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

 
Date: November 14th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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


319/09:49:38 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 5

320/05:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 213 5

320/18:14:08 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 3

322/09:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 213 1

322/19:30:01 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 213 2

325/21:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 213 1

331/13:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 9

Coasting Arc #1 (Orbit 2188)
---------------------------------------

Vector Time (GMT): 2018/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6653409
74                 A    =         6789165
94  meter
 Y    =        -250016
80  meter          E    =           
0018939
 Z    =        1277317
72                 I    =           51
58923
 XDOT =       -945
993776                 Wp   =           55
38890
 YDOT =       4893
241323  meter/sec      RA   =          349
09863  deg
 ZDOT =       5834
347714                 TA   =          318
52399
                                          MA   =          318
66758
                                          Ha   =            222
936  n
mi
                                          Hp   =            213
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21828772
11                 X    =         6649506
39
 Y    =        -820265
08  feet           Y    =         -175635
62  meter
 Z    =        4190674
94                 Z    =         1309628
61
 XDOT =      -3103
654120                 XDOT =       -1028
981608
 YDOT =      16053
941347  feet/sec       YDOT =        4882
198323  meter/sec
 ZDOT =      19141
560742                 ZDOT =        5829
550969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12571047
44                 X    =        -3831655
26
 Y    =       17829686
92  feet           Y    =         5434488
57  meter
 Z    =        4336002
03                 Z    =         1321613
42
 XDOT =      -9504
838048                 XDOT =       -2897
074637
 YDOT =     -11390
463387  feet/sec       YDOT =       -3471
813240  meter/sec
 ZDOT =      19119
280440                 ZDOT =        5827
556678


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   18318
56174389  
00016717  00000-0  10270-3 0  9001
2 25544  51
6407 349
3636 0005250  46
1974 313
9612 15
53932334 21895


Satellite: ISS
Catalog Number: 25544
Epoch time:      18318
56174389   =   yrday
fracday
Element set:     900
Inclination:       51
6407  deg
RA of node:       349
3636  deg
Eccentricity:     
0005250     
Arg of perigee:    46
1974  deg
Mean anomaly:     313
9612  deg
Mean motion:   15
53932334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2189
Checksum:              320


Coasting Arc #2 (Orbit 2202)
---------------------------------------

Vector Time (GMT): 2018/319/09:49:38
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3754994
83                 A    =         6779792
62  meter
 Y    =        2932559
55  meter          E    =           
0009762
 Z    =        4815099
47                 I    =           51
52960
 XDOT =      -6185
776680                 Wp   =           91
41150
 YDOT =       3781
673884  meter/sec      RA   =          344
56743  deg
 ZDOT =       2516
084069                 TA   =          333
80775
                                          MA   =          333
85710
                                          Ha   =            222
672  n
mi
                                          Hp   =            213
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12319536
85                 X    =         3698533
55
 Y    =        9621258
35  feet           Y    =         2974234
67  meter
 Z    =       15797570
44                 Z    =         4833203
11
 XDOT =     -20294
542914                 XDOT =       -6239
826633
 YDOT =      12407
066549  feet/sec       YDOT =        3712
197949  meter/sec
 ZDOT =       8254
868992                 ZDOT =        2485
904165

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14848325
70                 X    =        -4525769
67
 Y    =       -4615382
59  feet           Y    =        -1406768
61  meter
 Z    =       15878548
42                 Z    =         4839781
56
 XDOT =      14226
106562                 XDOT =        4336
117280
 YDOT =     -17784
235469  feet/sec       YDOT =       -5420
634971  meter/sec
 ZDOT =       8118
620620                 ZDOT =        2474
555565


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   18319
46206342  
00016717  00000-0  10270-3 0  9017
2 25544  51
6412 344
8759 0004853  48
4502 311
7066 15
53983942 22034


Satellite: ISS
Catalog Number: 25544
Epoch time:      18319
46206342   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:       344
8759  deg
Eccentricity:     
0004853     
Arg of perigee:    48
4502  deg
Mean anomaly:     311
7066  deg
Mean motion:   15
53983942  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2203
Checksum:              305


