[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: July 31st 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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


209/15:41:12 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 3

209/22:00:48 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 4

212/23:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 212 1

216/02:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 4

219/05:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 3

221/12:26:03 848 -0 5 0 8 0 8
N/A 0 6 -0 0 222 8
000/00:02:03 697 0 0 -0 0 213 0

Coasting Arc #1 (Orbit 2816)
---------------------------------------

Vector Time (GMT): 2017/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4213834
52                 A    =         6780379
65  meter
 Y    =        2820371
98  meter          E    =           
0015394
 Z    =       -4515781
43                 I    =           51
54898
 XDOT =      -5886
478534                 Wp   =           98
14095
 YDOT =      -3731
962337  meter/sec      RA   =          191
20937  deg
 ZDOT =       3169
191625                 TA   =          203
73045
                                          MA   =          203
80152
                                          Ha   =            223
112  n
mi
                                          Hp   =            212
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13824916
41                 X    =        -4223124
32
 Y    =        9253188
91  feet           Y    =         2773198
12  meter
 Z    =      -14815555
88                 Z    =        -4536273
20
 XDOT =     -19312
593616                 XDOT =       -5859
703428
 YDOT =     -12243
970923  feet/sec       YDOT =       -3797
639266  meter/sec
 ZDOT =      10397
610317                 ZDOT =        3140
662305

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15501714
19                 X    =         4724922
49
 Y    =        5808790
46  feet           Y    =         1770519
33  meter
 Z    =      -14906553
09                 Z    =        -4543517
38
 XDOT =       1702
313655                 XDOT =         518
865202
 YDOT =      21757
413705  feet/sec       YDOT =        6631
659697  meter/sec
 ZDOT =      10272
005624                 ZDOT =        3130
907314


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   17209
51048267  
00016717  00000-0  10270-3 0  9009
2 25544  51
6369 192
3365 0006212  77
5017 282
6830 15
54203785 28176


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
51048267   =   yrday
fracday
Element set:     900
Inclination:       51
6369  deg
RA of node:       192
3365  deg
Eccentricity:     
0006212     
Arg of perigee:    77
5017  deg
Mean anomaly:     282
6830  deg
Mean motion:   15
54203785  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2817
Checksum:              309


Coasting Arc #2 (Orbit 2819)
---------------------------------------

Vector Time (GMT): 2017/209/15:41:12
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -168188
93                 A    =         6777194
52  meter
 Y    =       -4271835
80  meter          E    =           
0008745
 Z    =        5251162
60                 I    =           51
54597
 XDOT =       7595
145359                 Wp   =           93
14703
 YDOT =        729
610724  meter/sec      RA   =          190
47354  deg
 ZDOT =        835
133141                 TA   =          348
85696
                                          MA   =          348
87632
                                          Ha   =            222
942  n
mi
                                          Hp   =            212
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -551800
96                 X    =         -145914
88
 Y    =      -14015209
31  feet           Y    =        -4273592
12  meter
 Z    =       17228223
75                 Z    =         5250399
65
 XDOT =      24918
455901                 XDOT =        7582
365559
 YDOT =       2393
735971  feet/sec       YDOT =         814
473335  meter/sec
 ZDOT =       2739
938126                 ZDOT =         871
996503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         892190
79                 X    =          271939
75
 Y    =       14001069
89  feet           Y    =         4267526
10  meter
 Z    =       17225455
22                 Z    =         5250318
75
 XDOT =     -23914
619260                 XDOT =       -7289
175951
 YDOT =      -2054
158131  feet/sec       YDOT =        -626
107398  meter/sec
 ZDOT =       2902
816934                 ZDOT =         884
778602


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   17209
70337551  
00016717  00000-0  10270-3 0  9018
2 25544  51
6391 191
3754 0005968  77
5082 282
6738 15
54267949 28204


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
70337551   =   yrday
fracday
Element set:     901
Inclination:       51
6391  deg
RA of node:       191
3754  deg
Eccentricity:     
0005968     
Arg of perigee:    77
5082  deg
Mean anomaly:     282
6738  deg
Mean motion:   15
54267949  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2820
Checksum:              336


Coasting Arc #3 (Orbit 2823)
---------------------------------------

Vector Time (GMT): 2017/209/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3736293
72                 A    =         6779622
45  meter
 Y    =       -3162965
68  meter          E    =           
0013618
 Z    =        4681313
60                 I    =           51
56076
 XDOT =       6334
358803                 Wp   =           70
39139
 YDOT =       3287
322634  meter/sec      RA   =          189
12705  deg
 ZDOT =      -2823
361592                 TA   =           47
67902
                                          MA   =           47
56371
                                          Ha   =            222
873  n
mi
                                          Hp   =            212
378

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12258181
50                 X    =         3748645
90
 Y    =      -10377184
00  feet           Y    =        -3121114
90  meter
 Z    =       15358640
40                 Z    =         4699493
10
 XDOT =      20782
017070                 XDOT =        6310
842655
 YDOT =      10785
179245  feet/sec       YDOT =        3358
026286  meter/sec
 ZDOT =      -9262
997349                 ZDOT =       -2792
648683

