threshold                             Gauss conditioned Gauss Laplace      Process      asteroid comet      Display Orb Els            Back 10  Forward 10  Use two-body mechanics .Use two-body mechanics, consider all asteroids Use integrated n-body mechanics 7Use integrated n-body mechanics, consider all asteroids 3Use integrated n-body mechanics, consider only NEAs BUse integrated n-body mechanics, consider only Main-Belt asteroids @Use integrated n-body mechanics, consider only Centaurs and TNOs  >Use integrated n-body mechanics, consider only single-opp NEAs FUse integrated n-body mechanics, consider only NEAs with Abs Mag <= 18 KUse integrated n-body mechanics, consider only NEAs with 18 < Abs Mag <= 20 KUse integrated n-body mechanics, consider only NEAs with 20 < Abs Mag <= 30 FUse integrated n-body mechanics, consider only NEAs with Abs Mag <= 20 KUse integrated n-body mechanics, consider only NEAs with 18 < Abs Mag <= 30   ? @ A B C D E F G H I J K Lq vs. e Mq vs. i Nq vs. w O q vs. omega Pq vs. M Q R SNext T U V W X YRequire prograde orbit ZRequire e < 1.0 [ Require RMS optical residuals < \ ]Use two-body mechanics ^Use n-body mechanics _ ` a MinorPlanet b cGraphing d e f g h i j i k l m n o n p g q g r g s gjava/lang/String t u v l w i x l y n z i { i | u } u ~ u  n n i i i i i i i i u g g g g g n i i u i i i n g l u l n n n u n l i g u i n g g i u u u u u u u n l l n n n n javax/swing/JPanel ~java/awt/GridBagLayoutjava/awt/GridBagConstraints  java/awt/Font monospaced javax/swing/JLabel   Welcome to CODES.!Please press the button to begin. Copyright 2000 by James Baer    java/lang/Exception java/lang/StringBuffer(Can't set cross-platform look and feel:     GUIGUI$1 InnerClasses          7 E )      1 2      i  n  n  n   F    i  i G       H U           ; : 8 9  < = >     differential correction   $ ( I L M  N O P Q R T  S V  n  n  n  n  g  g  n  n  Level One Menu      Create a new minor planet! Edit an existing minor planet  n  u # Delete an existing minor planet  Add a minor planet       Minor planet  has been added. Edit this new minor planet Return to the Level One Menu" Execute an Expedited ComparisonDelete a minor planet   has been deleted.Level Two Menu - minor planet   g  i  i ! i " l # g $ g % g & g ' i ( l ) l * i + i , i - i . i / i 01 2 i 3 i 4 i 5 l 6 l 7 l 8 i 9 i : i ; i < i = l > i ? l @ l A i B i C i D l E i F i G i H i I i J i K i L l M i N l O l P i Q i R i S l T i U i V g W  Designate  as comet or asteroid Add a new observation& Review/Delete existing observations< Compute/Evaluate/Propogate the orbit of this minor planet Display current orbit2 Manually specify an orbit for this minor planet< Import a minor planet from the MPCORBcr or COMET catalogs; Compare observations to positions of known minor planets Generate an optical ephemeris* Check for collisions and/or near misses8 Change the number of perturbing bodies for integrator2 Specify the radius/visual brightness parameters minor planet  Add an optical observation Add a radar observation0 Read observations from an MPEC or MPCOBS file' Read observations from a NEODyS file$ Cancel - Return to Level Two MenuOptical ObservationUTC date year month day.dddddAstrometric Right Ascension hours minutes seconds Uncertainty arc secsAstrometric Declination deg arc minsVisual MagnitudeCatalogEpoch#Cancel - Return to Level Two Menu Location of Observing SiteGeodetic LatitudeEast LongitudeAltitude meters6Earth Orientation Parameters for Observation Timeframe Julian DayxyUT1-UTCdPsidEpsilon('')(s)X YZ [No. of Leap Seconds Earth's Ang Velocity  microrad/secRadar ObservationUTC date of observation:  day hour minute second microseconds Uncertainty  HzTransmitter Frequency MHzLocation of Transmitting SiteLocation of Receiving Site \] ^Z _`- ab cd ef gh ij kl ml nj op *  q [ rZ-Input the Barycentric Equatorial State Vectorfor TDB Epoch #Note: Reference Frame is ICRF/J2000 coordinate covariance AUzxdot AU/dayydotzdot.