Coasting Arc #3 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2018/320/05:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4514259
13                 A    =         6786178
60  meter
 Y    =       -4107286
99  meter          E    =           
0009357
 Z    =       -2967872
84                 I    =           51
52412
 XDOT =       5353
339572                 Wp   =           59
01419
 YDOT =       2297
551651  meter/sec      RA   =          340
43795  deg
 ZDOT =       4979
411560                 TA   =          267
02601
                                          MA   =          267
13310
                                          Ha   =            222
907  n
mi
                                          Hp   =            213
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14810561
45                 X    =         4574268
99
 Y    =      -13475351
01  feet           Y    =        -4056469
82  meter
 Z    =       -9737115
63                 Z    =        -2945798
17
 XDOT =      17563
450041                 XDOT =        5303
062172
 YDOT =       7537
899119  feet/sec       YDOT =        2357
135207  meter/sec
 ZDOT =      16336
652099                 ZDOT =        5005
294483

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20065139
86                 X    =        -6115854
63
 Y    =        -512214
24  feet           Y    =         -156122
90  meter
 Z    =       -9637273
21                 Z    =        -2937440
87
 XDOT =      -7466
733386                 XDOT =       -2275
860336
 YDOT =     -16038
082525  feet/sec       YDOT =       -4888
407554  meter/sec
 ZDOT =      16452
696886                 ZDOT =        5014
782011


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   18320
23376777  
00016717  00000-0  10270-3 0  9025
2 25544  51
6410 341
0279 0004853  53
0215 307
1381 15
53952722 22155


Satellite: ISS
Catalog Number: 25544
Epoch time:      18320
23376777   =   yrday
fracday
Element set:     902
Inclination:       51
6410  deg
RA of node:       341
0279  deg
Eccentricity:     
0004853     
Arg of perigee:    53
0215  deg
Mean anomaly:     307
1381  deg
Mean motion:   15
53952722  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              284


Coasting Arc #4 (Orbit 2223)
---------------------------------------

Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4137892
71                 A    =         6779855
28  meter
 Y    =        2424560
94  meter          E    =           
0010294
 Z    =        4783491
43                 I    =           51
48646
 XDOT =      -5639
982255                 Wp   =           91
90338
 YDOT =       4518
393593  meter/sec      RA   =          337
82922  deg
 ZDOT =       2583
448982                 TA   =          332
58854
                                          MA   =          332
64281
                                          Ha   =            222
730  n
mi
                                          Hp   =            213
335

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13575763
48                 X    =         4087237
06
 Y    =        7954596
24  feet           Y    =         2470550
44  meter
 Z    =       15693869
52                 Z    =         4803469
14
 XDOT =     -18503
878788                 XDOT =       -5702
638219
 YDOT =      14824
125961  feet/sec       YDOT =        4454
973034  meter/sec
 ZDOT =       8475
882487                 ZDOT =        2555
899402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7309795
70                 X    =         2228025
73
 Y    =       13832116
69  feet           Y    =         4216029
17  meter
 Z    =       15783343
46                 Z    =         4810763
09
 XDOT =     -22566
245023                 XDOT =       -6878
191483
 YDOT =       2376
868698  feet/sec       YDOT =         724
469579  meter/sec
 ZDOT =       8351
371465                 ZDOT =        2545
498023


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   18320
81254295  
00016717  00000-0  10270-3 0  9030
2 25544  51
6402 338
1475 0005049  51
6763 308
4843 15
54003120 22248


Satellite: ISS
Catalog Number: 25544
Epoch time:      18320
81254295   =   yrday
fracday
Element set:     903
Inclination:       51
6402  deg
RA of node:       338
1475  deg
Eccentricity:     
0005049     
Arg of perigee:    51
6763  deg
Mean anomaly:     308
4843  deg
Mean motion:   15
54003120  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2224
Checksum:              282


Coasting Arc #5 (Orbit 2238)
---------------------------------------

Vector Time (GMT): 2018/321/18:14:08
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2698846
73                 A    =         6777937
81  meter
 Y    =       -3331554
89  meter          E    =           
0019268
 Z    =       -5266264
26                 I    =           51
45020
 XDOT =       6470
187764                 Wp   =           76
25027
 YDOT =      -4015
207837  meter/sec      RA   =          332
82104  deg
 ZDOT =       -773
627713                 TA   =          186
31184
                                          MA   =          186
33615
                                          Ha   =            222
939  n
mi
                                          Hp   =            213
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8854484
04                 X    =        -2635810
64
 Y    =      -10930298
20  feet           Y    =        -3361382
81  meter
 Z    =      -17277769
88                 Z    =        -5279221
42
 XDOT =      21227
650144                 XDOT =        6518
363994
 YDOT =     -13173
254059  feet/sec       YDOT =       -3942
584331  meter/sec
 ZDOT =      -2538
148665                 ZDOT =        -742
080282