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11607224
79                 X    =         3537882
12
 Y    =       10987812
24  feet           Y    =         3349085
17  meter
 Z    =       15439466
03                 Z    =         4705949
25
 XDOT =      -7710
817440                 XDOT =       -2350
257156
 YDOT =      21022
422165  feet/sec       YDOT =        6407
634276  meter/sec
 ZDOT =      -9127
668913                 ZDOT =       -2782
113485


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   17209
96056611  
00016717  00000-0  10270-3 0  9022
2 25544  51
6376 190
0905 0005866  79
2364 280
9449 15
54229126 28249


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
96056611   =   yrday
fracday
Element set:     902
Inclination:       51
6376  deg
RA of node:       190
0905  deg
Eccentricity:     
0005866     
Arg of perigee:    79
2364  deg
Mean anomaly:     280
9449  deg
Mean motion:   15
54229126  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2824
Checksum:              325


Coasting Arc #4 (Orbit 2838)
---------------------------------------

Vector Time (GMT): 2017/210/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5145439
70                 A    =         6783287
11  meter
 Y    =        2521041
96  meter          E    =           
0011495
 Z    =       -3640988
36                 I    =           51
60512
 XDOT =      -4973
042260                 Wp   =           92
00799
 YDOT =      -3839
849309  meter/sec      RA   =          184
13247  deg
 ZDOT =       4380
740927                 TA   =          224
81120
                                          MA   =          224
90409
                                          Ha   =            222
993  n
mi
                                          Hp   =            212
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16881363
85                 X    =        -5155562
27
 Y    =        8271135
04  feet           Y    =         2463445
63  meter
 Z    =      -11945499
87                 Z    =        -3666007
61
 XDOT =     -16315
755447                 XDOT =       -4951
013735
 YDOT =     -12597
930803  feet/sec       YDOT =       -3895
338162  meter/sec
 ZDOT =      14372
509602                 ZDOT =        4356
637086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10277080
25                 X    =        -3132454
06
 Y    =      -15655983
65  feet           Y    =        -4771943
82  meter
 Z    =      -12056487
25                 Z    =        -3674817
31
 XDOT =       9337
557074                 XDOT =        2846
087396
 YDOT =     -17086
918311  feet/sec       YDOT =       -5208
092701  meter/sec
 ZDOT =      14266
467605                 ZDOT =        4348
419326


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   17210
92503196  
00016717  00000-0  10270-3 0  9036
2 25544  51
6371 185
2808 0006019  83
6799 276
5039 15
54238919 28396


Satellite: ISS
Catalog Number: 25544
Epoch time:      17210
92503196   =   yrday
fracday
Element set:     903
Inclination:       51
6371  deg
RA of node:       185
2808  deg
Eccentricity:     
0006019     
Arg of perigee:    83
6799  deg
Mean anomaly:     276
5039  deg
Mean motion:   15
54238919  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2839
Checksum:              336


Coasting Arc #5 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2017/211/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6170574
00                 A    =         6786871
70  meter
 Y    =       -1797366
10  meter          E    =           
0019428
 Z    =        2156053
84                 I    =           51
64976
 XDOT =       3186
579557                 Wp   =          102
54461
 YDOT =       4301
745156  meter/sec      RA   =          179
15177  deg
 ZDOT =      -5496
173506                 TA   =           53
52958
                                          MA   =           53
35070
                                          Ha   =            222
882  n
mi
                                          Hp   =            212
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20244665
36                 X    =         6179741
05
 Y    =       -5896870
40  feet           Y    =        -1728311
35  meter
 Z    =        7073667
45                 Z    =         2186050
55
 XDOT =      10454
657338                 XDOT =        3164
936973
 YDOT =      14113
337126  feet/sec       YDOT =        4337
258805  meter/sec
 ZDOT =     -18032
065307                 ZDOT =       -5480
746653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8670628
76                 X    =         2642807
65
 Y    =       19171378
61  feet           Y    =         5843436
20  meter
 Z    =        7206578
02                 Z    =         2196564
98
 XDOT =     -11091
574307                 XDOT =       -3380
711849
 YDOT =      11814
842143  feet/sec       YDOT =        3601
163885  meter/sec
 ZDOT =     -17964
448958                 ZDOT =       -5475
564042


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   17211
95379051  
00016717  00000-0  10270-3 0  9042
2 25544  51
6369 180
1512 0005887  85
6852 274
4974 15
54271611 28552


Satellite: ISS
Catalog Number: 25544
Epoch time:      17211
95379051   =   yrday
fracday
Element set:     904
Inclination:       51
6369  deg
RA of node:       180
1512  deg
Eccentricity:     
0005887     
Arg of perigee:    85
6852  deg
Mean anomaly:     274
4974  deg
Mean motion:   15
54271611  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2855
Checksum:              328


