[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: July 2nd 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


187/05:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 8
000/00:00:00 000 0 0 0 0 216 2

191/20:25:31 000 0 0 0 2 0 2
N/A -0 2 0 0 220 1
000/00:00:58 000 0 0 -0 0 216 0

193/18:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 215 9

197/12:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 215 7

Coasting Arc #1 (Orbit 88)
---------------------------------------

Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1685218
15                 A    =         6787623
40  meter
 Y    =       -6173869
32  meter          E    =           
0003508
 Z    =       -2255673
19                 I    =           51
33241
 XDOT =       5401
217275                 Wp   =            7
66374
 YDOT =       -502
866809  meter/sec      RA   =          301
65007  deg
 ZDOT =       5416
015155                 TA   =          327
13806
                                          MA   =          327
15986
                                          Ha   =            219
961  n
mi
                                          Hp   =            216
239

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5528930
95                 X    =         1765087
53
 Y    =      -20255476
78  feet           Y    =        -6154577
21  meter
 Z    =       -7400502
59                 Z    =        -2247293
84
 XDOT =      17720
529118                 XDOT =        5380
131253
 YDOT =      -1649
825488  feet/sec       YDOT =        -442
585215  meter/sec
 ZDOT =      17769
078594                 ZDOT =        5442
200774

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20902692
37                 X    =        -6371140
63
 Y    =       -2120893
61  feet           Y    =         -646448
37  meter
 Z    =       -7362072
92                 Z    =        -2243959
83
 XDOT =      -4716
132402                 XDOT =       -1437
477156
 YDOT =     -15556
529589  feet/sec       YDOT =       -4741
630219  meter/sec
 ZDOT =      17886
285393                 ZDOT =        5451
739788


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18183
50446117  
00016717  00000-0  10270-3 0  9006
2 25544  51
6408 302
3636 0003757 256
3328 103
7407 15
53979983   898


Satellite: ISS
Catalog Number: 25544
Epoch time:      18183
50446117   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       302
3636  deg
Eccentricity:     
0003757     
Arg of perigee:   256
3328  deg
Mean anomaly:     103
7407  deg
Mean motion:   15
53979983  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              89
Checksum:              318


Coasting Arc #2 (Orbit 104)
---------------------------------------

Vector Time (GMT): 2018/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2562192
66                 A    =         6789552
79  meter
 Y    =        6247646
23  meter          E    =           
0011110
 Z    =         641055
33                 I    =           51
32179
 XDOT =      -4670
212639                 Wp   =          143
57420
 YDOT =      -1300
943383  meter/sec      RA   =          296
65733  deg
 ZDOT =      -5942
921206                 TA   =           29
47239
                                          MA   =           29
40980
                                          Ha   =            219
874  n
mi
                                          Hp   =            216
247

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8406143
90                 X    =        -2634979
00
 Y    =       20497527
02  feet           Y    =         6218586
99  meter
 Z    =        2103199
90                 Z    =          628433
10
 XDOT =     -15322
219943                 XDOT =       -4626
450814
 YDOT =      -4268
186952  feet/sec       YDOT =       -1352
923619  meter/sec
 ZDOT =     -19497
772987                 ZDOT =       -5965
501051

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21695792
82                 X    =         6612877
65
 Y    =        4510277
98  feet           Y    =         1374732
73  meter
 Z    =        2045796
97                 Z    =          623558
92
 XDOT =      -1076
645481                 XDOT =        -328
161543
 YDOT =      14136
418853  feet/sec       YDOT =        4308
780466  meter/sec
 ZDOT =     -19598
575892                 ZDOT =       -5973
645932


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18184
53337937  
00016717  00000-0  10270-3 0  9010
2 25544  51
6400 297
2359 0003824 257
6302 102
4423 15
53995443  1057


Satellite: ISS
Catalog Number: 25544
Epoch time:      18184
53337937   =   yrday
fracday
Element set:     901
Inclination:       51
6400  deg
RA of node:       297
2359  deg
Eccentricity:     
0003824     
Arg of perigee:   257
6302  deg
Mean anomaly:     102
4423  deg
Mean motion:   15
53995443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             105
Checksum:              301