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1959052
65                 X    =         -597119
25
 Y    =      -13857687
03  feet           Y    =        -4223823
01  meter
 Z    =      -17335549
06                 Z    =        -5283875
35
 XDOT =      23980
922806                 XDOT =        7309
385271
 YDOT =       -384
589051  feet/sec       YDOT =        -117
222743  meter/sec
 ZDOT =      -2395
749329                 ZDOT =        -730
224395


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   18321
77716846  
00016717  00000-0  10270-3 0  9042
2 25544  51
6410 333
3398 0005182  54
7190 305
4446 15
53991360 22397


Satellite: ISS
Catalog Number: 25544
Epoch time:      18321
77716846   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:       333
3398  deg
Eccentricity:     
0005182     
Arg of perigee:    54
7190  deg
Mean anomaly:     305
4446  deg
Mean motion:   15
53991360  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2239
Checksum:              313


Coasting Arc #6 (Orbit 2248)
---------------------------------------

Vector Time (GMT): 2018/322/09:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917504
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4600962
10                 A    =         6780270
14  meter
 Y    =       -1657978
09  meter          E    =           
0016021
 Z    =       -4711824
57                 I    =           51
43916
 XDOT =       4747
919316                 Wp   =           67
01570
 YDOT =      -5332
297596  meter/sec      RA   =          329
63916  deg
 ZDOT =      -2761
282686                 TA   =          175
52056
                                          MA   =          175
50621
                                          Ha   =            222
974  n
mi
                                          Hp   =            213
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15095020
02                 X    =        -4559192
21
 Y    =       -5439560
67  feet           Y    =        -1709195
71  meter
 Z    =      -15458742
03                 Z    =        -4734073
38
 XDOT =      15577
163109                 XDOT =        4820
606770
 YDOT =     -17494
414686  feet/sec       YDOT =       -5278
796651  meter/sec
 ZDOT =      -9059
326399                 ZDOT =       -2738
041973

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15948230
97                 X    =         4861020
80
 Y    =         -85305
03  feet           Y    =          -26000
97  meter
 Z    =      -15558528
43                 Z    =        -4742239
46
 XDOT =      -8620
372087                 XDOT =       -2627
489412
 YDOT =      20663
501196  feet/sec       YDOT =        6298
235164  meter/sec
 ZDOT =      -8954
093389                 ZDOT =       -2729
207665


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   18322
42024845  
00016717  00000-0  10270-3 0  9057
2 25544  51
6409 330
1335 0005088  59
7315 300
4340 15
53976072 22492


Satellite: ISS
Catalog Number: 25544
Epoch time:      18322
42024845   =   yrday
fracday
Element set:     905
Inclination:       51
6409  deg
RA of node:       330
1335  deg
Eccentricity:     
0005088     
Arg of perigee:    59
7315  deg
Mean anomaly:     300
4340  deg
Mean motion:   15
53976072  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2249
Checksum:              293


Coasting Arc #7 (Orbit 2255)
---------------------------------------

Vector Time (GMT): 2018/322/19:30:01
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5970593
78                 A    =         6785636
20  meter
 Y    =        -882982
31  meter          E    =           
0017770
 Z    =        3081284
98                 I    =           51
44645
 XDOT =      -1688
291634                 Wp   =           76
89826
 YDOT =       5678
498726  meter/sec      RA   =          327
57929  deg
 ZDOT =       4878
856716                 TA   =          318
65320
                                          MA   =          318
78759
                                          Ha   =            222
912  n
mi
                                          Hp   =            213
191

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19588562
28                 X    =         5965056
25
 Y    =       -2896923
60  feet           Y    =         -816245
94  meter
 Z    =       10109202
69                 Z    =         3110275
15
 XDOT =      -5539
014548                 XDOT =       -1775
364075
 YDOT =      18630
245164  feet/sec       YDOT =        5659
132240  meter/sec
 ZDOT =      16006
747757                 ZDOT =        4870
443919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19720626
79                 X    =         6010847
05
 Y    =         739164
49  feet           Y    =          225297
34  meter
 Z    =       10239650
01                 Z    =         3121045
32
 XDOT =      -8918
179791                 XDOT =       -2718
261200
 YDOT =      15839
197786  feet/sec       YDOT =        4827
787485  meter/sec
 ZDOT =      15968
128971                 ZDOT =        4867
085710


