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

 
Date: July 28th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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


209/20:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 215 1

212/23:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 214 7

215/16:42:42 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 214 5

216/02:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 214 4

222/19:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 213 6

Coasting Arc #1 (Orbit 476)
---------------------------------------

Vector Time (GMT): 2018/208/09:58:42
767
Vector Time (MET): N/A
Weight (LBS)     : 944329
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4713817
25                 A    =         6784400
78  meter
 Y    =       -3177313
45  meter          E    =           
0012703
 Z    =        3699103
53                 I    =           51
65152
 XDOT =       5510
377018                 Wp   =           60
39564
 YDOT =       3130
456250  meter/sec      RA   =          177
00241  deg
 ZDOT =      -4315
781359                 TA   =           75
54101
                                          MA   =           75
40009
                                          Ha   =            222
116  n
mi
                                          Hp   =            215
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15465279
69                 X    =         4731028
59
 Y    =      -10424256
71  feet           Y    =        -3124504
38  meter
 Z    =       12136166
43                 Z    =         3722042
66
 XDOT =      18078
664757                 XDOT =        5495
925207
 YDOT =      10270
525754  feet/sec       YDOT =        3191
996674  meter/sec
 ZDOT =     -14159
387660                 ZDOT =       -4289
049230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11429597
32                 X    =        -3483741
26
 Y    =      -14652280
77  feet           Y    =        -4466015
18  meter
 Z    =       12239342
83                 Z    =         3730551
70
 XDOT =       7961
691224                 XDOT =        2426
723485
 YDOT =     -17985
350673  feet/sec       YDOT =       -5481
934885  meter/sec
 ZDOT =     -14039
900732                 ZDOT =       -4279
361743


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   18208
45593002  
00016717  00000-0  10270-3 0  9004
2 25544  51
6367 178
0070 0005223 353
4037   6
7045 15
53795626  4779


Satellite: ISS
Catalog Number: 25544
Epoch time:      18208
45593002   =   yrday
fracday
Element set:     900
Inclination:       51
6367  deg
RA of node:       178
0070  deg
Eccentricity:     
0005223     
Arg of perigee:   353
4037  deg
Mean anomaly:       6
7045  deg
Mean motion:   15
53795626  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             477
Checksum:              297


Coasting Arc #2 (Orbit 491)
---------------------------------------

Vector Time (GMT): 2018/209/09:58:42
767
Vector Time (MET): N/A
Weight (LBS)     : 944329
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5721298
87                 A    =         6787794
45  meter
 Y    =        2728681
43  meter          E    =           
0009674
 Z    =       -2416631
08                 I    =           51
69617
 XDOT =      -4029
600407                 Wp   =           24
86619
 YDOT =      -3713
383099  meter/sec      RA   =          172
02775  deg
 ZDOT =       5363
443119                 TA   =          308
13571
                                          MA   =          308
22287
                                          Ha   =            222
276  n
mi
                                          Hp   =            214
948

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18770665
60                 X    =        -5739648
07
 Y    =        8952366
90  feet           Y    =         2664599
50  meter
 Z    =       -7928579
66                 Z    =        -2444466
92
 XDOT =     -13220
473777                 XDOT =       -4013
829049
 YDOT =     -12183
015418  feet/sec       YDOT =       -3758
357090  meter/sec
 ZDOT =      17596
598160                 ZDOT =        5343
907178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10493859
25                 X    =         3198528
30
 Y    =       17898670
31  feet           Y    =         5455514
71  meter
 Z    =       -8053673
37                 Z    =        -2454759
64
 XDOT =      -9711
927550                 XDOT =       -2960
195517
 YDOT =      13548
770118  feet/sec       YDOT =        4129
665132  meter/sec
 ZDOT =      17509
417658                 ZDOT =        5336
870502


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   18209
42068379  
00016717  00000-0  10270-3 0  9017
2 25544  51
6373 173
2010 0005184 359
4640    
6506 15
53776381  4928


Satellite: ISS
Catalog Number: 25544
Epoch time:      18209
42068379   =   yrday
fracday
Element set:     901
Inclination:       51
6373  deg
RA of node:       173
2010  deg
Eccentricity:     
0005184     
Arg of perigee:   359
4640  deg
Mean anomaly:        
6506  deg
Mean motion:   15
53776381  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             492
Checksum:              299