Coasting Arc #3 (Orbit 120)
---------------------------------------

Vector Time (GMT): 2018/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3216329
52                 A    =         6789217
83  meter
 Y    =       -5884824
85  meter          E    =           
0010417
 Z    =        1019493
94                 I    =           51
30811
 XDOT =       3824
618546                 Wp   =           46
60895
 YDOT =       3113
109189  meter/sec      RA   =          291
66531  deg
 ZDOT =       5872
935789                 TA   =          324
49286
                                          MA   =          324
56214
                                          Ha   =            219
828  n
mi
                                          Hp   =            216
188

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10552262
22                 X    =         3276944
10
 Y    =      -19307168
14  feet           Y    =        -5848518
81  meter
 Z    =        3344796
39                 Z    =         1035264
28
 XDOT =      12547
961108                 XDOT =        3760
995314
 YDOT =      10213
612826  feet/sec       YDOT =        3155
522432  meter/sec
 ZDOT =      19268
162038                 ZDOT =        5891
360035

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21026887
55                 X    =        -6408995
32
 Y    =       -6442371
48  feet           Y    =        -1963634
83  meter
 Z    =        3416210
24                 Z    =         1041260
88
 XDOT =       7045
954550                 XDOT =        2147
606947
 YDOT =     -12683
522703  feet/sec       YDOT =       -3865
937720  meter/sec
 ZDOT =      19350
109931                 ZDOT =        5897
913507


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18185
56229313  
00016717  00000-0  10270-3 0  9023
2 25544  51
6412 292
1078 0003733 263
9719  96
1008 15
54009489  1216


Satellite: ISS
Catalog Number: 25544
Epoch time:      18185
56229313   =   yrday
fracday
Element set:     902
Inclination:       51
6412  deg
RA of node:       292
1078  deg
Eccentricity:     
0003733     
Arg of perigee:   263
9719  deg
Mean anomaly:      96
1008  deg
Mean motion:   15
54009489  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             121
Checksum:              303


Coasting Arc #4 (Orbit 135)
---------------------------------------

Vector Time (GMT): 2018/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3691106
00                 A    =         6786751
16  meter
 Y    =        5065242
88  meter          E    =           
0003190
 Z    =       -2599008
21                 I    =           51
28821
 XDOT =      -2922
550240                 Wp   =          174
83463
 YDOT =      -4802
022298  meter/sec      RA   =          286
66896  deg
 ZDOT =      -5211
748554                 TA   =           34
56544
                                          MA   =           34
54470
                                          Ha   =            219
779  n
mi
                                          Hp   =            216
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12109927
81                 X    =        -3734848
08
 Y    =       16618250
92  feet           Y    =         5023722
03  meter
 Z    =       -8526929
82                 Z    =        -2617044
00
 XDOT =      -9588
419423                 XDOT =       -2843
319751
 YDOT =     -15754
666333  feet/sec       YDOT =       -4834
260814  meter/sec
 ZDOT =     -17098
912579                 ZDOT =       -5225
753174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18840841
52                 X    =         5742688
49
 Y    =        8151336
26  feet           Y    =         2484527
29  meter
 Z    =       -8608342
21                 Z    =        -2623822
71
 XDOT =     -12724
369369                 XDOT =       -3878
387784
 YDOT =      11300
311569  feet/sec       YDOT =        3444
334966  meter/sec
 ZDOT =     -17160
851661                 ZDOT =       -5230
627586


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18186
52689592  
00016717  00000-0  10270-3 0  9030
2 25544  51
6407 287
3005 0003757 267
5989  92
4734 15
54010783  1361


Satellite: ISS
Catalog Number: 25544
Epoch time:      18186
52689592   =   yrday
fracday
Element set:     903
Inclination:       51
6407  deg
RA of node:       287
3005  deg
Eccentricity:     
0003757     
Arg of perigee:   267
5989  deg
Mean anomaly:      92
4734  deg
Mean motion:   15
54010783  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             136
Checksum:              335