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   18322
87040472  
00016717  00000-0  10270-3 0  9061
2 25544  51
6420 327
8915 0005238  57
9730 302
1931 15
53977839 22565


Satellite: ISS
Catalog Number: 25544
Epoch time:      18322
87040472   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:       327
8915  deg
Eccentricity:     
0005238     
Arg of perigee:    57
9730  deg
Mean anomaly:     302
1931  deg
Mean motion:   15
53977839  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2256
Checksum:              320


Coasting Arc #8 (Orbit 2270)
---------------------------------------

Vector Time (GMT): 2018/323/19:30:01
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5261558
45                 A    =         6781817
31  meter
 Y    =        -279667
81  meter          E    =           
0013620
 Z    =       -4284091
63                 I    =           51
40586
 XDOT =       3193
243621                 Wp   =           65
84752
 YDOT =      -5994
407024  meter/sec      RA   =          322
58125  deg
 ZDOT =      -3533
951484                 TA   =          167
97169
                                          MA   =          167
93913
                                          Ha   =            222
958  n
mi
                                          Hp   =            213
040

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17262330
89                 X    =        -5237229
76
 Y    =        -917545
31  feet           Y    =         -338370
17  meter
 Z    =      -14055418
75                 Z    =        -4309591
94
 XDOT =      10476
521066                 XDOT =        3277
203880
 YDOT =     -19666
689710  feet/sec       YDOT =       -5958
228491  meter/sec
 ZDOT =     -11594
329016                 ZDOT =       -3518
235559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16774724
44                 X    =        -5112936
01
 Y    =       -3768857
21  feet           Y    =        -1148747
68  meter
 Z    =      -14170006
66                 Z    =        -4319018
03
 XDOT =      13410
804350                 XDOT =        4087
613166
 YDOT =     -16408
900342  feet/sec       YDOT =       -5001
432824  meter/sec
 ZDOT =     -11522
845701                 ZDOT =       -3512
163370


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   18323
83502115  
00016717  00000-0  10270-3 0  9076
2 25544  51
6414 323
0846 0005135  60
7492 299
4174 15
53999467 22717


Satellite: ISS
Catalog Number: 25544
Epoch time:      18323
83502115   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:       323
0846  deg
Eccentricity:     
0005135     
Arg of perigee:    60
7492  deg
Mean anomaly:     299
4174  deg
Mean motion:   15
53999467  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2271
Checksum:              317


Coasting Arc #9 (Orbit 2286)
---------------------------------------

Vector Time (GMT): 2018/324/19:30:01
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4267930
72                 A    =         6778847
60  meter
 Y    =        1542538
07  meter          E    =           
0009253
 Z    =        5027953
41                 I    =           51
37027
 XDOT =      -4378
050487                 Wp   =           95
62846
 YDOT =       6021
140691  meter/sec      RA   =          317
57109  deg
 ZDOT =       1865
172998                 TA   =          336
22465
                                          MA   =          336
26737
                                          Ha   =            222
872  n
mi
                                          Hp   =            213
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14002397
37                 X    =         4225940
66
 Y    =        5060820
44  feet           Y    =         1590030
16  meter
 Z    =       16495910
15                 Z    =         5048584
11
 XDOT =     -14363
682699                 XDOT =       -4454
115433
 YDOT =      19754
398593  feet/sec       YDOT =        5971
756946  meter/sec
 ZDOT =       6119
333983                 ZDOT =        1843
720774

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12977293
97                 X    =         3955479
20
 Y    =        7085759
16  feet           Y    =         2159739
39  meter
 Z    =       16588428
07                 Z    =         5056152
88
 XDOT =     -16683
861275                 XDOT =       -5085
240917
 YDOT =      16428
178551  feet/sec       YDOT =        5007
308822  meter/sec
 ZDOT =       6022
072139                 ZDOT =        1835
527588


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   18324
86394391  
00016717  00000-0  10270-3 0  9086
2 25544  51
6414 317
9562 0005143  65
5009 294
6680 15
53994862 22870


Satellite: ISS
Catalog Number: 25544
Epoch time:      18324
86394391   =   yrday
fracday
Element set:     908
Inclination:       51
6414  deg
RA of node:       317
9562  deg
Eccentricity:     
0005143     
Arg of perigee:    65
5009  deg
Mean anomaly:     294
6680  deg
Mean motion:   15
53994862  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2287
Checksum:              340


