[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 15th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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
200/11:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
7
201/17:45:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2017/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 180726
22 A = 6789338
31 meter
Y = -6777624
07 meter E =
0017411
Z = 33141
96 I = 51
28589
XDOT = 4796
088250 Wp = 39
13005
YDOT = 165
519396 meter/sec RA = 271
30294 deg
ZDOT = 5986
624952 TA = 321
22889
MA = 321
35370
Ha = 222
385 n
mi
Hp = 213
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 592933
80 X = 256340
98
Y = -22236299
45 feet Y = -6775180
28 meter
Z = 108733
47 Z = 34202
92
XDOT = 15735
197669 XDOT = 4764
801290
YDOT = 543
042637 feet/sec YDOT = 218
977047 meter/sec
ZDOT = 19641
157978 ZDOT = 6009
846521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21133257
95 X = -6441417
02
Y = 6941807
23 feet Y = 2115862
84 meter
Z = 114575
13 Z = 34922
50
XDOT = -4244
261521 XDOT = -1293
650912
YDOT = -13334
694777 feet/sec YDOT = -4064
414968 meter/sec
ZDOT = 19743
641373 ZDOT = 6017
861890
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 17193
56423794
00016717 00000-0 10270-3 0 9008
2 25544 51
6406 271
8366 0005504 24
3370 335
8041 15
54127107 25699
Satellite: ISS
Catalog Number: 25544
Epoch time: 17193
56423794 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 271
8366 deg
Eccentricity:
0005504
Arg of perigee: 24
3370 deg
Mean anomaly: 335
8041 deg
Mean motion: 15
54127107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 301
Coasting Arc #2 (Orbit 2583)
---------------------------------------
Vector Time (GMT): 2017/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -988320
91 A = 6787921
55 meter
Y = 6484238
16 meter E =
0007308
Z = -1751142
77 I = 51
28113
XDOT = -4677
623856 Wp = 98
35636
YDOT = -2231
247859 meter/sec RA = 266
30739 deg
ZDOT = -5643
330082 TA = 100
94894
MA = 100
86671
Ha = 222
424 n
mi
Hp = 213
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3242522
68 X = -1052249
85
Y = 21273747
24 feet Y = 6472828
76 meter
Z = -5745219
06 Z = -1756098
46
XDOT = -15346
534961 XDOT = -4624
913675
YDOT = -7320
366991 feet/sec YDOT = -2283
261098 meter/sec
ZDOT = -18514
862475 ZDOT = -5665
924340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21033126
15 X = 6410896
85
Y = -4519894
06 feet Y = -1377663
71 meter
Z = -5768186
81 Z = -1758143
34
XDOT = -1798
600495 XDOT = -548
213431
YDOT = 15296
462807 feet/sec YDOT = 4662
361863 meter/sec
ZDOT = -18614
233099 ZDOT = -5673
618249
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 17194
52874961
00016717 00000-0 10270-3 0 9012
2 25544 51
6400 267
0284 0005470 28
3207 331
8242 15
54159946 25846
Satellite: ISS
Catalog Number: 25544
Epoch time: 17194
52874961 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 267
0284 deg
Eccentricity:
0005470
Arg of perigee: 28
3207 deg
Mean anomaly: 331
8242 deg
Mean motion: 15
54159946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2584
Checksum: 312
Coasting Arc #3 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2017/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1763716
10 A = 6784694
70 meter
Y = -5680228
33 meter E =
0016498
Z = 3244951
96 I = 51
27347
XDOT = 4457
372495 Wp = 71
34723
YDOT = 4090
666448 meter/sec RA = 261
30487 deg
ZDOT = 4723
374597 TA = 326
52539
MA = 326
62956
Ha = 222
425 n
mi
Hp = 213
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5786470
14 X = 1811340
63
Y = -18635919
73 feet Y = -5660239
17 meter
Z = 10646167
85 Z = 3253634
78
XDOT = 14623
925509 XDOT = 4388
354740
YDOT = 13420
821680 feet/sec YDOT = 4140