Coasting Arc #6 (Orbit 2869)
---------------------------------------

Vector Time (GMT): 2017/212/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6681556
19                 A    =         6788877
38  meter
 Y    =        1069825
76  meter          E    =           
0015573
 Z    =        -489718
33                 I    =           51
68791
 XDOT =      -1170
985911                 Wp   =           59
50802
 YDOT =      -4639
122142  meter/sec      RA   =          174
18124  deg
 ZDOT =       5991
602501                 TA   =          295
21359
                                          MA   =          295
37496
                                          Ha   =            223
036  n
mi
                                          Hp   =            212
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21921116
10                 X    =        -6690643
88
 Y    =        3509927
05  feet           Y    =          995057
27  meter
 Z    =       -1606687
45                 Z    =         -522197
04
 XDOT =      -3841
817294                 XDOT =       -1148
127030
 YDOT =     -15220
217000  feet/sec       YDOT =       -4652
089330  meter/sec
 ZDOT =      19657
488521                 ZDOT =        5985
969593

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6911595
09                 X    =        -2106654
18
 Y    =      -21085587
52  feet           Y    =        -6426887
08  meter
 Z    =       -1750490
17                 Z    =         -533549
40
 XDOT =      12867
206826                 XDOT =        3921
924640
 YDOT =      -5810
240366  feet/sec       YDOT =       -1770
961264  meter/sec
 ZDOT =      19633
230346                 ZDOT =        5984
208609


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   17212
91825359  
00016717  00000-0  10270-3 0  9057
2 25544  51
6361 175
3425 0006125  92
0364 268
1491 15
54241206 28707


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
91825359   =   yrday
fracday
Element set:     905
Inclination:       51
6361  deg
RA of node:       175
3425  deg
Eccentricity:     
0006125     
Arg of perigee:    92
0364  deg
Mean anomaly:     268
1491  deg
Mean motion:   15
54241206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2870
Checksum:              298


Coasting Arc #7 (Orbit 2870)
---------------------------------------

Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2659264
20                 A    =         6779404
60  meter
 Y    =        4061349
83  meter          E    =           
0017213
 Z    =       -4748498
85                 I    =           51
65952
 XDOT =      -7013
473318                 Wp   =          103
73935
 YDOT =      -1414
986893  meter/sec      RA   =          173
89662  deg
 ZDOT =       2721
782543                 TA   =          193
19497
                                          MA   =          193
24005
                                          Ha   =            223
085  n
mi
                                          Hp   =            212
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8724620
07                 X    =        -2681415
94
 Y    =       13324638
56  feet           Y    =         4031488
47  meter
 Z    =      -15579064
46                 Z    =        -4761470
27
 XDOT =     -23010
083064                 XDOT =       -7010
350287
 YDOT =      -4642
345448  feet/sec       YDOT =       -1493
398965  meter/sec
 ZDOT =       8929
732751                 ZDOT =        2687
721056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15823544
13                 X    =        -4823016
25
 Y    =       -1213084
20  feet           Y    =         -369748
06  meter
 Z    =      -15637011
08                 Z    =        -4766160
98
 XDOT =      -7026
612867                 XDOT =       -2141
711602
 YDOT =     -21330
383340  feet/sec       YDOT =       -6501
500842  meter/sec
 ZDOT =       8779
279744                 ZDOT =        2675
924466


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   17212
98255152  
00016717  00000-0  10270-3 0  9063
2 25544  51
6376 175
0218 0006201  93
4558 266
7304 15
54239870 28717


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
98255152   =   yrday
fracday
Element set:     906
Inclination:       51
6376  deg
RA of node:       175
0218  deg
Eccentricity:     
0006201     
Arg of perigee:    93
4558  deg
Mean anomaly:     266
7304  deg
Mean motion:   15
54239870  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2871
Checksum:              314


Coasting Arc #8 (Orbit 2886)
---------------------------------------

Vector Time (GMT): 2017/213/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4231735
24                 A    =         6783180
08  meter
 Y    =       -3795503
34  meter          E    =           
0017771
 Z    =        3685924
83                 I    =           51
70457
 XDOT =       5886
787039                 Wp   =           89
32723
 YDOT =       2334
875322  meter/sec      RA   =          168
90814  deg
 ZDOT =      -4335
962196                 TA   =           46
78744
                                          MA   =           46
63916
                                          Ha   =            223
022  n
mi
                                          Hp   =            212
243

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13883645
80                 X    =         4255958
79
 Y    =      -12452438
78  feet           Y    =        -3748045
94  meter
 Z    =       12092929
23                 Z    =         3706539
75
 XDOT =      19313
605772                 XDOT =        5881
302124
 YDOT =       7660
352106  feet/sec       YDOT =        2400
674924  meter/sec
 ZDOT =     -14225
597756                 ZDOT =       -4307
379461