Coasting Arc #10 (Orbit 2301)
---------------------------------------

Vector Time (GMT): 2018/325/19:30:01
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3124700
68                 A    =         6777673
34  meter
 Y    =       -2868973
09  meter          E    =           
0019657
 Z    =       -5303008
86                 I    =           51
34272
 XDOT =       5176
932095                 Wp   =           84
08159
 YDOT =      -5637
435805  meter/sec      RA   =          312
55281  deg
 ZDOT =          1
480060                 TA   =          185
92096
                                          MA   =          185
94423
                                          Ha   =            222
957  n
mi
                                          Hp   =            212
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10251642
64                 X    =        -3066626
86
 Y    =       -9412641
36  feet           Y    =        -2903590
72  meter
 Z    =      -17398323
02                 Z    =        -5318047
05
 XDOT =      16984
685350                 XDOT =        5239
579524
 YDOT =     -18495
524294  feet/sec       YDOT =       -5579
193470  meter/sec
 ZDOT =          4
855840                 ZDOT =          26
780410

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8796094
89                 X    =        -2681049
72
 Y    =      -10676142
46  feet           Y    =        -3254088
22  meter
 Z    =      -17465518
46                 Z    =        -5323490
03
 XDOT =      18510
776473                 XDOT =        5642
084669
 YDOT =     -15435
671238  feet/sec       YDOT =       -4704
792593  meter/sec
 ZDOT =        119
352309                 ZDOT =          36
378584


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   18325
82855421  
00016717  00000-0  10270-3 0  9090
2 25544  51
6415 313
1480 0005093  67
1279 293
0411 15
54021372 23020


Satellite: ISS
Catalog Number: 25544
Epoch time:      18325
82855421   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:       313
1480  deg
Eccentricity:     
0005093     
Arg of perigee:    67
1279  deg
Mean anomaly:     293
0411  deg
Mean motion:   15
54021372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2302
Checksum:              284


Coasting Arc #11 (Orbit 2303)
---------------------------------------

Vector Time (GMT): 2018/325/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4222118
90                 A    =         6778582
91  meter
 Y    =        1416279
16  meter          E    =           
0008719
 Z    =        5103138
62                 I    =           51
34112
 XDOT =      -4030
866212                 Wp   =           95
27644
 YDOT =       6338
596831  meter/sec      RA   =          312
09505  deg
 ZDOT =       1572
700472                 TA   =          339
49197
                                          MA   =          339
52695
                                          Ha   =            222
910  n
mi
                                          Hp   =            213
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13852096
13                 X    =         4181178
84
 Y    =        4646585
16  feet           Y    =         1463264
68  meter
 Z    =       16742580
78                 Z    =         5123549
40
 XDOT =     -13224
626680                 XDOT =       -4109
086147
 YDOT =      20795
921361  feet/sec       YDOT =        6293
083458  meter/sec
 ZDOT =       5159
778453                 ZDOT =        1552
929684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14380310
08                 X    =         4383118
51
 Y    =       -1898486
46  feet           Y    =         -578658
67  meter
 Z    =       16834124
96                 Z    =         5131041
29
 XDOT =      -2849
170761                 XDOT =        -868
427248
 YDOT =      23465
266235  feet/sec       YDOT =        7152
213149  meter/sec
 ZDOT =       5070
039369                 ZDOT =        1545
348000


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   18325
95716927  
00016717  00000-0  10270-3 0  9103
2 25544  51
6393 312
5051 0005119  68
2419 291
9278 15
53974234 23042


Satellite: ISS
Catalog Number: 25544
Epoch time:      18325
95716927   =   yrday
fracday
Element set:     910
Inclination:       51
6393  deg
RA of node:       312
5051  deg
Eccentricity:     
0005119     
Arg of perigee:    68
2419  deg
Mean anomaly:     291
9278  deg
Mean motion:   15
53974234  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2304
Checksum:              319