125628 meter/sec
ZDOT = 15496
635817 ZDOT = 4744
859492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19428615
47 X = -5921842
00
Y = 1572222
45 feet Y = 479213
40 meter
Z = 10685440
94 Z = 3256922
40
XDOT = 7222
221238 XDOT = 2201
333033
YDOT = -17036
763546 feet/sec YDOT = -5192
805529 meter/sec
ZDOT = 15590
810084 ZDOT = 4752
078913
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 17195
55755931
00016717 00000-0 10270-3 0 9022
2 25544 51
6400 261
8993 0005547 32
0135 328
1354 15
54174017 26000
Satellite: ISS
Catalog Number: 25544
Epoch time: 17195
55755931 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 261
8993 deg
Eccentricity:
0005547
Arg of perigee: 32
0135 deg
Mean anomaly: 328
1354 deg
Mean motion: 15
54174017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 296
Coasting Arc #4 (Orbit 2614)
---------------------------------------
Vector Time (GMT): 2017/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2568347
11 A = 6780894
30 meter
Y = 4461243
75 meter E =
0014207
Z = -4428562
43 I = 51
26554
XDOT = -4070
222904 Wp = 57
12592
YDOT = -5595
786801 meter/sec RA = 256
29301 deg
ZDOT = -3276
670577 TA = 179
59985
MA = 179
59871
Ha = 222
588 n
mi
Hp = 213
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8426335
67 X = -2596531
43
Y = 14636626
46 feet Y = 4432365
40 meter
Z = -14529404
30 Z = -4441106
77
XDOT = -13353
749685 XDOT = -3991
430510
YDOT = -18358
880581 feet/sec YDOT = -5640
862060 meter/sec
ZDOT = -10750
231552 ZDOT = -3296
251232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16715489
23 X = 5094881
12
Y = 2047614
74 feet Y = 624112
97 meter
Z = -14585515
07 Z = -4445664
99
XDOT = -11673
559387 XDOT = -3558
100901
YDOT = 18113
558309 feet/sec YDOT = 5521
012572 meter/sec
ZDOT = -10835
765960 ZDOT = -3302
741464
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 17196
52206873
00016717 00000-0 10270-3 0 9037
2 25544 51
6390 257
0914 0005560 36
1597 323
9930 15
54155888 26154
Satellite: ISS
Catalog Number: 25544
Epoch time: 17196
52206873 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 257
0914 deg
Eccentricity:
0005560
Arg of perigee: 36
1597 deg
Mean anomaly: 323
9930 deg
Mean motion: 15
54155888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2615
Checksum: 325
Coasting Arc #5 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2017/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3340158
60 A = 6777950
63 meter
Y = -2925213
40 meter E =
0007568
Z = 5114452
08 I = 51
26523
XDOT = 3525
446602 Wp = 77
52362
YDOT = 6649
587463 meter/sec RA = 251
27124 deg
ZDOT = 1500
553963 TA = 357
95842
MA = 357
96150
Ha = 222
472 n
mi
Hp = 213
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10958525
60 X = 3347777
49
Y = -9597156
83 feet Y = -2887819
18 meter
Z = 16779698
43 Z = 5130695
79
XDOT = 11566
425860 XDOT = 3443
538226
YDOT = 21816
231834 feet/sec YDOT = 6688
553334 meter/sec
ZDOT = 4923
077307 ZDOT = 1517
480858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13141859
54 X = -4005638
79
Y = -6087558
44 feet Y = -1855487
81 meter
Z = 16851888
38 Z = 5136455
58
XDOT = 14912
857649 XDOT = 4545
439011
YDOT = -18359
265456 feet/sec YDOT = -5595
904111 meter/sec
ZDOT = 4996
740144 ZDOT = 1523
006396
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 17197
55087344
00016717 00000-0 10270-3 0 9042
2 25544 51
6395 251
9621 0005614 38
7693 321
3862 15
54182970 26318
Satellite: ISS
Catalog Number: 25544
Epoch time: 17197
55087344 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 251
9621 deg
Eccentricity:
0005614
Arg of perigee: 38
7693 deg
Mean anomaly: 321
3862 deg
Mean motion: 15
54182970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 324