Coasting Arc #5 (Orbit 146)
---------------------------------------

Vector Time (GMT): 2018/187/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2058942
54                 A    =         6783026
07  meter
 Y    =       -5127529
78  meter          E    =           
0003028
 Z    =       -3937744
74                 I    =           51
26581
 XDOT =       4403
568959                 Wp   =          119
32429
 YDOT =      -4835
349041  meter/sec      RA   =          282
98703  deg
 ZDOT =       3994
707213                 TA   =          192
60296
                                          MA   =          192
61053
                                          Ha   =            219
778  n
mi
                                          Hp   =            216
159

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6755060
84                 X    =        -1982324
68
 Y    =      -16822604
26  feet           Y    =        -5150125
55  meter
 Z    =      -12919110
05                 Z    =        -3947560
69
 XDOT =      14447
404720                 XDOT =        4437
907791
 YDOT =     -15864
006040  feet/sec       YDOT =       -4785
913645  meter/sec
 ZDOT =      13105
994792                 ZDOT =        4016
181103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7975544
76                 X    =        -2430946
04
 Y    =      -16245134
54  feet           Y    =        -4951517
01  meter
 Z    =      -12962274
30                 Z    =        -3950901
21
 XDOT =      11879
560439                 XDOT =        3620
890022
 YDOT =     -16364
688032  feet/sec       YDOT =       -4987
956912  meter/sec
 ZDOT =      13202
743588                 ZDOT =        4024
196246


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18187
23426875  
00016717  00000-0  10270-3 0  9043
2 25544  51
6371 283
7759 0003806 276
7347  83
3372 15
54021328  1478


Satellite: ISS
Catalog Number: 25544
Epoch time:      18187
23426875   =   yrday
fracday
Element set:     904
Inclination:       51
6371  deg
RA of node:       283
7759  deg
Eccentricity:     
0003806     
Arg of perigee:   276
7347  deg
Mean anomaly:      83
3372  deg
Mean motion:   15
54021328  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             147
Checksum:              325


Coasting Arc #6 (Orbit 162)
---------------------------------------

Vector Time (GMT): 2018/188/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1268047
10                 A    =         6786591
17  meter
 Y    =        6123316
56  meter          E    =           
0009510
 Z    =        2625964
01                 I    =           51
27251
 XDOT =      -4652
139428                 Wp   =          102
72201
 YDOT =       3195
782386  meter/sec      RA   =          277
98011  deg
 ZDOT =      -5191
692918                 TA   =           47
52212
                                          MA   =           47
44178
                                          Ha   =            219
699  n
mi
                                          Hp   =            216
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4160259
51                 X    =         1186724
72
 Y    =       20089621
25  feet           Y    =         6137041
78  meter
 Z    =        8615367
49                 Z    =         2631926
80
 XDOT =     -15262
924634                 XDOT =       -4662
311335
 YDOT =      10484
850349  feet/sec       YDOT =        3143
702577  meter/sec
 ZDOT =     -17033
113249                 ZDOT =       -5214
315756

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6013100
65                 X    =         1832793
08
 Y    =       19603522
00  feet           Y    =         5975153
51  meter
 Z    =        8641165
65                 Z    =         2633827
29
 XDOT =     -12643
567615                 XDOT =       -3853
759409
 YDOT =      11451
194490  feet/sec       YDOT =        3490
324081  meter/sec
 ZDOT =     -17134
758152                 ZDOT =       -5222
674285


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18188
26317242  
00016717  00000-0  10270-3 0  9055
2 25544  51
6379 278
6473 0004075 282
4477  77
6220 15
54059046  1633


Satellite: ISS
Catalog Number: 25544
Epoch time:      18188
26317242   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:       278
6473  deg
Eccentricity:     
0004075     
Arg of perigee:   282
4477  deg
Mean anomaly:      77
6220  deg
Mean motion:   15
54059046  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             163
Checksum:              322