(Optional Non-Gravitational Thrust Parameters)A1 x 10^(-9) AU/(day)^2A2DT days2Input the Heliocentric Ecliptical Orbital ElementselementaqeiwomegaMT' Enter the classical orbital elements Enter the state vector stu vw xZ y 4) Display the classical orbital elements Display the state vector,The Heliocentric Ecliptical Orbital Elements(Output will also be sent to the file 'ephemeris_output.txt'.)0Create RA/Dec scatterplots using sampled orbits ephemeris_output.txt 0. -0++0 999999  9999.999.99 # Compute an initial two-body orbit" Compute an n-body best-fit orbit0 Sample valid orbits: Observational Monte Carlo* Sample valid orbits: Statistical RangingF Compute the observational residuals resulting from the current orbit, Propogate the current orbit to a new epoch# Cancel - Return to Level Two Menu1Propogate the epoch of the orbit of minor planet Current Epoch (TDB Juldate): Enter New Epoch (TDB Juldate): BOutput will also be sent to the file 'propogate_epoch_output.txt'. propogate_epoch_output.txt>Propogated State Vector and Orbital Elements for minor planet 2Barycentric Equatorial State Vector for TDB Epoch x pos = cov = y pos = z pos = x vel = y vel = z vel = 7Heliocentric Ecliptical Orbital Elements for TDB Epoch a = e = i = w = omega = T = M = q = ,Optional Non-Gravitational Thrust ParametersA1 = A2 = DT = _compute_residuals_output.txt2Computed Observational Residuals for minor planet h OBS ++++UTC DATE+++++ ++RA/DELAY++++++rms+++++resid DEC/DOPPLER++++rms++++resid VMAG CHI OBS4Compute the Observational Residuals of minor planet _compute_residuals_output.txt'.    g  g  g  g    _best_fit_output.txt 200 iterations. Initial solution returned.OSector fails to converge; > 100 iterations. Initial or zero solution returned.CObservations too widely-spaced. Initial or zero solution returned.=conditioned Gauss rho loop diverges. Zero solution returned.Rconditioned Gauss fails to converge; > 200 iterations. Initial solution returned.>Differential Correction diverges. Original solution returned.   Z t  ZObs  =  arc secondsxxx.xx   lPHeliocentric Ecliptical Orbital Elements and Barycentric Equatorial State Vector for TDB Epoch 5WARNING: THIS IS A POTENTIALLY HAZARDOUS MINOR PLANET componentx y z w xdot ydot zdot  Residuals: Accept This OrbitApply Differential Correction$Try Another Value of Semi-Major AxisTry Another Method)Try a Different Set of Three ObservationsQuit#Please press the button to move on.MPC file ReaderJIn order to read and process the MPEC or MPCOBS file, please save the file%(from the web browser or text editor)Was ''mpec.txt'' in the ''codes'' folder, using file-type ''text file'' or ''text-only'',Please press the button to process the MPEC.java/io/FileReaderMPEC.txtjava/io/BufferedReader   Observations: Rr-30 bVvSs1 72.921151467 0.0 ObsCode.txt244500245247248249250 Z neodys.txt! delay obs 251252253254255256 doppler obs NEODyS File ReaderBIn order to read and process the NEODyS file, please save the fileYas ''neodys.txt'' in the ''codes'' folder, using file-type ''text file'' or ''text-only''3Please press the button to process the NEODyS file.Designate minor planet  as an asteroid or as a comet2The estimated physical properties of minor planet :estimated radius =    variant trajectories Set near-miss threshold:  AUsSelect integration accuracy:Select target filtering:KSelect the timeframe over which to search for collisions and/or near misses Through 2030 Through 2050 Through 2075 Through 2100 Through 2150 Through 2200 asteroidscomets Compare optical observations of  to positions of known @Make certain that the current Minor Planet Center Orbit Database>(located at ftp://cfa-ftp.harvard.edu/pub/MPCORB/MPCORBcr.DAT)Ehas been saved to the ''codes'' folder as text file ''MPCORBcr.DAT'' FMake certain that the current Minor Planet Center Comet Orbit Database;(located at ftp://cfa-ftp.harvard.edu/pub/MPCORB/COMET.DAT)Bhas been saved to the ''codes'' folder as text file ''COMET.DAT'' @Output will also be sent to the file ''MPC_compare_output.txt''.   