Coasting Arc #6 (Orbit 2645)
---------------------------------------
Vector Time (GMT): 2017/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4077533
40 A = 6777348
98 meter
Y = 1251480
82 meter E =
0018948
Z = -5282859
19 I = 51
27468
XDOT = -2752
230851 Wp = 79
66266
YDOT = -7129
511004 meter/sec RA = 246
24540 deg
ZDOT = 440
032408 TA = 194
53554
MA = 194
59011
Ha = 222
742 n
mi
Hp = 212
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13377734
25 X = -4065563
27
Y = 4105908
21 feet Y = 1205950
38 meter
Z = -17332215
19 Z = -5302637
37
XDOT = -9029
628776 XDOT = -2674
439684
YDOT = -23390
784135 feet/sec YDOT = -7159
853393 meter/sec
ZDOT = 1443
675878 ZDOT = 426
851392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9260245
17 X = 2822522
73
Y = 10345449
80 feet Y = 3153293
10 meter
Z = -17419743
61 Z = -5309537
85
XDOT = -16738
656886 XDOT = -5101
942619
YDOT = 17291
851340 feet/sec YDOT = 5270
556288 meter/sec
ZDOT = 1386
613567 ZDOT = 422
639815
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 17198
51537699
00016717 00000-0 10270-3 0 9053
2 25544 51
6399 247
1539 0005787 42
0240 318
1356 15
54152438 26468
Satellite: ISS
Catalog Number: 25544
Epoch time: 17198
51537699 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 247
1539 deg
Eccentricity:
0005787
Arg of perigee: 42
0240 deg
Mean anomaly: 318
1356 deg
Mean motion: 15
54152438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2646
Checksum: 335
Coasting Arc #7 (Orbit 2661)
---------------------------------------
Vector Time (GMT): 2017/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4696539
09 A = 6778955
12 meter
Y = 459746
19 meter E =
0012466
Z = 4860888
51 I = 51
29380
XDOT = 1748
338997 Wp = 53
02500
YDOT = 7092
313303 meter/sec RA = 241
22249 deg
ZDOT = -2348
470119 TA = 60
12966
MA = 60
00585
Ha = 222
601 n
mi
Hp = 212
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15408592
81 X = 4667437
27
Y = 1508353
65 feet Y = 512102
93 meter
Z = 15947796
96 Z = 4883632
16
XDOT = 5736
020333 XDOT = 1680
308632
YDOT = 23268
744433 feet/sec YDOT = 7111
484244 meter/sec
ZDOT = -7704
954459 ZDOT = -2340
141854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5256959
23 X = -1602321
17
Y = -14451754
23 feet Y = -4404894
69 meter
Z = 16048154
73 Z = 4891477
56
XDOT = 17423
625232 XDOT = 5310
720971
YDOT = -14896
312560 feet/sec YDOT = -4540
396068 meter/sec
ZDOT = -7669
299960 ZDOT = -2337
602628
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 17199
54417724
00016717 00000-0 10270-3 0 9064
2 25544 51
6391 242
0256 0005792 45
9821 314
1809 15
54200060 26625
Satellite: ISS
Catalog Number: 25544
Epoch time: 17199
54417724 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 242
0256 deg
Eccentricity:
0005792
Arg of perigee: 45
9821 deg
Mean anomaly: 314
1809 deg
Mean motion: 15
54200060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2662
Checksum: 303
Coasting Arc #8 (Orbit 2676)
---------------------------------------
Vector Time (GMT): 2017/200/11:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4621191
90 A = 6778660
22 meter
Y = 245884
77 meter E =
0016673
Z = -4967555
02 I = 51
30972
XDOT = -2600
350832 Wp = 88
47738
YDOT = -6893
059393 meter/sec RA = 236
23527 deg
ZDOT = 2084
364912 TA = 201
89983
MA = 201
97117
Ha = 222
832 n
mi
Hp = 212
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15161390
73 X = -4599468
13
Y = 806708
56 feet Y = 194329
46 meter
Z = -16297752
69 Z = -4989950
47
XDOT = -8531
334751 XDOT = -2533
202347
YDOT = -22615
024256 feet/sec YDOT = -6921
763052 meter/sec
ZDOT = 6838
467560 ZDOT = 2071
895619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7145503
32 X = 2177949
41
Y = 13274994