Coasting Arc #3 (Orbit 498)
---------------------------------------

Vector Time (GMT): 2018/209/20:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944329
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5443976
04                 A    =         6785021
07  meter
 Y    =        1906713
87  meter          E    =           
0007640
 Z    =       -3582515
49                 I    =           51
70030
 XDOT =      -4455
327246                 Wp   =           40
47228
 YDOT =       4360
105804  meter/sec      RA   =          169
92951  deg
 ZDOT =      -4449
385115                 TA   =          181
77189
                                          MA   =          181
77460
                                          Ha   =            222
335  n
mi
                                          Hp   =            215
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17860813
78                 X    =         5439651
62
 Y    =        6255622
92  feet           Y    =         1967568
23  meter
 Z    =      -11753659
74                 Z    =        -3556081
50
 XDOT =     -14617
215374                 XDOT =       -4482
139742
 YDOT =      14304
809067  feet/sec       YDOT =        4310
133636  meter/sec
 ZDOT =     -14597
720193                 ZDOT =       -4471
091898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11962849
85                 X    =        -3646276
64
 Y    =       14758010
89  feet           Y    =         4498241
72  meter
 Z    =      -11635348
83                 Z    =        -3546454
32
 XDOT =      -7461
544053                 XDOT =       -2274
278627
 YDOT =     -17635
306389  feet/sec       YDOT =       -5375
241387  meter/sec
 ZDOT =     -14695
518015                 ZDOT =       -4479
193891


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   18209
87090061  
00016717  00000-0  10270-3 0  9020
2 25544  51
6368 170
9562 0005363 357
3770   2
7353 15
53779676  4998


Satellite: ISS
Catalog Number: 25544
Epoch time:      18209
87090061   =   yrday
fracday
Element set:     902
Inclination:       51
6368  deg
RA of node:       170
9562  deg
Eccentricity:     
0005363     
Arg of perigee:   357
3770  deg
Mean anomaly:       2
7353  deg
Mean motion:   15
53779676  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             499
Checksum:              332


Coasting Arc #4 (Orbit 514)
---------------------------------------

Vector Time (GMT): 2018/210/20:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944329
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4259694
82                 A    =         6781605
73  meter
 Y    =       -2600419
61  meter          E    =           
0008196
 Z    =        4583789
37                 I    =           51
72091
 XDOT =       5759
670462                 Wp   =           77
02213
 YDOT =      -4045
123333  meter/sec      RA   =          164
94936  deg
 ZDOT =       3054
810409                 TA   =          342
48689
                                          MA   =          342
51514
                                          Ha   =            222
550  n
mi
                                          Hp   =            214
994

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13975376
70                 X    =        -4252564
77
 Y    =       -8531560
39  feet           Y    =        -2648014
82  meter
 Z    =       15038679
03                 Z    =         4563114
89
 XDOT =      18896
556635                 XDOT =        5789
637747
 YDOT =     -13271
402010  feet/sec       YDOT =       -3980
547310  meter/sec
 ZDOT =      10022
343862                 ZDOT =        3082
860865

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12614866
82                 X    =         3845011
41
 Y    =      -10570486
90  feet           Y    =        -3221884
41  meter
 Z    =       14946253
21                 Z    =         4555617
98
 XDOT =       5715
902910                 XDOT =        1742
207207
 YDOT =      21184
102616  feet/sec       YDOT =        6456
914477  meter/sec
 ZDOT =      10148
564056                 ZDOT =        3093
282324


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   18210
89996931  
00016717  00000-0  10270-3 0  9036
2 25544  51
6368 165
8286 0005336    
2576 359
8578 15
53753366  5154


Satellite: ISS
Catalog Number: 25544
Epoch time:      18210
89996931   =   yrday
fracday
Element set:     903
Inclination:       51
6368  deg
RA of node:       165
8286  deg
Eccentricity:     
0005336     
Arg of perigee:      
2576  deg
Mean anomaly:     359
8578  deg
Mean motion:   15
53753366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             515
Checksum:              344