Coasting Arc #7 (Orbit 177)
---------------------------------------

Vector Time (GMT): 2018/189/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -508733
37                 A    =         6789141
95  meter
 Y    =       -6680104
26  meter          E    =           
0008704
 Z    =       -1066781
71                 I    =           51
27644
 XDOT =       4772
795630                 Wp   =           14
82172
 YDOT =      -1296
324579  meter/sec      RA   =          272
98041  deg
 ZDOT =       5860
294155                 TA   =          333
54998
                                          MA   =          333
59438
                                          Ha   =            219
852  n
mi
                                          Hp   =            216
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1669072
75                 X    =         -428814
94
 Y    =      -21916352
55  feet           Y    =        -6685346
29  meter
 Z    =       -3499940
00                 Z    =        -1069059
59
 XDOT =      15658
778315                 XDOT =        4758
470554
 YDOT =      -4253
033397  feet/sec       YDOT =       -1243
032632  meter/sec
 ZDOT =      19226
686860                 ZDOT =        5883
443804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4114573
53                 X    =        -1254122
01
 Y    =      -21589760
78  feet           Y    =        -6580559
09  meter
 Z    =       -3509188
92                 Z    =        -1069600
78
 XDOT =      13375
969504                 XDOT =        4076
995505
 YDOT =      -5681
099767  feet/sec       YDOT =       -1731
599209  meter/sec
 ZDOT =      19330
417302                 ZDOT =        5891
911194


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18189
22776959  
00016717  00000-0  10270-3 0  9067
2 25544  51
6372 273
8384 0003808 284
0531  76
0198 15
54025370  1782


Satellite: ISS
Catalog Number: 25544
Epoch time:      18189
22776959   =   yrday
fracday
Element set:     906
Inclination:       51
6372  deg
RA of node:       273
8384  deg
Eccentricity:     
0003808     
Arg of perigee:   284
0531  deg
Mean anomaly:      76
0198  deg
Mean motion:   15
54025370  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             178
Checksum:              333


Coasting Arc #8 (Orbit 193)
---------------------------------------

Vector Time (GMT): 2018/190/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -260958
25                 A    =         6789325
77  meter
 Y    =        6751523
66  meter          E    =           
0007576
 Z    =        -621196
76                 I    =           51
27669
 XDOT =      -4791
866997                 Wp   =          152
72327
 YDOT =       -728
537317  meter/sec      RA   =          267
98586  deg
 ZDOT =      -5940
618185                 TA   =           34
01591
                                          MA   =           33
96737
                                          Ha   =            219
940  n
mi
                                          Hp   =            216
038

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -856162
24                 X    =         -333418
80
 Y    =       22150668
19  feet           Y    =         6748200
38  meter
 Z    =       -2038047
11                 Z    =         -622639
52
 XDOT =     -15721
348416                 XDOT =       -4754
507761
 YDOT =      -2390
214294  feet/sec       YDOT =        -781
913618  meter/sec
 ZDOT =     -19490
217142                 ZDOT =       -5963
804776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2048506
65                 X    =          624384
83
 Y    =       22071668
45  feet           Y    =         6727444
54  meter
 Z    =       -2045439
63                 Z    =         -623450
00
 XDOT =     -14160
975354                 XDOT =       -4316
265288
 YDOT =       -490
764434  feet/sec       YDOT =        -149
584999  meter/sec
 ZDOT =     -19593
833643                 ZDOT =       -5972
200494


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18190
25666785  
00016717  00000-0  10270-3 0  9078
2 25544  51
6371 268
7101 0003792 291
8721  68
2028 15
54072341  1943


Satellite: ISS
Catalog Number: 25544
Epoch time:      18190
25666785   =   yrday
fracday
Element set:     907
Inclination:       51
6371  deg
RA of node:       268
7101  deg
Eccentricity:     
0003792     
Arg of perigee:   291
8721  deg
Mean anomaly:      68
2028  deg
Mean motion:   15
54072341  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             194
Checksum:              315