99 feet Y = 4046218
47 meter
Z = -16396694
21 Z = -4997712
39
XDOT = -15833
476382 XDOT = -4826
043601
YDOT = 16876
295019 feet/sec YDOT = 5143
894722 meter/sec
ZDOT = 6784
481037 ZDOT = 2067
909820
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 17200
50867700
00016717 00000-0 10270-3 0 9077
2 25544 51
6398 237
2169 0005889 49
2030 310
9633 15
54165921 26778
Satellite: ISS
Catalog Number: 25544
Epoch time: 17200
50867700 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 237
2169 deg
Eccentricity:
0005889
Arg of perigee: 49
2030 deg
Mean anomaly: 310
9633 deg
Mean motion: 15
54165921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2677
Checksum: 319
Coasting Arc #9 (Orbit 2692)
---------------------------------------
Vector Time (GMT): 2017/201/11:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5244654
81 A = 6781870
87 meter
Y = 1306462
34 meter E =
0016125
Z = 4087703
60 I = 51
33928
XDOT = 1347
792951 Wp = 68
04171
YDOT = 6528
767659 meter/sec RA = 231
22058 deg
ZDOT = -3797
917765 TA = 61
38012
MA = 61
21802
Ha = 222
754 n
mi
Hp = 212
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17206872
74 X = 5209799
89
Y = 4286293
76 feet Y = 1364916
26 meter
Z = 13411101
05 Z = 4113095
83
XDOT = 4421
892883 XDOT = 1293
134669
YDOT = 21419
841401 feet/sec YDOT = 6543
534432 meter/sec
ZDOT = -12460
360123 ZDOT = -3791
502631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3715831
00 X = -1132585
29
Y = -17251844
88 feet Y = -5258362
32 meter
Z = 13523049
34 Z = 4121825
44
XDOT = 15968
121381 XDOT = 4867
083397
YDOT = -13230
990107 feet/sec YDOT = -4032
805785 meter/sec
ZDOT = -12433
040237 ZDOT = -3789
590664
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 17201
53747144
00016717 00000-0 10270-3 0 9081
2 25544 51
6392 232
0882 0005987 52
7724 307
3971 15
54213377 26937
Satellite: ISS
Catalog Number: 25544
Epoch time: 17201
53747144 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 232
0882 deg
Eccentricity:
0005987
Arg of perigee: 52
7724 deg
Mean anomaly: 307
3971 deg
Mean motion: 15
54213377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2693
Checksum: 322
Coasting Arc #10 (Orbit 2696)
---------------------------------------
Vector Time (GMT): 2017/201/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 60297
68 A = 6781302
31 meter
Y = -5253620
56 meter E =
0014129
Z = 4274749
31 I = 51
34147
XDOT = 6148
078745 Wp = 87
37080
YDOT = 2947
295792 meter/sec RA = 230
05043 deg
ZDOT = 3526
012015 TA = 326
55062
MA = 326
63978
Ha = 222
789 n
mi
Hp = 212
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 197827
03 X = 98276
10
Y = -17236287
93 feet Y = -5252734
44 meter
Z = 14024768
06 Z = 4275133
82
XDOT = 20170
862025 XDOT = 6097
536875
YDOT = 9669
605616 feet/sec YDOT = 3015
764759 meter/sec
ZDOT = 11568
280888 ZDOT = 3555
754835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6970023
33 X = 2124463
11
Y = 15763154
76 feet Y = 4804609
57 meter
Z = 14027280
68 Z = 4275515
15
XDOT = -21143
608430 XDOT = -6444
571849
YDOT = -1089
360455 feet/sec YDOT = -332
037067 meter/sec
ZDOT = 11699
195070 ZDOT = 3565
914657
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 17201
79467021
00016717 00000-0 10270-3 0 9093
2 25544 51
6385 230
8063 0005895 52
3945 307
7742 15
54216695 26975
Satellite: ISS
Catalog Number: 25544
Epoch time: 17201
79467021 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 230
8063 deg
Eccentricity:
0005895
Arg of perigee: 52
3945 deg
Mean anomaly: 307
7742 deg
Mean motion: 15
54216695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2697
Checksum: 332
Coasting Arc #11 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2017/202/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1449346