MPCORBcr.DAT COMET.DAT cometold.txtchecking asteroid  candidates so farK181920A1011C1213E14F15G16H17L2122N23O24P25Q26272829U3031W32X33Y3435 P-L T-12 T-2 T-33456789  % checking comet java/io/FileNotFoundExceptionjava/lang/NullPointerExceptionjava/io/EOFException  Z # " ! " Z ZMPC_compare_output.txt MPC Comparison for minor planet FOrdered list of comets with RMS position residuals less than 3 degreesIOrdered list of asteroids with RMS position residuals less than 3 degreesCandidate No. Comet  Asteroid RMS position residual = RMS brightness residual =  magnitudesRMS brightness residual = NA$No viable candidates in MPC catalog Processing time (in minutes) =  & ':Best candidates to match the observations of minor planet ;Best candidates to match the optical observations of comet >Best candidates to match the optical observations of asteroid #No viable candidates in MPC catalog CandidateRMS Position ResidualRMS Brightness ResidualNARMS Optical Residuals = RMS Delay Residuals =  microsecsRMS Doppler Residuals = 00000000000000 # * _~&  3 4creating variant trajectory  ? @  'no. of events for variant trajectory =  l  A B  C D   g  g  g  g  g  g  g  g  g  g  gnumber of trails = 5 6!beginning differential correction#end second update - no of events = event = type = date = miss distance = probability = event number =  to_hit =  distance =  dcos_theta = event_epsilon =  max sigma = #no of events for to_hit_variant =  not_found =  m = Sreversal or differential correction failure - initiating an LOV search with 101 VAs' reversal - Monte Carlo search - VA = number of VIs =  number of near-miss events =  near-miss Vir Imp  SunMercury Venus Earth MarsJupiter Saturn UranusNeptune Pluto MoonImport a minor planetDhas been saved to the ''codes'' folder as text file ''MPCORBcr.DAT''Ahas been saved to the ''codes'' folder as text file ''COMET.DAT''ASelect a minor planet from the drop-down list, and press 'Import'_trail_output.txtNo trails were detected.fDate , Target , MOID , stretching , Distance , i , x , y , z , xdot , ydot , zdot reversal  , *Estimate the slant ranges of minor planet  atApply iterative least squaresTry Other Values of Slant Range#Try a Different Set of Observations eopc04.txtESample valid orbits using Observational Monte Carlo for minor planet J K Select which graphs to display: q vs. e q vs. i q vs. w  q vs. omega q vs. M  graphing_dataEpoch =  TDB  JDisplay Observational Monte Carlo ephemeris scattergrams for minor planet "Move to the next ephemeris entry: JD RADec1004.06.0,Statistical ranging survey for minor planet 4No realistic orbits. Please try a larger RMS error.Create  candidatesSet rho min = Set rho max = !Begin Statistical Ranging Survey C(Note that this will be a lengthy calculation. Please be patient.) W X Y XNumber of candidates = "Total SR variant orbits created = accumulated_attempts =  SR_flag = javax/swing/JFramejava/awt/event/ActionListener.(Ljava/lang/String;ZLjava/awt/CheckboxGroup;)V(Ljava/lang/String;Z)V setLayout(Ljava/awt/LayoutManager;)V(Ljava/lang/String;II)VsetConstraints4(Ljava/awt/Component;Ljava/awt/GridBagConstraints;)VsetFont(Ljava/awt/Font;)Vadd*(Ljava/awt/Component;)Ljava/awt/Component;addActionListener"(Ljava/awt/event/ActionListener;)VsetContentPane(Ljava/awt/Container;)Vjavax/swing/UIManagergetSystemLookAndFeelClassName()Ljava/lang/String;setLookAndFeeljava/lang/SystemerrLjava/io/PrintStream;append,(Ljava/lang/String;)Ljava/lang/StringBuffer;,(Ljava/lang/Object;)Ljava/lang/StringBuffer;toStringjava/io/PrintStreamprintlnaddWindowListener"(Ljava/awt/event/WindowListener;)VsetSize(II)V setVisible(Z)Vjava/awt/event/ActionEvent getSource()Ljava/lang/Object;removeActionListenergetTextcurrent_minor_planetgetSelectedItem optical_timenumber_of_optical_observationsnumber_of_delay_observationsnumber_of_doppler_observationsjava/lang/DoublevalueOf&(Ljava/lang/String;)Ljava/lang/Double; 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