Coasting Arc #5 (Orbit 529)
---------------------------------------

Vector Time (GMT): 2018/211/20:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944329
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2861074
75                 A    =         6779038
47  meter
 Y    =        3312685
10  meter          E    =           
0016039
 Z    =       -5190183
26                 I    =           51
74429
 XDOT =      -6632
006465                 Wp   =           61
45588
 YDOT =       3570
694367  meter/sec      RA   =          159
96320  deg
 ZDOT =      -1372
593960                 TA   =          195
32242
                                          MA   =          195
37104
                                          Ha   =            222
483  n
mi
                                          Hp   =            214
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9386728
19                 X    =         2849029
42
 Y    =       10868389
43  feet           Y    =         3344612
43  meter
 Z    =      -17028160
32                 Z    =        -5176314
58
 XDOT =     -21758
551395                 XDOT =       -6664
774852
 YDOT =      11714
876533  feet/sec       YDOT =        3496
347512  meter/sec
 ZDOT =      -4503
261024                 ZDOT =       -1404
888769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13254278
27                 X    =        -4039904
02
 Y    =        5714791
44  feet           Y    =         1741868
43  meter
 Z    =      -16966321
50                 Z    =        -5171334
79
 XDOT =      -4080
184391                 XDOT =       -1243
640202
 YDOT =     -23305
311461  feet/sec       YDOT =       -7103
458933  meter/sec
 ZDOT =      -4648
478363                 ZDOT =       -1416
856205


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   18211
86471823  
00016717  00000-0  10270-3 0  9043
2 25544  51
6368 161
0214 0005205   5
0539 355
0665 15
53781523  5308


Satellite: ISS
Catalog Number: 25544
Epoch time:      18211
86471823   =   yrday
fracday
Element set:     904
Inclination:       51
6368  deg
RA of node:       161
0214  deg
Eccentricity:     
0005205     
Arg of perigee:     5
0539  deg
Mean anomaly:     355
0665  deg
Mean motion:   15
53781523  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             530
Checksum:              285


Coasting Arc #6 (Orbit 545)
---------------------------------------

Vector Time (GMT): 2018/212/20:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944329
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1319472
98                 A    =         6778505
83  meter
 Y    =       -3999152
33  meter          E    =           
0006836
 Z    =        5309123
30                 I    =           51
77327
 XDOT =       7077
935299                 Wp   =           29
74504
 YDOT =      -2924
009008  meter/sec      RA   =          154
97498  deg
 ZDOT =       -437
428572                 TA   =           64
45321
                                          MA   =           64
38254
                                          Ha   =            222
660  n
mi
                                          Hp   =            214
720

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4328979
60                 X    =        -1300443
76
 Y    =      -13120578
52  feet           Y    =        -4013801
29  meter
 Z    =       17418383
52                 Z    =         5302760
01
 XDOT =      23221
572504                 XDOT =        7112
231092
 YDOT =      -9593
205407  feet/sec       YDOT =       -2844
666875  meter/sec
 ZDOT =      -1435
133111                 ZDOT =        -402
963778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13844297
10                 X    =         4219741
76
 Y    =        -451106
98  feet           Y    =         -137497
41  meter
 Z    =       17390275
16                 Z    =         5300555
87
 XDOT =       2415
234928                 XDOT =         736
163606
 YDOT =      24004
419578  feet/sec       YDOT =        7316
547087  meter/sec
 ZDOT =      -1280
237151                 ZDOT =        -390
216284


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   18212
89378228  
00016717  00000-0  10270-3 0  9053
2 25544  51
6370 155
8935 0005244   9
3570 350
7680 15
53747966  5466


Satellite: ISS
Catalog Number: 25544
Epoch time:      18212
89378228   =   yrday
fracday
Element set:     905
Inclination:       51
6370  deg
RA of node:       155
8935  deg
Eccentricity:     
0005244     
Arg of perigee:     9
3570  deg
Mean anomaly:     350
7680  deg
Mean motion:   15
53747966  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             546
Checksum:              333


Coasting Arc #7 (Orbit 547)
---------------------------------------

Vector Time (GMT): 2018/212/23:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944329
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1327080
69                 A    =         6781097
50  meter
 Y    =       -4724691
65  meter          E    =           
0011690
 Z    =        4676464
68                 I    =           51
78860
 XDOT =       7053
890677                 Wp   =           44
80123
 YDOT =       -880
398239  meter/sec      RA   =          154
29490  deg
 ZDOT =      -2878
744577                 TA   =           73
79917
                                          MA   =           73
67056
                                          Ha   =            222
539  n
mi
                                          Hp   =            214
682

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4353939
28                 X    =         1357099
46
 Y    =      -15500956
84  feet           Y    =        -4709683
55  meter
 Z    =       15342731
89                 Z    =         4682983
89
 XDOT =      23142
685949                 XDOT =        7077
194461
 YDOT =      -2888
445667  feet/sec       YDOT =        -801
386407  meter/sec
 ZDOT =      -9444
700057                 ZDOT =       -2844
423225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15463889
53                 X    =         4713393
53
 Y    =       -4380727
61  feet           Y    =        -1335245
78  meter
 Z    =       15372482
50                 Z    =         4685532
67
 XDOT =      14158
859351                 XDOT =        4315
620330
 YDOT =      17235
131315  feet/sec       YDOT =        5253
268025  meter/sec
 ZDOT =      -9290
666011                 ZDOT =       -2831
795000