61 A = 6778248
77 meter
Y = 4282787
62 meter E =
0018955
Z = -5067142
63 I = 51
35208
XDOT = -6166
407964 Wp = 70
19293
YDOT = -4176
444751 meter/sec RA = 225
03545 deg
ZDOT = -1765
302808 TA = 182
62583
MA = 182
63580
Ha = 222
941 n
mi
Hp = 212
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4755074
17 X = -1472516
79
Y = 14051140
47 feet Y = 4266451
10 meter
Z = -16624483
70 Z = -5074238
77
XDOT = -20230
997256 XDOT = -6110
672699
YDOT = -13702
246559 feet/sec YDOT = -4245
089862 meter/sec
ZDOT = -5791
675878 ZDOT = -1795
122047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1775978
20 X = -541318
15
Y = -14691019
53 feet Y = -4477822
75 meter
Z = -16656487
74 Z = -5076897
46
XDOT = 23033
383759 XDOT = 7020
575370
YDOT = 3933
989590 feet/sec YDOT = 1199
080027 meter/sec
ZDOT = -5922
762918 ZDOT = -1805
258137
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 17202
75916495
00016717 00000-0 10270-3 0 9106
2 25544 51
6378 225
9977 0006060 55
4788 304
6936 15
54195232 27122
Satellite: ISS
Catalog Number: 25544
Epoch time: 17202
75916495 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 225
9977 deg
Eccentricity:
0006060
Arg of perigee: 55
4788 deg
Mean anomaly: 304
6936 deg
Mean motion: 15
54195232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 332
Coasting Arc #12 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2017/203/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2870279
96 A = 6777068
63 meter
Y = -3107719
73 meter E =
0008122
Z = 5288221
29 I = 51
37248
XDOT = 5785
405088 Wp = 65
51574
YDOT = 5039
883802 meter/sec RA = 220
01703 deg
ZDOT = -174
837061 TA = 26
17579
MA = 26
13475
Ha = 222
738 n
mi
Hp = 212
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9416929
01 X = 2879130
87
Y = -10195930
88 feet Y = -3075573
41 meter
Z = 17349807
38 Z = 5302185
12
XDOT = 18980
987823 XDOT = 5729
467055
YDOT = 16535
051845 feet/sec YDOT = 5104
267380 meter/sec
ZDOT = -573
612406 ZDOT = -146
869175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3851682
26 X = -1173992
75
Y = 13252891
45 feet Y = 4039481
31 meter
Z = 17411972
50 Z = 5307169
22
XDOT = -23365
192989 XDOT = -7121
710823
YDOT = -6183
219414 feet/sec YDOT = -1884
645277 meter/sec
ZDOT = -450
808147 ZDOT = -137
406323
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 17203
78795460
00016717 00000-0 10270-3 0 9118
2 25544 51
6380 220
8693 0005862 57
8535 302
3186 15
54224636 27289
Satellite: ISS
Catalog Number: 25544
Epoch time: 17203
78795460 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 220
8693 deg
Eccentricity:
0005862
Arg of perigee: 57
8535 deg
Mean anomaly: 302
3186 deg
Mean motion: 15
54224636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 321
Coasting Arc #13 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2017/204/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4217941
92 A = 6778552
68 meter
Y = 1892318
19 meter E =
0017564
Z = -4972924
61 I = 51
40327
XDOT = -4918
062008 Wp = 91
86168
YDOT = -5481
451414 meter/sec RA = 214
99904 deg
ZDOT = 2091
438608 TA = 198
56593
MA = 198
63009
Ha = 222
971 n
mi
Hp = 212
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13838392
13 X = -4214633
34
Y = 6208393
01 feet Y = 1845169
25 meter
Z = -16315369
44 Z = -4993405
41
XDOT = -16135
374043 XDOT = -4866
560415
YDOT = -17983
764483 feet/sec YDOT = -5536
160748 meter/sec
ZDOT = 6861
675224 ZDOT = 2067
673301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9383267
18 X = 2860019
84
Y = -11791054
95 feet Y = -3593913
55 meter
Z = -16406152
53 Z = -5000595
29
XDOT = 21745
404095 XDOT = 6627
999168
YDOT = 7929
071499 feet/sec YDOT = 2416
780993 meter/sec
ZDOT = 6757
478910 ZDOT = 2059