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17635800
50                 X    =         5375391
99
 Y    =        5879660
86  feet           Y    =         1792120
63  meter
 Z    =       12184659
14                 Z    =         3713884
11
 XDOT =       3322
844248                 XDOT =        1012
802927
 YDOT =      19375
355984  feet/sec       YDOT =        5905
608504  meter/sec
 ZDOT =     -14099
490958                 ZDOT =       -4297
524844


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   17214
01130743  
00016717  00000-0  10270-3 0  9078
2 25544  51
6377 169
8912 0006174  97
4264 262
7591 15
54229032 28877


Satellite: ISS
Catalog Number: 25544
Epoch time:      17214
01130743   =   yrday
fracday
Element set:     907
Inclination:       51
6377  deg
RA of node:       169
8912  deg
Eccentricity:     
0006174     
Arg of perigee:    97
4264  deg
Mean anomaly:     262
7591  deg
Mean motion:   15
54229032  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2887
Checksum:              319


Coasting Arc #9 (Orbit 2901)
---------------------------------------

Vector Time (GMT): 2017/214/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5410441
28                 A    =         6786721
62  meter
 Y    =        3416334
94  meter          E    =           
0010690
 Z    =       -2265014
57                 I    =           51
74963
 XDOT =      -4310
653681                 Wp   =           73
62906
 YDOT =      -3229
605120  meter/sec      RA   =          163
93421  deg
 ZDOT =       5449
892062                 TA   =          261
22592
                                          MA   =          261
34700
                                          Ha   =            223
041  n
mi
                                          Hp   =            212
184

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17750791
60                 X    =        -5437239
31
 Y    =       11208447
95  feet           Y    =         3355682
00  meter
 Z    =       -7431150
16                 Z    =        -2291361
43
 XDOT =     -14142
564570                 XDOT =       -4300
691632
 YDOT =     -10595
817324  feet/sec       YDOT =       -3277
754391  meter/sec
 ZDOT =      17880
223300                 ZDOT =        5428
976471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18640784
81                 X    =        -5681711
21
 Y    =       -9564921
28  feet           Y    =        -2915388
00  meter
 Z    =       -7548199
99                 Z    =        -2300691
36
 XDOT =       1194
599154                 XDOT =         364
113822
 YDOT =     -16303
865346  feet/sec       YDOT =       -4969
418157  meter/sec
 ZDOT =      17788
147885                 ZDOT =        5421
827475


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   17214
97576238  
00016717  00000-0  10270-3 0  9087
2 25544  51
6389 165
0830 0006223  99
9829 260
2027 15
54251375 29026


Satellite: ISS
Catalog Number: 25544
Epoch time:      17214
97576238   =   yrday
fracday
Element set:     908
Inclination:       51
6389  deg
RA of node:       165
0830  deg
Eccentricity:     
0006223     
Arg of perigee:    99
9829  deg
Mean anomaly:     260
2027  deg
Mean motion:   15
54251375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2902
Checksum:              327


Coasting Arc #10 (Orbit 2917)
---------------------------------------

Vector Time (GMT): 2017/215/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6143828
16                 A    =         6788813
29  meter
 Y    =       -2818427
13  meter          E    =           
0018832
 Z    =         541083
71                 I    =           51
78687
 XDOT =       2431
649425                 Wp   =          121
35555
 YDOT =       4122
048672  meter/sec      RA   =          158
97039  deg
 ZDOT =      -5995
348010                 TA   =           52
81573
                                          MA   =           52
64395
                                          Ha   =            223
024  n
mi
                                          Hp   =            212
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20156916
53                 X    =         6172259
65
 Y    =       -9246808
18  feet           Y    =        -2749563
73  meter
 Z    =        1775209
01                 Z    =          570997
02
 XDOT =       7977
852443                 XDOT =        2414
496945
 YDOT =      13523
781731  feet/sec       YDOT =        4149
145486  meter/sec
 ZDOT =     -19669
776935                 ZDOT =       -5983
577373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18405980
45                 X    =         5610142
84
 Y    =       12350531
81  feet           Y    =         3764442
10  meter
 Z    =        1907972
81                 Z    =          581550
11
 XDOT =      -6397
457035                 XDOT =       -1949
944904
 YDOT =      12632
795491  feet/sec       YDOT =        3850
476066  meter/sec
 ZDOT =     -19618
281866                 ZDOT =       -5979
652313


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   17216
00451272  
00016717  00000-0  10270-3 0  9094
2 25544  51
6382 159
9535 0006146 104
1410 256
0426 15
54257962 29183


Satellite: ISS
Catalog Number: 25544
Epoch time:      17216
00451272   =   yrday
fracday
Element set:     909
Inclination:       51
6382  deg
RA of node:       159
9535  deg
Eccentricity:     
0006146     
Arg of perigee:   104
1410  deg
Mean anomaly:     256
0426  deg
Mean motion:   15
54257962  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2918
Checksum:              301