Coasting Arc #9 (Orbit 209)
---------------------------------------

Vector Time (GMT): 2018/191/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1021804
58                 A    =         6787491
16  meter
 Y    =       -6323062
01  meter          E    =           
0011255
 Z    =        2227046
05                 I    =           51
27153
 XDOT =       4713
733005                 Wp   =           59
74211
 YDOT =       2678
151678  meter/sec      RA   =          262
98843  deg
 ZDOT =       5426
106117                 TA   =          325
15429
                                          MA   =          325
22792
                                          Ha   =            219
969  n
mi
                                          Hp   =            216
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3352377
22                 X    =         1081617
06
 Y    =      -20744954
11  feet           Y    =        -6311301
39  meter
 Z    =        7306581
53                 Z    =         2232153
94
 XDOT =      15465
003297                 XDOT =        4657
077727
 YDOT =       8786
586871  feet/sec       YDOT =        2730
546300  meter/sec
 ZDOT =      17802
185422                 ZDOT =        5448
866560

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         213568
31                 X    =           65095
62
 Y    =      -21004732
18  feet           Y    =        -6402242
37  meter
 Z    =        7330300
27                 Z    =         2234275
52
 XDOT =      14941
579325                 XDOT =        4554
193378
 YDOT =       6417
114610  feet/sec       YDOT =        1955
936533  meter/sec
 ZDOT =      17903
636100                 ZDOT =        5457
028283


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18191
28556622  
00016717  00000-0  10270-3 0  9081
2 25544  51
6362 263
5813 0003669 290
7729  69
3030 15
54033579  2109


Satellite: ISS
Catalog Number: 25544
Epoch time:      18191
28556622   =   yrday
fracday
Element set:     908
Inclination:       51
6362  deg
RA of node:       263
5813  deg
Eccentricity:     
0003669     
Arg of perigee:   290
7729  deg
Mean anomaly:      69
3030  deg
Mean motion:   15
54033579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             210
Checksum:              314


Coasting Arc #10 (Orbit 218)
---------------------------------------

Vector Time (GMT): 2018/191/20:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944252
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4346853
14                 A    =         6778834
67  meter
 Y    =       -1319129
83  meter          E    =           
0009302
 Z    =       -5040003
46                 I    =           51
24767
 XDOT =        148
925558                 Wp   =           97
89233
 YDOT =      -7440
198346  meter/sec      RA   =          259
82248  deg
 ZDOT =       1820
534601                 TA   =          189
83938
                                          MA   =          189
85761
                                          Ha   =            220
102  n
mi
                                          Hp   =            216
019

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14261329
20                 X    =        -4307297
62
 Y    =       -4327853
76  feet           Y    =        -1367517
36  meter
 Z    =      -16535444
43                 Z    =        -5061023
03
 XDOT =        488
600912                 XDOT =         223
269671
 YDOT =     -24410
099560  feet/sec       YDOT =       -7438
117565  meter/sec
 ZDOT =       5972
882550                 ZDOT =        1821
437407

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11768338
44                 X    =         3586989
56
 Y    =       -8972698
33  feet           Y    =        -2734878
45  meter
 Z    =      -16629300
83                 Z    =        -5068610
89
 XDOT =      18914
858391                 XDOT =        5765
248838
 YDOT =      13739
077612  feet/sec       YDOT =        4187
670856  meter/sec
 ZDOT =       5977
935098                 ZDOT =        1822
074618


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18191
86432034  
00016717  00000-0  10270-3 0  9096
2 25544  51
6388 260
7002 0004009 297
3016  62
7728 15
53997091  2194


Satellite: ISS
Catalog Number: 25544
Epoch time:      18191
86432034   =   yrday
fracday
Element set:     909
Inclination:       51
6388  deg
RA of node:       260
7002  deg
Eccentricity:     
0004009     
Arg of perigee:   297
3016  deg
Mean anomaly:      62
7728  deg
Mean motion:   15
53997091  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             219
Checksum:              314