Coasting Arc #12 (Orbit 2318)
---------------------------------------

Vector Time (GMT): 2018/326/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3172781
99                 A    =         6777739
14  meter
 Y    =       -2832635
82  meter          E    =           
0019702
 Z    =       -5294116
41                 I    =           51
31527
 XDOT =       4803
917200                 Wp   =           87
22626
 YDOT =      -5950
496590  meter/sec      RA   =          307
07388  deg
 ZDOT =        306
757285                 TA   =          185
70561
                                          MA   =          185
72808
                                          Ha   =            223
012  n
mi
                                          Hp   =            212
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10409389
73                 X    =        -3115154
13
 Y    =       -9293424
62  feet           Y    =        -2867793
49  meter
 Z    =      -17369148
34                 Z    =        -5309389
34
 XDOT =      15760
883202                 XDOT =        4868
610170
 YDOT =     -19522
626606  feet/sec       YDOT =       -5896
414151  meter/sec
 ZDOT =       1006
421538                 ZDOT =         330
250402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13403473
34                 X    =        -4085378
67
 Y    =       -3562901
16  feet           Y    =        -1085972
27  meter
 Z    =      -17437404
84                 Z    =        -5314920
99
 XDOT =       4830
288312                 XDOT =        1472
271877
 YDOT =     -23586
881628  feet/sec       YDOT =       -7189
281520  meter/sec
 ZDOT =       1112
831277                 ZDOT =         339
190973


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   18326
92177594  
00016717  00000-0  10270-3 0  9113
2 25544  51
6375 307
6961 0005122  72
6732 287
4980 15
54012078 23194


Satellite: ISS
Catalog Number: 25544
Epoch time:      18326
92177594   =   yrday
fracday
Element set:     911
Inclination:       51
6375  deg
RA of node:       307
6961  deg
Eccentricity:     
0005122     
Arg of perigee:    72
6732  deg
Mean anomaly:     287
4980  deg
Mean motion:   15
54012078  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2319
Checksum:              321


Coasting Arc #13 (Orbit 2334)
---------------------------------------

Vector Time (GMT): 2018/327/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2045298
49                 A    =         6779317
60  meter
 Y    =        4173029
34  meter          E    =           
0011203
 Z    =        4928460
01                 I    =           51
30190
 XDOT =      -5266
316989                 Wp   =           65
55959
 YDOT =       5145
544670  meter/sec      RA   =          302
05354  deg
 ZDOT =      -2162
886868                 TA   =           45
65631
                                          MA   =           45
56455
                                          Ha   =            222
919  n
mi
                                          Hp   =            213
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6710296
88                 X    =         1974542
05
 Y    =       13691041
14  feet           Y    =         4195505
21  meter
 Z    =       16169488
22                 Z    =         4938224
13
 XDOT =     -17277
942878                 XDOT =       -5312
958078
 YDOT =      16881
708234  feet/sec       YDOT =        5086
392468  meter/sec
 ZDOT =      -7096
085525                 ZDOT =       -2188
582260

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12286026
71                 X    =         3744780
94
 Y    =        8951175
72  feet           Y    =         2728318
36  meter
 Z    =       16212804
88                 Z    =         4941662
93
 XDOT =      -6562
923157                 XDOT =       -2000
378978
 YDOT =      22121
282236  feet/sec       YDOT =        6742
566825  meter/sec
 ZDOT =      -7212
278931                 ZDOT =       -2198
302618


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   18327
95068785  
00016717  00000-0  10270-3 0  9129
2 25544  51
6380 302
5679 0004954  76
5539 283
6166 15
54002088 23352


Satellite: ISS
Catalog Number: 25544
Epoch time:      18327
95068785   =   yrday
fracday
Element set:     912
Inclination:       51
6380  deg
RA of node:       302
5679  deg
Eccentricity:     
0004954     
Arg of perigee:    76
5539  deg
Mean anomaly:     283
6166  deg
Mean motion:   15
54002088  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2335
Checksum:              335


Coasting Arc #14 (Orbit 2349)
---------------------------------------

Vector Time (GMT): 2018/328/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -975856
88                 A    =         6782494
80  meter
 Y    =       -5320586
51  meter          E    =           
0012164
 Z    =       -4103218
17                 I    =           51
29581
 XDOT =       5395
141744                 Wp   =           97
42598
 YDOT =      -3901
469779  meter/sec      RA   =          297
03733  deg
 ZDOT =       3784
006210                 TA   =          211
82132
                                          MA   =          211
89487
                                          Ha   =            223
008  n
mi
                                          Hp   =            212
949

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3201630
18                 X    =         -896356
39
 Y    =      -17455992
50  feet           Y    =        -5331054
27  meter
 Z    =      -13462001
87                 Z    =        -4107766
12
 XDOT =      17700
596274                 XDOT =        5419
987011
 YDOT =     -12800
097701  feet/sec       YDOT =       -3840
999046  meter/sec
 ZDOT =      12414
718538                 ZDOT =        3810
274401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11224931
40                 X    =        -3421359
09
 Y    =      -13727039
97  feet           Y    =        -4184001
78  meter
 Z    =      -13481724
41                 Z    =        -4109229
60
 XDOT =       8145
136501                 XDOT =        2482
637605
 YDOT =     -18943
630991  feet/sec       YDOT =       -5774
018726  meter/sec
 ZDOT =      12533
315039                 ZDOT =        3820
154424