Coasting Arc #11 (Orbit 2919)
---------------------------------------

Vector Time (GMT): 2017/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         849441
81                 A    =         6777144
99  meter
 Y    =        4159482
94  meter          E    =           
0020592
 Z    =       -5300579
50                 I    =           51
75404
 XDOT =      -7258
964836                 Wp   =           97
69466
 YDOT =       2331
845253  meter/sec      RA   =          158
24238  deg
 ZDOT =        666
099688                 TA   =          178
67068
                                          MA   =          178
66520
                                          Ha   =            222
968  n
mi
                                          Hp   =            212
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2786882
57                 X    =          828613
51
 Y    =       13646597
57  feet           Y    =         4168865
84  meter
 Z    =      -17390352
69                 Z    =        -5296503
57
 XDOT =     -23815
501429                 XDOT =       -7287
736189
 YDOT =       7650
410936  feet/sec       YDOT =        2250
509665  meter/sec
 ZDOT =       2185
366431                 ZDOT =         630
768615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1580112
87                 X    =          481618
40
 Y    =       13860227
99  feet           Y    =         4224597
49  meter
 Z    =      -17372910
80                 Z    =        -5295263
21
 XDOT =     -23441
944571                 XDOT =       -7145
104705
 YDOT =       5217
233909  feet/sec       YDOT =        1590
212896  meter/sec
 ZDOT =       2028
695889                 ZDOT =         618
346507


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   17216
13310544  
00016717  00000-0  10270-3 0  9106
2 25544  51
6400 159
3154 0005963 103
3530 256
8288 15
54246723 29205


Satellite: ISS
Catalog Number: 25544
Epoch time:      17216
13310544   =   yrday
fracday
Element set:     910
Inclination:       51
6400  deg
RA of node:       159
3154  deg
Eccentricity:     
0005963     
Arg of perigee:   103
3530  deg
Mean anomaly:     256
8288  deg
Mean motion:   15
54246723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2920
Checksum:              285


Coasting Arc #12 (Orbit 2935)
---------------------------------------

Vector Time (GMT): 2017/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         896284
45                 A    =         6778997
94  meter
 Y    =       -4687270
36  meter          E    =           
0012084
 Z    =        4805086
76                 I    =           51
79188
 XDOT =       7108
207208                 Wp   =           81
49867
 YDOT =      -1301
268145  meter/sec      RA   =          153
25229  deg
 ZDOT =      -2587
950655                 TA   =           33
94920
                                          MA   =           33
87193
                                          Ha   =            222
834  n
mi
                                          Hp   =            212
326

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2940565
77                 X    =          925291
75
 Y    =      -15378183
60  feet           Y    =        -4677085
58  meter
 Z    =       15764720
33                 Z    =         4809510
75
 XDOT =      23320
889790                 XDOT =        7134
800830
 YDOT =      -4269
252443  feet/sec       YDOT =       -1221
630501  meter/sec
 ZDOT =      -8490
651755                 ZDOT =       -2553
357225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4038120
19                 X    =         1230819
03
 Y    =      -15105964
86  feet           Y    =        -4604298
09  meter
 Z    =       15784969
94                 Z    =         4811258
84
 XDOT =      22537
914987                 XDOT =        6869
556488
 YDOT =      -2712
275097  feet/sec       YDOT =        -826
701450  meter/sec
 ZDOT =      -8337
369952                 ZDOT =       -2541
230362


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   17217
16185157  
00016717  00000-0  10270-3 0  9111
2 25544  51
6411 154
1857 0005862 106
9229 253
2559 15
54295458 29360


Satellite: ISS
Catalog Number: 25544
Epoch time:      17217
16185157   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:       154
1857  deg
Eccentricity:     
0005862     
Arg of perigee:   106
9229  deg
Mean anomaly:     253
2559  deg
Mean motion:   15
54295458  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2936
Checksum:              325


Coasting Arc #13 (Orbit 2950)
---------------------------------------

Vector Time (GMT): 2017/218/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2458658
52                 A    =         6782637
86  meter
 Y    =        5048136
19  meter          E    =           
0012247
 Z    =       -3817849
96                 I    =           51
83229
 XDOT =      -6395
946679                 Wp   =          107
40925
 YDOT =         63
460440  meter/sec      RA   =          148
27360  deg
 ZDOT =       4210
401175                 TA   =          206
93346
                                          MA   =          206
99707
                                          Ha   =            222
904  n
mi
                                          Hp   =            212
252

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8066464
97                 X    =        -2496380
49
 Y    =       16562126
59  feet           Y    =         5020431
06  meter
 Z    =      -12525754
47                 Z    =        -3829884
53
 XDOT =     -20984
077030                 XDOT =       -6416
632634
 YDOT =        208
203544  feet/sec       YDOT =          -8
179239  meter/sec
 ZDOT =      13813
652148                 ZDOT =        4179
281988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8987770
84                 X    =        -2739472
55
 Y    =       16038590
74  feet           Y    =         4888562
46  meter
 Z    =      -12579745
69                 Z    =        -3834306
49
 XDOT =     -19877
523120                 XDOT =       -6058
669047
 YDOT =       -431
835073  feet/sec       YDOT =        -131
623330  meter/sec
 ZDOT =      13675
904130                 ZDOT =        4168
415579