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   18213
02241590  
00016717  00000-0  10270-3 0  9061
2 25544  51
6395 155
2514 0004907  11
7686 348
3581 15
53756696  5485


Satellite: ISS
Catalog Number: 25544
Epoch time:      18213
02241590   =   yrday
fracday
Element set:     906
Inclination:       51
6395  deg
RA of node:       155
2514  deg
Eccentricity:     
0004907     
Arg of perigee:    11
7686  deg
Mean anomaly:     348
3581  deg
Mean motion:   15
53756696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             548
Checksum:              320


Coasting Arc #8 (Orbit 562)
---------------------------------------

Vector Time (GMT): 2018/213/23:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944329
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2682695
16                 A    =         6784431
79  meter
 Y    =        4997044
29  meter          E    =           
0007749
 Z    =       -3725853
52                 I    =           51
82901
 XDOT =      -6330
120546                 Wp   =           62
67314
 YDOT =       -188
726353  meter/sec      RA   =          149
32141  deg
 ZDOT =       4315
054898                 TA   =          253
02890
                                          MA   =          253
11385
                                          Ha   =            222
578  n
mi
                                          Hp   =            214
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8801493
30                 X    =        -2720276
12
 Y    =       16394502
26  feet           Y    =         4966834
45  meter
 Z    =      -12223928
88                 Z    =        -3738976
17
 XDOT =     -20768
112028                 XDOT =       -6348
499666
 YDOT =       -619
180949  feet/sec       YDOT =        -259
616951  meter/sec
 ZDOT =      14157
004259                 ZDOT =        4284
261146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18520233
75                 X    =        -5644967
25
 Y    =        1338301
78  feet           Y    =          407914
38  meter
 Z    =      -12283334
90                 Z    =        -3743960
48
 XDOT =     -10478
071474                 XDOT =       -3193
716185
 YDOT =     -16642
387607  feet/sec       YDOT =       -5072
599743  meter/sec
 ZDOT =      14018
894306                 ZDOT =        4272
958985


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   18213
98715969  
00016717  00000-0  10270-3 0  9073
2 25544  51
6393 150
4457 0004967  13
3110 346
8172 15
53769467  5638


Satellite: ISS
Catalog Number: 25544
Epoch time:      18213
98715969   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       150
4457  deg
Eccentricity:     
0004967     
Arg of perigee:    13
3110  deg
Mean anomaly:     346
8172  deg
Mean motion:   15
53769467  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             563
Checksum:              335


Coasting Arc #9 (Orbit 578)
---------------------------------------

Vector Time (GMT): 2018/214/23:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944329
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3826365
85                 A    =         6787860
19  meter
 Y    =       -5061673
94  meter          E    =           
0014749
 Z    =        2399731
69                 I    =           51
86861
 XDOT =       5272
288479                 Wp   =           86
94476
 YDOT =       1419
468901  meter/sec      RA   =          144
35762  deg
 ZDOT =      -5383
349813                 TA   =           66
32996
                                          MA   =           66
17524
                                          Ha   =            222
625  n
mi
                                          Hp   =            214
467

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12553693
75                 X    =         3871025
99
 Y    =      -16606541
81  feet           Y    =        -5018635
20  meter
 Z    =        7873135
46                 Z    =         2418427
06
 XDOT =      17297
534381                 XDOT =        5282
172951
 YDOT =       4657
050200  feet/sec       YDOT =        1478
482614  meter/sec
 ZDOT =     -17661
908836                 ZDOT =       -5357
715097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20738701
48                 X    =         6321156
21
 Y    =        1393645
20  feet           Y    =          424783
06  meter
 Z    =        7957558
26                 Z    =         2425463
76
 XDOT =       5719
971942                 XDOT =        1743
447448
 YDOT =      15615
773302  feet/sec       YDOT =        4759
687703  meter/sec
 ZDOT =     -17547
064570                 ZDOT =       -5348
345281


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   18215
01621872  
00016717  00000-0  10270-3 0  9089
2 25544  51
6395 145
3181 0004852  17
9146 342
2176 15
53777416  5793


Satellite: ISS
Catalog Number: 25544
Epoch time:      18215
01621872   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:       145
3181  deg
Eccentricity:     
0004852     
Arg of perigee:    17
9146  deg
Mean anomaly:     342
2176  deg
Mean motion:   15
53777416  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             579
Checksum:              316