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   18328
91528938  
00016717  00000-0  10270-3 0  9138
2 25544  51
6379 297
7588 0005085  81
0202 279
1526 15
54021174 23502


Satellite: ISS
Catalog Number: 25544
Epoch time:      18328
91528938   =   yrday
fracday
Element set:     913
Inclination:       51
6379  deg
RA of node:       297
7588  deg
Eccentricity:     
0005085     
Arg of perigee:    81
0202  deg
Mean anomaly:     279
1526  deg
Mean motion:   15
54021174  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2350
Checksum:              324


Coasting Arc #15 (Orbit 2365)
---------------------------------------

Vector Time (GMT): 2018/329/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -51283
28                 A    =         6786200
56  meter
 Y    =        6161736
41  meter          E    =           
0018188
 Z    =        2825077
05                 I    =           51
29424
 XDOT =      -5297
181325                 Wp   =           95
09865
 YDOT =       2286
848007  meter/sec      RA   =          292
03101  deg
 ZDOT =      -5057
393588                 TA   =           52
62158
                                          MA   =           52
45610
                                          Ha   =            222
930  n
mi
                                          Hp   =            212
991

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -168252
23                 X    =         -133904
66
 Y    =       20215670
64  feet           Y    =         6160700
64  meter
 Z    =        9268625
48                 Z    =         2824627
95
 XDOT =     -17379
203821                 XDOT =       -5297
793288
 YDOT =       7502
782176  feet/sec       YDOT =        2227
608399  meter/sec
 ZDOT =     -16592
498649                 ZDOT =       -5083
127069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9955697
92                 X    =         3034496
73
 Y    =       17596544
79  feet           Y    =         5363426
85  meter
 Z    =        9265784
20                 Z    =         2824211
02
 XDOT =      -9880
677442                 XDOT =       -3011
630484
 YDOT =      14434
331818  feet/sec       YDOT =        4399
584338  meter/sec
 ZDOT =     -16708
474512                 ZDOT =       -5092
743031


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   18329
94419204  
00016717  00000-0  10270-3 0  9148
2 25544  51
6379 292
6303 0004958  83
4271 276
7446 15
54042169 23669


Satellite: ISS
Catalog Number: 25544
Epoch time:      18329
94419204   =   yrday
fracday
Element set:     914
Inclination:       51
6379  deg
RA of node:       292
6303  deg
Eccentricity:     
0004958     
Arg of perigee:    83
4271  deg
Mean anomaly:     276
7446  deg
Mean motion:   15
54042169  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2366
Checksum:              331


Coasting Arc #16 (Orbit 2380)
---------------------------------------

Vector Time (GMT): 2018/330/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         921447
08                 A    =         6788904
77  meter
 Y    =       -6594137
10  meter          E    =           
0012751
 Z    =       -1310847
89                 I    =           51
29100
 XDOT =       4995
548404                 Wp   =           56
25105
 YDOT =       -444
920846  meter/sec      RA   =          287
03286  deg
 ZDOT =       5797
417366                 TA   =          289
41654
                                          MA   =          289
55430
                                          Ha   =            223
057  n
mi
                                          Hp   =            212
918

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3023120
35                 X    =         1001483
55
 Y    =      -21634308
06  feet           Y    =        -6583385
18  meter
 Z    =       -4300682
05                 Z    =        -1306178
09
 XDOT =      16389
594501                 XDOT =        4971
991295
 YDOT =      -1459
714061  feet/sec       YDOT =        -389
189496  meter/sec
 ZDOT =      19020
398181                 ZDOT =        5821
626974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8575103
56                 X    =        -2613691
56
 Y    =      -20095712
68  feet           Y    =        -6125173
23  meter
 Z    =       -4278824
48                 Z    =        -1304185
70
 XDOT =      11700
067461                 XDOT =        3566
180562
 YDOT =      -9032
128992  feet/sec       YDOT =       -2752
992917  meter/sec
 ZDOT =      19129
282832                 ZDOT =        5830
605407


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   18330
90878851  
00016717  00000-0  10270-3 0  9154
2 25544  51
6371 287
8227 0005188  89
5941 270
5806 15
54024502 23819