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   17218
12630014  
00016717  00000-0  10270-3 0  9126
2 25544  51
6406 149
3779 0006070 109
7245 250
4563 15
54289360 29510


Satellite: ISS
Catalog Number: 25544
Epoch time:      17218
12630014   =   yrday
fracday
Element set:     912
Inclination:       51
6406  deg
RA of node:       149
3779  deg
Eccentricity:     
0006070     
Arg of perigee:   109
7245  deg
Mean anomaly:     250
4563  deg
Mean motion:   15
54289360  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2951
Checksum:              300


Coasting Arc #14 (Orbit 2966)
---------------------------------------

Vector Time (GMT): 2017/219/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3757340
14                 A    =         6786422
96  meter
 Y    =       -5118494
38  meter          E    =           
0019745
 Z    =        2368741
76                 I    =           51
87227
 XDOT =       5276
758447                 Wp   =          108
31356
 YDOT =       1358
118124  meter/sec      RA   =          143
30736  deg
 ZDOT =      -5404
622179                 TA   =           45
30586
                                          MA   =           45
14518
                                          Ha   =            222
838  n
mi
                                          Hp   =            212
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12327231
43                 X    =         3802791
29
 Y    =      -16792960
58  feet           Y    =        -5076223
19  meter
 Z    =        7771462
46                 Z    =         2387103
62
 XDOT =      17312
199628                 XDOT =        5287
431902
 YDOT =       4455
768125  feet/sec       YDOT =        1417
186267  meter/sec
 ZDOT =     -17731
700061                 ZDOT =       -5378
963879

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13008398
46                 X    =         3964959
85
 Y    =      -16231580
08  feet           Y    =        -4947385
61  meter
 Z    =        7853481
14                 Z    =         2393741
05
 XDOT =      16029
751500                 XDOT =        4885
868257
 YDOT =       4273
865841  feet/sec       YDOT =        1302
674308  meter/sec
 ZDOT =     -17618
312823                 ZDOT =       -5370
061748


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   17219
15504137  
00016717  00000-0  10270-3 0  9137
2 25544  51
6408 144
2489 0005987 112
1038 248
0751 15
54293566 29670


Satellite: ISS
Catalog Number: 25544
Epoch time:      17219
15504137   =   yrday
fracday
Element set:     913
Inclination:       51
6408  deg
RA of node:       144
2489  deg
Eccentricity:     
0005987     
Arg of perigee:   112
1038  deg
Mean anomaly:     248
0751  deg
Mean motion:   15
54293566  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2967
Checksum:              321


Coasting Arc #15 (Orbit 2968)
---------------------------------------

Vector Time (GMT): 2017/219/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -127311
82                 A    =         6778784
11  meter
 Y    =       -4707870
29  meter          E    =           
0011796
 Z    =        4865971
05                 I    =           51
84901
 XDOT =       6747
040016                 Wp   =           84
10020
 YDOT =      -2720
388191  meter/sec      RA   =          142
70563  deg
 ZDOT =      -2449
202769                 TA   =           29
87116
                                          MA   =           29
80389
                                          Ha   =            222
972  n
mi
                                          Hp   =            212
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -417689
70                 X    =          -98293
72
 Y    =      -15445768
68  feet           Y    =        -4709131
87  meter
 Z    =       15964471
96                 Z    =         4865422
97
 XDOT =      22135
958059                 XDOT =        6788
855448
 YDOT =      -8925
158107  feet/sec       YDOT =       -2644
704330  meter/sec
 ZDOT =      -8035
442156                 ZDOT =       -2416
326927

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10591372
92                 X    =        -3228250
46
 Y    =      -11252773
31  feet           Y    =        -3429845
30  meter
 Z    =       15962722
58                 Z    =         4865437
84
 XDOT =       9946
682792                 XDOT =        3031
748915
 YDOT =     -20582
976125  feet/sec       YDOT =       -6273
691123  meter/sec
 ZDOT =      -7889
516470                 ZDOT =       -2404
724620


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   17219
28363382  
00016717  00000-0  10270-3 0  9147
2 25544  51
6398 143
6085 0006198 111
3243 248
8571 15
54291746 29695


Satellite: ISS
Catalog Number: 25544
Epoch time:      17219
28363382   =   yrday
fracday
Element set:     914
Inclination:       51
6398  deg
RA of node:       143
6085  deg
Eccentricity:     
0006198     
Arg of perigee:   111
3243  deg
Mean anomaly:     248
8571  deg
Mean motion:   15
54291746  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2969
Checksum:              336