Coasting Arc #11 (Orbit 234)
---------------------------------------

Vector Time (GMT): 2018/192/20:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944252
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4357359
93                 A    =         6781812
95  meter
 Y    =        2945341
49  meter          E    =           
0007811
 Z    =        4279619
24                 I    =           51
26483
 XDOT =      -1090
794076                 Wp   =           48
99710
 YDOT =       6728
878733  meter/sec      RA   =          254
80358  deg
 ZDOT =      -3511
130326                 TA   =           76
99240
                                          MA   =           76
90520
                                          Ha   =            220
178  n
mi
                                          Hp   =            216
095

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14295800
28                 X    =         4303312
52
 Y    =        9663193
88  feet           Y    =         2993765
58  meter
 Z    =       14040745
55                 Z    =         4300654
82
 XDOT =      -3578
720723                 XDOT =       -1148
902118
 YDOT =      22076
373796  feet/sec       YDOT =        6716
356408  meter/sec
 ZDOT =     -11519
456450                 ZDOT =       -3516
568982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16028537
92                 X    =        -4885498
36
 Y    =        6180011
72  feet           Y    =         1883667
57  meter
 Z    =       14134467
96                 Z    =         4308185
83
 XDOT =     -15709
906834                 XDOT =       -4788
379603
 YDOT =     -14272
286391  feet/sec       YDOT =       -4350
192892  meter/sec
 ZDOT =     -11544
693023                 ZDOT =       -3518
822433


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18192
89323748  
00016717  00000-0  10270-3 0  9103
2 25544  51
6390 255
5724 0004067 302
5638  57
5121 15
54006738  2350


Satellite: ISS
Catalog Number: 25544
Epoch time:      18192
89323748   =   yrday
fracday
Element set:     910
Inclination:       51
6390  deg
RA of node:       255
5724  deg
Eccentricity:     
0004067     
Arg of perigee:   302
5638  deg
Mean anomaly:      57
5121  deg
Mean motion:   15
54006738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             235
Checksum:              307


Coasting Arc #12 (Orbit 248)
---------------------------------------

Vector Time (GMT): 2018/193/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944252
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3345782
39                 A    =         6778413
67  meter
 Y    =        2894729
75  meter          E    =           
0011448
 Z    =       -5145496
18                 I    =           51
26019
 XDOT =      -3577
489155                 Wp   =           64
44730
 YDOT =      -6626
899016  meter/sec      RA   =          250
21240  deg
 ZDOT =      -1399
515833                 TA   =          191
99204
                                          MA   =          192
01933
                                          Ha   =            220
366  n
mi
                                          Hp   =            215
914

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10976976
35                 X    =        -3352909
66
 Y    =        9497144
85  feet           Y    =         2857275
89  meter
 Z    =      -16881549
15                 Z    =        -5161765
43
 XDOT =     -11737
169144                 XDOT =       -3496
321456
 YDOT =     -21741
794671  feet/sec       YDOT =       -6666
450902  meter/sec
 ZDOT =      -4591
587378                 ZDOT =       -1416
697723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4962964
21                 X    =         1512711
49
 Y    =      -13549263
88  feet           Y    =        -4129815
63  meter
 Z    =      -16954731
09                 Z    =        -5167802
04
 XDOT =      19728
224705                 XDOT =        6013
162890
 YDOT =      13076
839986  feet/sec       YDOT =        3985
820828  meter/sec
 ZDOT =      -4667
596613                 ZDOT =       -1422
683448


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18193
79353846  
00016717  00000-0  10270-3 0  9116
2 25544  51
6371 251
0847 0004027 306
0901  53
9878 15
53996166  2490


Satellite: ISS
Catalog Number: 25544
Epoch time:      18193
79353846   =   yrday
fracday
Element set:     911
Inclination:       51
6371  deg
RA of node:       251
0847  deg
Eccentricity:     
0004027     
Arg of perigee:   306
0901  deg
Mean anomaly:      53
9878  deg
Mean motion:   15
53996166  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             249
Checksum:              330