Satellite: ISS
Catalog Number: 25544
Epoch time:      18330
90878851   =   yrday
fracday
Element set:     915
Inclination:       51
6371  deg
RA of node:       287
8227  deg
Eccentricity:     
0005188     
Arg of perigee:    89
5941  deg
Mean anomaly:     270
5806  deg
Mean motion:   15
54024502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2381
Checksum:              327


Coasting Arc #17 (Orbit 2391)
---------------------------------------

Vector Time (GMT): 2018/331/13:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1705585
34                 A    =         6789598
89  meter
 Y    =       -6564661
57  meter          E    =           
0016538
 Z    =         110708
72                 I    =           51
28953
 XDOT =       4615
314476                 Wp   =           58
46300
 YDOT =       1311
028328  meter/sec      RA   =          283
81464  deg
 ZDOT =       5982
720291                 TA   =          302
73542
                                          MA   =          302
89473
                                          Ha   =            223
018  n
mi
                                          Hp   =            212
918

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5595752
41                 X    =         1778328
69
 Y    =      -21537603
59  feet           Y    =        -6545181
81  meter
 Z    =         363217
58                 Z    =          119169
95
 XDOT =      15142
107862                 XDOT =        4571
250081
 YDOT =       4301
274043  feet/sec       YDOT =        1362
393011  meter/sec
 ZDOT =      19628
347412                 ZDOT =        6005
033144

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20872080
83                 X    =         6361810
24
 Y    =        7714097
09  feet           Y    =         2351256
79  meter
 Z    =         402105
03                 Z    =          122561
61
 XDOT =      -5216
402026                 XDOT =       -1589
959338
 YDOT =      12984
793249  feet/sec       YDOT =        3957
764982  meter/sec
 ZDOT =      19728
480481                 ZDOT =        6013
240850


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   18331
61615638  
00016717  00000-0  10270-3 0  9166
2 25544  51
6392 284
3007 0005135  88
4995 271
6746 15
54034247 23923


Satellite: ISS
Catalog Number: 25544
Epoch time:      18331
61615638   =   yrday
fracday
Element set:     916
Inclination:       51
6392  deg
RA of node:       284
3007  deg
Eccentricity:     
0005135     
Arg of perigee:    88
4995  deg
Mean anomaly:     271
6746  deg
Mean motion:   15
54034247  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2392
Checksum:              323


Coasting Arc #18 (Orbit 2406)
---------------------------------------

Vector Time (GMT): 2018/332/13:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2399006
34                 A    =         6788196
73  meter
 Y    =        6090384
85  meter          E    =           
0011322
 Z    =       -1792174
57                 I    =           51
27900
 XDOT =      -4063
348907                 Wp   =          120
60741
 YDOT =      -3247
517686  meter/sec      RA   =          278
81922  deg
 ZDOT =      -5629
174851                 TA   =           79
17589
                                          MA   =           79
04849
                                          Ha   =            223
005  n
mi
                                          Hp   =            212
890

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7870755
70                 X    =        -2458226
95
 Y    =       19981577
60  feet           Y    =         6063226
51  meter
 Z    =       -5879837
83                 Z    =        -1803971
52
 XDOT =     -13331
197201                 XDOT =       -3999
388587
 YDOT =     -10654
585584  feet/sec       YDOT =       -3292
598812  meter/sec
 ZDOT =     -18468
421427                 ZDOT =       -5648
758179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19265607
38                 X    =        -5872157
13
 Y    =       -9455842
94  feet           Y    =        -2882140
93  meter
 Z    =       -5933644
60                 Z    =        -1808574
88
 XDOT =      11021
479194                 XDOT =        3359
346858
 YDOT =     -10877
189956  feet/sec       YDOT =       -3315
367498  meter/sec
 ZDOT =     -18556
045931                 ZDOT =       -5655
882800


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   18332
58074454  
00016717  00000-0  10270-3 0  9179
2 25544  51
6401 279
4925 0005161  90
5998 269
5746 15
54039239 24073


Satellite: ISS
Catalog Number: 25544
Epoch time:      18332
58074454   =   yrday
fracday
Element set:     917
Inclination:       51
6401  deg
RA of node:       279
4925  deg
Eccentricity:     
0005161     
Arg of perigee:    90
5998  deg
Mean anomaly:     269
5746  deg
Mean motion:   15
54039239  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2407
Checksum:              336
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