Coasting Arc #16 (Orbit 2983)
---------------------------------------

Vector Time (GMT): 2017/220/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1356296
27                 A    =         6782410
59  meter
 Y    =        5381134
72  meter          E    =           
0012629
 Z    =       -3913117
56                 I    =           51
88736
 XDOT =      -6313
685749                 Wp   =          110
61737
 YDOT =       1388
379885  meter/sec      RA   =          137
72999  deg
 ZDOT =       4103
946356                 TA   =          202
29187
                                          MA   =          202
34681
                                          Ha   =            222
920  n
mi
                                          Hp   =            212
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4449790
91                 X    =        -1397361
13
 Y    =       17654641
48  feet           Y    =         5365738
13  meter
 Z    =      -12838312
19                 Z    =        -3919805
57
 XDOT =     -20714
192090                 XDOT =       -6348
676280
 YDOT =       4555
052116  feet/sec       YDOT =        1317
580275  meter/sec
 ZDOT =      13464
390931                 ZDOT =        4073
192095

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8656202
42                 X    =         2638410
50
 Y    =       15993000
16  feet           Y    =         4874666
45  meter
 Z    =      -12868697
30                 Z    =        -3922378
94
 XDOT =     -11148
717592                 XDOT =       -3398
129122
 YDOT =      16741
796940  feet/sec       YDOT =        5102
899707  meter/sec
 ZDOT =      13328
033089                 ZDOT =        4062
384486


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   17220
24807598  
00016717  00000-0  10270-3 0  9158
2 25544  51
6409 138
8006 0006101 114
6514 245
5275 15
54268668 29847


Satellite: ISS
Catalog Number: 25544
Epoch time:      17220
24807598   =   yrday
fracday
Element set:     915
Inclination:       51
6409  deg
RA of node:       138
8006  deg
Eccentricity:     
0006101     
Arg of perigee:   114
6514  deg
Mean anomaly:     245
5275  deg
Mean motion:   15
54268668  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2984
Checksum:              319


Coasting Arc #17 (Orbit 2999)
---------------------------------------

Vector Time (GMT): 2017/221/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2640017
53                 A    =         6786167
40  meter
 Y    =       -5724077
44  meter          E    =           
0019716
 Z    =        2487091
74                 I    =           51
92278
 XDOT =       5507
921234                 Wp   =          108
65936
 YDOT =        207
391175  meter/sec      RA   =          132
76576  deg
 ZDOT =      -5340
911880                 TA   =           43
54977
                                          MA   =           43
39427
                                          Ha   =            222
849  n
mi
                                          Hp   =            212
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8661474
85                 X    =         2691748
64
 Y    =      -18779781
61  feet           Y    =        -5694265
70  meter
 Z    =        8159749
81                 Z    =         2500041
57
 XDOT =      18070
607723                 XDOT =        5531
135791
 YDOT =        680
417240  feet/sec       YDOT =         269
114252  meter/sec
 ZDOT =     -17522
676773                 ZDOT =       -5314
100255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6614571
64                 X    =        -2016121
44
 Y    =      -19570288
06  feet           Y    =        -5965023
80  meter
 Z    =        8217915
08                 Z    =         2504820
52
 XDOT =      12273
026188                 XDOT =        3740
818382
 YDOT =     -11495
217410  feet/sec       YDOT =       -3503
742267  meter/sec
 ZDOT =     -17403
992977                 ZDOT =       -5304
737059


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   17221
27680925  
00016717  00000-0  10270-3 0  9166
2 25544  51
6400 133
6709 0006114 116
9716 243
2061 15
54301823 30003


Satellite: ISS
Catalog Number: 25544
Epoch time:      17221
27680925   =   yrday
fracday
Element set:     916
Inclination:       51
6400  deg
RA of node:       133
6709  deg
Eccentricity:     
0006114     
Arg of perigee:   116
9716  deg
Mean anomaly:     243
2061  deg
Mean motion:   15
54301823  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3000
Checksum:              273


Coasting Arc #18 (Orbit 3003)
---------------------------------------

Vector Time (GMT): 2017/221/12:27:05
697
Vector Time (MET): N/A
Weight (LBS)     : 902191
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2695481
88                 A    =         6777417
67  meter
 Y    =        3249077
08  meter          E    =           
0019648
 Z    =       -5318921
16                 I    =           51
90033
 XDOT =      -5378
728871                 Wp   =          101
60615
 YDOT =       5414
515891  meter/sec      RA   =          131
39598  deg
 ZDOT =        579
645805                 TA   =          173
92819
                                          MA   =          173
90434
                                          Ha   =            222
803  n
mi
                                          Hp   =            212
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8843444
49                 X    =         2684785
72
 Y    =       10659701
71  feet           Y    =         3279159
92  meter
 Z    =      -17450528
76                 Z    =        -5305853
62
 XDOT =     -17646
748263                 XDOT =       -5441
691245
 YDOT =      17764
159746  feet/sec       YDOT =        5354
015250  meter/sec
 ZDOT =       1901
725083                 ZDOT =         553
365118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1006121
31                 X    =         -306665
78
 Y    =      -13886077
79  feet           Y    =        -4232476
51  meter
 Z    =      -17393138
55                 Z    =        -5301428
63
 XDOT =      23708
353469                 XDOT =        7226
306137
 YDOT =      -3961
475320  feet/sec       YDOT =       -1207
457678  meter/sec
 ZDOT =       1784
575997                 ZDOT =         543
938764