Coasting Arc #13 (Orbit 264)
---------------------------------------

Vector Time (GMT): 2018/194/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944252
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4068075
52                 A    =         6777785
82  meter
 Y    =       -1273056
27  meter          E    =           
0003588
 Z    =        5270328
57                 I    =           51
27051
 XDOT =       2854
369622                 Wp   =          350
79298
 YDOT =       7100
523599  meter/sec      RA   =          245
18876  deg
 ZDOT =       -484
660436                 TA   =          103
87420
                                          MA   =          103
83428
                                          Ha   =            220
318  n
mi
                                          Hp   =            215
994

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13346704
47                 X    =         4056408
89
 Y    =       -4176693
80  feet           Y    =        -1227630
24  meter
 Z    =       17291104
22                 Z    =         5290060
95
 XDOT =       9364
729732                 XDOT =        2777
111651
 YDOT =      23295
681098  feet/sec       YDOT =        7132
011223  meter/sec
 ZDOT =      -1590
093295                 ZDOT =        -470
981785

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9422149
24                 X    =        -2871871
09
 Y    =       10185039
69  feet           Y    =         3104400
10  meter
 Z    =       17379575
57                 Z    =         5297294
63
 XDOT =     -18946
822625                 XDOT =       -5774
991536
 YDOT =     -14898
096927  feet/sec       YDOT =       -4540
939943  meter/sec
 ZDOT =      -1529
795549                 ZDOT =        -466
281683


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18194
82245283  
00016717  00000-0  10270-3 0  9127
2 25544  51
6372 245
9572 0004080 309
8952  50
1841 15
54003444  2650


Satellite: ISS
Catalog Number: 25544
Epoch time:      18194
82245283   =   yrday
fracday
Element set:     912
Inclination:       51
6372  deg
RA of node:       245
9572  deg
Eccentricity:     
0004080     
Arg of perigee:   309
8952  deg
Mean anomaly:      50
1841  deg
Mean motion:   15
54003444  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             265
Checksum:              301


Coasting Arc #14 (Orbit 279)
---------------------------------------

Vector Time (GMT): 2018/195/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944252
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4700487
09                 A    =         6779467
32  meter
 Y    =        -332256
49  meter          E    =           
0008608
 Z    =       -4881739
39                 I    =           51
29114
 XDOT =      -1903
883290                 Wp   =           94
54518
 YDOT =      -7050
595346  meter/sec      RA   =          240
16623  deg
 ZDOT =       2315
935705                 TA   =          198
23055
                                          MA   =          198
26142
                                          Ha   =            220
492  n
mi
                                          Hp   =            215
772

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15421545
59                 X    =        -4672710
00
 Y    =       -1090080
34  feet           Y    =         -384664
69  meter
 Z    =      -16016205
35                 Z    =        -4904504
78
 XDOT =      -6246
336252                 XDOT =       -1836
149429
 YDOT =     -23131
874494  feet/sec       YDOT =       -7071
507433  meter/sec
 ZDOT =       7598
214254                 ZDOT =        2306
851187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13725734
26                 X    =         4183603
80
 Y    =       -6880675
94  feet           Y    =        -2097230
03  meter
 Z    =      -16118054
94                 Z    =        -4912783
14
 XDOT =      16722
060715                 XDOT =        5096
884106
 YDOT =      15673
742124  feet/sec       YDOT =        4777
356599  meter/sec
 ZDOT =       7558
444295                 ZDOT =        2303
813821


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18195
78705660  
00016717  00000-0  10270-3 0  9134
2 25544  51
6374 241
1489 0004147 313
2380  46
8426 15
54005332  2801


Satellite: ISS
Catalog Number: 25544
Epoch time:      18195
78705660   =   yrday
fracday
Element set:     913
Inclination:       51
6374  deg
RA of node:       241
1489  deg
Eccentricity:     
0004147     
Arg of perigee:   313
2380  deg
Mean anomaly:      46
8426  deg
Mean motion:   15
54005332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             280
Checksum:              299