Coasting Arc #10 (Orbit 589)
---------------------------------------

Vector Time (GMT): 2018/215/16:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 919622
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5892610
36                 A    =         6787866
98  meter
 Y    =       -2314890
17  meter          E    =           
0005729
 Z    =       -2455326
22                 I    =           51
88775
 XDOT =        -75
213149                 Wp   =           75
72737
 YDOT =       5477
792354  meter/sec      RA   =          140
84106  deg
 ZDOT =      -5354
063026                 TA   =          131
63152
                                          MA   =          131
58244
                                          Ha   =            222
785  n
mi
                                          Hp   =            214
506

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19332711
15                 X    =         5929984
74
 Y    =       -7594784
03  feet           Y    =        -2248785
91  meter
 Z    =       -8055532
21                 Z    =        -2426611
46
 XDOT =       -246
762300                 XDOT =        -110
454738
 YDOT =      17971
759693  feet/sec       YDOT =        5476
754323  meter/sec
 ZDOT =     -17565
823575                 ZDOT =       -5354
513873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15126320
59                 X    =        -4610502
52
 Y    =       14307056
19  feet           Y    =         4360790
73  meter
 Z    =       -7926451
45                 Z    =        -2415982
40
 XDOT =      -5570
847570                 XDOT =       -1697
994339
 YDOT =     -15606
428880  feet/sec       YDOT =       -4756
839523  meter/sec
 ZDOT =     -17568
450318                 ZDOT =       -5354
863657


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   18215
72369328  
00016717  00000-0  10270-3 0  9093
2 25544  51
6398 141
7974 0005429  16
0328 344
0995 15
53779740  5903


Satellite: ISS
Catalog Number: 25544
Epoch time:      18215
72369328   =   yrday
fracday
Element set:     909
Inclination:       51
6398  deg
RA of node:       141
7974  deg
Eccentricity:     
0005429     
Arg of perigee:    16
0328  deg
Mean anomaly:     344
0995  deg
Mean motion:   15
53779740  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             590
Checksum:              340


Coasting Arc #11 (Orbit 595)
---------------------------------------

Vector Time (GMT): 2018/216/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919622
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3681567
90                 A    =         6788591
26  meter
 Y    =        5329160
81  meter          E    =           
0011669
 Z    =       -2016734
95                 I    =           51
90074
 XDOT =      -5061
936713                 Wp   =           31
42525
 YDOT =      -1390
963359  meter/sec      RA   =          138
76853  deg
 ZDOT =       5589
249585                 TA   =          306
37916
                                          MA   =          306
48676
                                          Ha   =            222
772  n
mi
                                          Hp   =            214
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12078634
83                 X    =        -3731090
26
 Y    =       17484123
40  feet           Y    =         5287714
13  meter
 Z    =       -6616584
49                 Z    =        -2034738
76
 XDOT =     -16607
403914                 XDOT =       -5073
155800
 YDOT =      -4563
528080  feet/sec       YDOT =       -1447
632298  meter/sec
 ZDOT =      18337
433021                 ZDOT =        5564
633342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14956487
13                 X    =        -4558737
28
 Y    =       15060150
43  feet           Y    =         4590333
85  meter
 Z    =       -6697950
62                 Z    =        -2041535
35
 XDOT =     -14550
281376                 XDOT =       -4434
925763
 YDOT =      -6378
573417  feet/sec       YDOT =       -1944
189178  meter/sec
 ZDOT =      18227
144897                 ZDOT =        5555
633764


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   18216
10958886  
00016717  00000-0  10270-3 0  9101
2 25544  51
6398 139
8729 0005261  19
0875 341
0474 15
53773231  5967


Satellite: ISS
Catalog Number: 25544
Epoch time:      18216
10958886   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:       139
8729  deg
Eccentricity:     
0005261     
Arg of perigee:    19
0875  deg
Mean anomaly:     341
0474  deg
Mean motion:   15
53773231  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             596
Checksum:              332


Coasting Arc #12 (Orbit 611)
---------------------------------------

Vector Time (GMT): 2018/217/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919622
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4442597
92                 A    =         6790154
50  meter
 Y    =       -5113286
47  meter          E    =           
0012577
 Z    =         427353
33                 I    =           51
92992
 XDOT =       3829
861153                 Wp   =          106
15543
 YDOT =       2812
872563  meter/sec      RA   =          133
81771  deg
 ZDOT =      -6014
576313                 TA   =           69
25712
                                          MA   =           69
12239
                                          Ha   =            222
874  n
mi
                                          Hp   =            214
134