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   17221
53399369  
00016717  00000-0  10270-3 0  9175
2 25544  51
6422 132
3895 0005354 121
0961 239
0718 15
54142834 30044


Satellite: ISS
Catalog Number: 25544
Epoch time:      17221
53399369   =   yrday
fracday
Element set:     917
Inclination:       51
6422  deg
RA of node:       132
3895  deg
Eccentricity:     
0005354     
Arg of perigee:   121
0961  deg
Mean anomaly:     239
0718  deg
Mean motion:   15
54142834  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3004
Checksum:              303


Coasting Arc #19 (Orbit 3019)
---------------------------------------

Vector Time (GMT): 2017/222/12:27:05
697
Vector Time (MET): N/A
Weight (LBS)     : 902191
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1425469
85                 A    =         6779171
45  meter
 Y    =       -4489512
88  meter          E    =           
0010305
 Z    =        4866728
63                 I    =           51
92655
 XDOT =       5713
919213                 Wp   =           87
17572
 YDOT =      -4492
124538  meter/sec      RA   =          126
41758  deg
 ZDOT =      -2465
350078                 TA   =           26
93274
                                          MA   =           26
87928
                                          Ha   =            222
747  n
mi
                                          Hp   =            212
963

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4676738
35                 X    =        -1398800
78
 Y    =      -14729372
98  feet           Y    =        -4505304
21  meter
 Z    =       15966957
45                 Z    =         4859869
15
 XDOT =      18746
454111                 XDOT =        5775
701935
 YDOT =     -14737
941396  feet/sec       YDOT =       -4427
882224  meter/sec
 ZDOT =      -8088
418891                 ZDOT =       -2437
443910

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4509165
51                 X    =        -1374393
65
 Y    =       14813574
00  feet           Y    =         4515177
35  meter
 Z    =       15937236
03                 Z    =         4857669
54
 XDOT =     -22770
832891                 XDOT =       -6940
549865
 YDOT =       1654
611566  feet/sec       YDOT =         504
325605  meter/sec
 ZDOT =      -7964
193431                 ZDOT =       -2427
486158


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   17222
56282277  
00016717  00000-0  10270-3 0  9189
2 25544  51
6414 127
2617 0005217 124
9599 235
2044 15
54170895 30203


Satellite: ISS
Catalog Number: 25544
Epoch time:      17222
56282277   =   yrday
fracday
Element set:     918
Inclination:       51
6414  deg
RA of node:       127
2617  deg
Eccentricity:     
0005217     
Arg of perigee:   124
9599  deg
Mean anomaly:     235
2044  deg
Mean motion:   15
54170895  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3020
Checksum:              306


Coasting Arc #20 (Orbit 3034)
---------------------------------------

Vector Time (GMT): 2017/223/12:27:05
697
Vector Time (MET): N/A
Weight (LBS)     : 902191
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         230807
88                 A    =         6782724
92  meter
 Y    =        5527560
64  meter          E    =           
0011544
 Z    =       -3937052
98                 I    =           51
95732
 XDOT =      -5665
687254                 Wp   =          116
73819
 YDOT =       3141
483315  meter/sec      RA   =          121
44699  deg
 ZDOT =       4082
614188                 TA   =          195
85166
                                          MA   =          195
88782
                                          Ha   =            222
648  n
mi
                                          Hp   =            213
119

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         757243
70                 X    =          188104
11
 Y    =       18135041
47  feet           Y    =         5529902
78  meter
 Z    =      -12916840
47                 Z    =        -3936035
71
 XDOT =     -18588
212774                 XDOT =       -5720
226152
 YDOT =      10306
703788  feet/sec       YDOT =        3077
820944  meter/sec
 ZDOT =      13394
403504                 ZDOT =        4054
959813

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9423390
47                 X    =         2872249
41
 Y    =      -15516065
46  feet           Y    =        -4729296
75  meter
 Z    =      -12913146
00                 Z    =        -3935926
90
 XDOT =      20117
669457                 XDOT =        6131
865650
 YDOT =       1184
372039  feet/sec       YDOT =         360
996597  meter/sec
 ZDOT =      13271
478550                 ZDOT =        4045
146662


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   17223
52734800  
00016717  00000-0  10270-3 0  9191
2 25544  51
6419 122
4533 0005155 129
4401 230
7208 15
54145333 30352


Satellite: ISS
Catalog Number: 25544
Epoch time:      17223
52734800   =   yrday
fracday
Element set:     919
Inclination:       51
6419  deg
RA of node:       122
4533  deg
Eccentricity:     
0005155     
Arg of perigee:   129
4401  deg
Mean anomaly:     230
7208  deg
Mean motion:   15
54145333  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3035
Checksum:              277
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