Coasting Arc #15 (Orbit 295)
---------------------------------------

Vector Time (GMT): 2018/196/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929538
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5168146
63                 A    =         6782774
85  meter
 Y    =        1834268
50  meter          E    =           
0009451
 Z    =        3988659
71                 I    =           51
31962
 XDOT =        720
873331                 Wp   =           55
94876
 YDOT =       6543
678057  meter/sec      RA   =          235
15243  deg
 ZDOT =      -3931
383911                 TA   =           75
15849
                                          MA   =           75
05383
                                          Ha   =            220
610  n
mi
                                          Hp   =            215
764

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16955861
63                 X    =         5127876
87
 Y    =        6017941
29  feet           Y    =         1891836
77  meter
 Z    =       13086153
90                 Z    =         4013666
56
 XDOT =       2365
069983                 XDOT =         666
742698
 YDOT =      21468
760029  feet/sec       YDOT =        6551
437050  meter/sec
 ZDOT =     -12898
241178                 ZDOT =       -3928
013122

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17515774
00                 X    =        -5338807
91
 Y    =        3738766
02  feet           Y    =         1139575
88  meter
 Z    =       13197862
51                 Z    =         4022708
49
 XDOT =     -13088
926249                 XDOT =       -3989
504721
 YDOT =     -15703
250945  feet/sec       YDOT =       -4786
350888  meter/sec
 ZDOT =     -12883
959443                 ZDOT =       -3927
030838


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18196
81596519  
00016717  00000-0  10270-3 0  9141
2 25544  51
6372 236
0205 0004211 318
8230  41
2604 15
54023277  2967


Satellite: ISS
Catalog Number: 25544
Epoch time:      18196
81596519   =   yrday
fracday
Element set:     914
Inclination:       51
6372  deg
RA of node:       236
0205  deg
Eccentricity:     
0004211     
Arg of perigee:   318
8230  deg
Mean anomaly:      41
2604  deg
Mean motion:   15
54023277  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             296
Checksum:              292


Coasting Arc #16 (Orbit 307)
---------------------------------------

Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929538
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -682317
50                 A    =         6783845
74  meter
 Y    =       -5626087
83  meter          E    =           
0009527
 Z    =        3718773
12                 I    =           51
33747
 XDOT =       6027
684283                 Wp   =           78
43394
 YDOT =       2089
862559  meter/sec      RA   =          231
41720  deg
 ZDOT =       4260
278061                 TA   =          326
20179
                                          MA   =          326
26248
                                          Ha   =            220
798  n
mi
                                          Hp   =            215
659

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2238574
47                 X    =         -637417
78
 Y    =      -18458293
40  feet           Y    =        -5633467
19  meter
 Z    =       12200699
23                 Z    =         3715567
38
 XDOT =      19775
867069                 XDOT =        5983
173132
 YDOT =       6856
504459  feet/sec       YDOT =        2157
019104  meter/sec
 ZDOT =      13977
290226                 ZDOT =        4289
449887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13858175
19                 X    =        -4223971
80
 Y    =       12409840
31  feet           Y    =         3782519
33  meter
 Z    =       12187030
66                 Z    =         3714606
94
 XDOT =      -4655
602219                 XDOT =       -1419
027556
 YDOT =     -19077
167200  feet/sec       YDOT =       -5814
720563  meter/sec
 ZDOT =      14107
623436                 ZDOT =        4300
003623


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18197
58764615  
00016717  00000-0  10270-3 0  9151
2 25544  51
6372 232
1734 0003868 323
3031  36
7856 15
54000692  3086


Satellite: ISS
Catalog Number: 25544
Epoch time:      18197
58764615   =   yrday
fracday
Element set:     915
Inclination:       51
6372  deg
RA of node:       232
1734  deg
Eccentricity:     
0003868     
Arg of perigee:   323
3031  deg
Mean anomaly:      36
7856  deg
Mean motion:   15
54000692  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             308
Checksum:              311
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