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14575452
48                 X    =         4497370
07
 Y    =      -16775874
25  feet           Y    =        -5063300
04  meter
 Z    =        1402077
87                 Z    =          449066
64
 XDOT =      12565
161262                 XDOT =        3827
337664
 YDOT =       9228
584524  feet/sec       YDOT =        2855
686844  meter/sec
 ZDOT =     -19732
861920                 ZDOT =       -5995
978301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17079396
71                 X    =         5205800
12
 Y    =      -14208573
42  feet           Y    =        -4330773
18  meter
 Z    =        1500081
20                 Z    =          457224
75
 XDOT =      10006
462323                 XDOT =        3049
969716
 YDOT =       9907
386051  feet/sec       YDOT =        3019
771268  meter/sec
 ZDOT =     -19649
728974                 ZDOT =       -5989
237391


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   18217
13864196  
00016717  00000-0  10270-3 0  9116
2 25544  51
6393 134
7458 0005353  24
7701 335
3708 15
53813452  6123


Satellite: ISS
Catalog Number: 25544
Epoch time:      18217
13864196   =   yrday
fracday
Element set:     911
Inclination:       51
6393  deg
RA of node:       134
7458  deg
Eccentricity:     
0005353     
Arg of perigee:    24
7701  deg
Mean anomaly:     335
3708  deg
Mean motion:   15
53813452  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             612
Checksum:              303


Coasting Arc #13 (Orbit 627)
---------------------------------------

Vector Time (GMT): 2018/218/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919622
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4859137
35                 A    =         6789852
15  meter
 Y    =        4583874
79  meter          E    =           
0018600
 Z    =        1158338
15                 I    =           51
95011
 XDOT =      -2543
645548                 Wp   =           49
39653
 YDOT =      -4199
245087  meter/sec      RA   =          128
86942  deg
 ZDOT =       5897
175782                 TA   =          323
13419
                                          MA   =          323
26192
                                          Ha   =            223
064  n
mi
                                          Hp   =            214
122

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15942051
67                 X    =        -4915660
92
 Y    =       15038959
29  feet           Y    =         4529220
45  meter
 Z    =        3800322
02                 Z    =         1134597
27
 XDOT =      -8345
293793                 XDOT =       -2525
144573
 YDOT =     -13777
050809  feet/sec       YDOT =       -4227
586777  meter/sec
 ZDOT =      19347
689574                 ZDOT =        5884
864408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17968542
19                 X    =        -5476811
66
 Y    =       12579867
82  feet           Y    =         3834343
71  meter
 Z    =        3693260
44                 Z    =         1125705
78
 XDOT =      -5481
401740                 XDOT =       -1670
731250
 YDOT =     -13543
110308  feet/sec       YDOT =       -4127
940022  meter/sec
 ZDOT =      19292
922746                 ZDOT =        5880
482853


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   18218
16769375  
00016717  00000-0  10270-3 0  9124
2 25544  51
6390 129
6185 0005441  28
3422 331
8026 15
53766396  6283


Satellite: ISS
Catalog Number: 25544
Epoch time:      18218
16769375   =   yrday
fracday
Element set:     912
Inclination:       51
6390  deg
RA of node:       129
6185  deg
Eccentricity:     
0005441     
Arg of perigee:    28
3422  deg
Mean anomaly:     331
8026  deg
Mean motion:   15
53766396  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             628
Checksum:              321


Coasting Arc #14 (Orbit 642)
---------------------------------------

Vector Time (GMT): 2018/219/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919622
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5019788
70                 A    =         6787253
78  meter
 Y    =       -3703334
34  meter          E    =           
0007173
 Z    =       -2683130
97                 I    =           51
96309
 XDOT =       1246
717580                 Wp   =           76
77449
 YDOT =       5464
788224  meter/sec      RA   =          123
91847  deg
 ZDOT =      -5220
330194                 TA   =          133
33626
                                          MA   =          133
27645
                                          Ha   =            223
037  n
mi
                                          Hp   =            213
979

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16469123
03                 X    =         5073860
45
 Y    =      -12150047
04  feet           Y    =        -3646897
06  meter
 Z    =       -8802923
13                 Z    =        -2658615
72
 XDOT =       4090
280773                 XDOT =        1210
873545
 YDOT =      17929
095222  feet/sec       YDOT =        5478
529838  meter/sec
 ZDOT =     -17127
067566                 ZDOT =       -5214
360791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17937957
85                 X    =         5467489
55
 Y    =       -9950768
29  feet           Y    =        -3032994
17  meter
 Z    =       -8692467
47                 Z    =        -2649464
09
 XDOT =       1164
739166                 XDOT =         355
012498
 YDOT =      17008
728899  feet/sec       YDOT =        5184
260568  meter/sec
 ZDOT =     -17100
912357                 ZDOT =       -5212
358087


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   18219
13242354  
00016717  00000-0  10270-3 0  9136
2 25544  51
6402 124
8112 0005459  32
6690 327
4800 15
53818561  6438


Satellite: ISS
Catalog Number: 25544
Epoch time:      18219
13242354   =   yrday
fracday
Element set:     913
Inclination:       51
6402  deg
RA of node:       124
8112  deg
Eccentricity:     
0005459     
Arg of perigee:    32
6690  deg
Mean anomaly:     327
4800  deg
Mean motion:   15
53818561  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             643
Checksum:              288


Coasting Arc #15 (Orbit 658)
---------------------------------------

Vector Time (GMT): 2018/220/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919622
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4909111
39                 A    =         6783797
02  meter
 Y    =        2528043
25  meter          E    =           
0014564
 Z    =        3926344
29                 I    =           51
96870
 XDOT =        -63
594193                 Wp   =           79
62156
 YDOT =      -6493
258030  meter/sec      RA   =          118
96173  deg
 ZDOT =       4091
001152                 TA   =          327
74535
                                          MA   =          327
83433
                                          Ha   =            223
240  n
mi
                                          Hp   =            213
811

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16106008
50                 X    =        -4956087
68
 Y    =        8294105
14  feet           Y    =         2472883
20  meter
 Z    =       12881706
99                 Z    =         3902383
93
 XDOT =       -208
642367                 XDOT =         -10
851741
 YDOT =     -21303
339995  feet/sec       YDOT =       -6493
674607  meter/sec
 ZDOT =      13421
919790                 ZDOT =        4090
819825

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17005791
03                 X    =        -5183365
11
 Y    =        6462632
22  feet           Y    =         1969810
30  meter
 Z    =       12773860
85                 Z    =         3893472
79
 XDOT =       2519
932516                 XDOT =         768
075431
 YDOT =     -19965
578896  feet/sec       YDOT =       -6085
508447  meter/sec
 ZDOT =      13421
872474                 ZDOT =        4090
986730


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   18220
16146647  
00016717  00000-0  10270-3 0  9140
2 25544  51
6398 119
6843 0005510  36
4592 323
6935 15
53817162  6596


Satellite: ISS
Catalog Number: 25544
Epoch time:      18220
16146647   =   yrday
fracday
Element set:     914
Inclination:       51
6398  deg
RA of node:       119
6843  deg
Eccentricity:     
0005510     
Arg of perigee:    36
4592  deg
Mean anomaly:     323
6935  deg
Mean motion:   15
53817162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             659
Checksum:              320


Coasting Arc #16 (Orbit 673)
---------------------------------------

Vector Time (GMT): 2018/221/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919622
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4633663
14                 A    =         6780480
56  meter
 Y    =       -1097000
57  meter          E    =           
0016299
 Z    =       -4842566
02                 I    =           51
97351
 XDOT =       -987
312712                 Wp   =           61
78438
 YDOT =       7145
254519  meter/sec      RA   =          113
99677  deg
 ZDOT =      -2562
420026                 TA   =          183
06279
                                          MA   =          183
07278
                                          Ha   =            223
142  n
mi
                                          Hp   =            213
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15202306
89                 X    =         4669107
94
 Y    =       -3599083
25  feet           Y    =        -1044985
20  meter
 Z    =      -15887683
79                 Z    =        -4819971
68
 XDOT =      -3239
214934                 XDOT =       -1054
692875
 YDOT =      23442
436085  feet/sec       YDOT =        7133
837152  meter/sec
 ZDOT =      -8406
889850                 ZDOT =       -2567
379080

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15575834
52                 X    =         4747514
36
 Y    =       -2161872
18  feet           Y    =         -658938
64  meter
 Z    =      -15786124
25                 Z    =        -4811610
67
 XDOT =      -5506
113989                 XDOT =       -1678
263544
 YDOT =      21908
606245  feet/sec       YDOT =        6677
743184  meter/sec
 ZDOT =      -8430
005586                 ZDOT =       -2569
465703


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   18221
12619317  
00016717  00000-0  10270-3 0  9157
2 25544  51
6407 114
8778 0005437  39
7670 320
3881 15
53808520  6741


Satellite: ISS
Catalog Number: 25544
Epoch time:      18221
12619317   =   yrday
fracday
Element set:     915
Inclination:       51
6407  deg
RA of node:       114
8778  deg
Eccentricity:     
0005437     
Arg of perigee:    39
7670  deg
Mean anomaly:     320
3881  deg
Mean motion:   15
53808520  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             674
Checksum:              312


Coasting Arc #17 (Orbit 689)
---------------------------------------

Vector Time (GMT): 2018/222/02:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919622
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4204895
31                 A    =         6778434
35  meter
 Y    =        -488877
36  meter          E    =           
0007134
 Z    =        5288009
25                 I    =           51
97902
 XDOT =       1878
853991                 Wp   =           69
79428
 YDOT =      -7395
748949  meter/sec      RA   =          109
02558  deg
 ZDOT =        811
796787                 TA   =           12
49719
                                          MA   =           12
47951
                                          Ha   =            223
372  n
mi
                                          Hp   =            213
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13795588
27                 X    =        -4224801
81
 Y    =       -1603928
35  feet           Y    =         -536011
02  meter
 Z    =       17349111
73                 Z    =         5267535
41
 XDOT =       6164
219132                 XDOT =        1957
472467
 YDOT =     -24264
268205  feet/sec       YDOT =       -7374
298769  meter/sec
 ZDOT =       2663
375284                 ZDOT =         821
113919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13748955
48                 X    =        -4190681
63
 Y    =       -2652548
84  feet           Y    =         -808496
89  meter
 Z    =       17257251
45                 Z    =         5260010
24
 XDOT =       7774
736096                 XDOT =        2369
739562
 YDOT =     -22725
690720  feet/sec       YDOT =       -6926
790531  meter/sec
 ZDOT =       2706
097771                 ZDOT =         824
818601


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   18222
15523043  
00016717  00000-0  10270-3 0  9162
2 25544  51
6403 109
7506 0005612  43
3908 316
7686 15
53830363  6909


Satellite: ISS
Catalog Number: 25544
Epoch time:      18222
15523043   =   yrday
fracday
Element set:     916
Inclination:       51
6403  deg
RA of node:       109
7506  deg
Eccentricity:     
0005612     
Arg of perigee:    43
3908  deg
Mean anomaly:     316
7686  deg
Mean motion:   15
53830363  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             690
Checksum:              295


Coasting Arc #18 (Orbit 700)
---------------------------------------

Vector Time (GMT): 2018/222/19:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919622
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4285110
29                 A    =         6778559
02  meter
 Y    =         109025
22  meter          E    =           
0007127
 Z    =        5244937
06                 I    =           51
98703
 XDOT =       1176
410698                 Wp   =           77
70661
 YDOT =      -7500
321992  meter/sec      RA   =          105
51929  deg
 ZDOT =       1117
236841                 TA   =            1
64563
                                          MA   =            1
64329
                                          Ha   =            223
239  n
mi
                                          Hp   =            213
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14058760
80                 X    =        -4311487
47
 Y    =         357694
30  feet           Y    =           60958
46  meter
 Z    =       17207798
75                 Z    =         5224057
93
 XDOT =       3859
615152                 XDOT =        1254
767124
 YDOT =     -24607
355618  feet/sec       YDOT =       -7486
728481  meter/sec
 ZDOT =       3665
475201                 ZDOT =        1123
141305

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4310349
33                 X    =         1313794
48
 Y    =      -13506129
65  feet           Y    =        -4116668
32  meter
 Z    =       17114040
69                 Z    =         5216359
60
 XDOT =      21002
206210                 XDOT =        6401
472453
 YDOT =      11381
185257  feet/sec       YDOT =        3468
985266  meter/sec
 ZDOT =       3692
895319                 ZDOT =        1125
594493


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   18222
86269158  
00016717  00000-0  10270-3 0  9175
2 25544  51
6404 106
2218 0005235  45
7364 314
4218 15
53854344  7019


Satellite: ISS
Catalog Number: 25544
Epoch time:      18222
86269158   =   yrday
fracday
Element set:     917
Inclination:       51
6404  deg
RA of node:       106
2218  deg
Eccentricity:     
0005235     
Arg of perigee:    45
7364  deg
Mean anomaly:     314
4218  deg
Mean motion:   15
53854344  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             701
Checksum:              298
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