679572
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 17204
75244360
00016717 00000-0 10270-3 0 9125
2 25544 51
6384 216
0598 0006056 61
7119 298
4644 15
54199742 27432
Satellite: ISS
Catalog Number: 25544
Epoch time: 17204
75244360 = yrday
fracday
Element set: 912
Inclination: 51
6384 deg
RA of node: 216
0598 deg
Eccentricity:
0006056
Arg of perigee: 61
7119 deg
Mean anomaly: 298
4644 deg
Mean motion: 15
54199742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 321
Coasting Arc #14 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2017/205/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5362064
31 A = 6781915
24 meter
Y = -667806
14 meter E =
0016465
Z = 4088211
26 I = 51
44156
XDOT = 3615
336318 Wp = 72
76369
YDOT = 5593
652032 meter/sec RA = 209
99142 deg
ZDOT = -3810
632458 TA = 56
74009
MA = 56
58242
Ha = 222
922 n
mi
Hp = 212
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17592074
51 X = 5349275
31
Y = -2190965
02 feet Y = -607915
67 meter
Z = 13412766
61 Z = 4114226
81
XDOT = 11861
339627 XDOT = 3571
027684
YDOT = 18351
876746 feet/sec YDOT = 5633
833679 meter/sec
ZDOT = -12502
074993 ZDOT = -3793
177933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14400600
01 X = -4389302
88
Y = 10188427
52 feet Y = 3105432
71 meter
Z = 13527837
43 Z = 4123284
85
XDOT = -18444
622545 XDOT = -5621
920952
YDOT = -9496
081927 feet/sec YDOT = -2894
405771 meter/sec
ZDOT = -12425
759379 ZDOT = -3787
371459
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 17205
78122893
00016717 00000-0 10270-3 0 9136
2 25544 51
6382 210
9312 0006078 65
7135 294
4652 15
54195646 27594
Satellite: ISS
Catalog Number: 25544
Epoch time: 17205
78122893 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 210
9312 deg
Eccentricity:
0006078
Arg of perigee: 65
7135 deg
Mean anomaly: 294
4652 deg
Mean motion: 15
54195646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 324
Coasting Arc #15 (Orbit 2773)
---------------------------------------
Vector Time (GMT): 2017/206/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6165585
57 A = 6785647
81 meter
Y = -409895
51 meter E =
0010628
Z = -2806538
97 I = 51
48375
XDOT = -1951
744080 Wp = 66
43937
YDOT = -5382
597984 meter/sec RA = 204
99527 deg
ZDOT = 5093
335520 TA = 261
65467
MA = 261
77518
Ha = 222
945 n
mi
Hp = 212
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20228299
12 X = -6146911
28
Y = -1344801
56 feet Y = -478738
75 meter
Z = -9207805
03 Z = -2836443
48
XDOT = -6403
359841 XDOT = -1916
149776
YDOT = -17659
442204 feet/sec YDOT = -5404
224895 meter/sec
ZDOT = 16710
418373 ZDOT = 5083
940995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18271136
21 X = 5569042
32
Y = -8643362
56 feet Y = -2634496
91 meter
Z = -9339920
50 Z = -2846807
77
XDOT = 13655
290323 XDOT = 4162
132491
YDOT = 10920
861838 feet/sec YDOT = 3328
678688 meter/sec
ZDOT = 16669
676349 ZDOT = 5080
917351
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 17206
74571304
00016717 00000-0 10270-3 0 9149
2 25544 51
6390 206
1224 0005988 69
0643 291
1150 15
54211323 27747
Satellite: ISS
Catalog Number: 25544
Epoch time: 17206
74571304 = yrday
fracday
Element set: 914
Inclination: 51
6390 deg
RA of node: 206
1224 deg
Eccentricity:
0005988
Arg of perigee: 69
0643 deg
Mean anomaly: 291
1150 deg
Mean motion: 15
54211323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2774
Checksum: 290
Coasting Arc #16 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2017/207/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6534280
89 A = 6788520
09 meter
Y = 1391501
70 meter E =
0018249
Z = 1168373
62 I = 51
52405
XDOT = 4
458277 Wp = 107
88643
YDOT = 4954
063035 meter/sec RA = 200
01121 deg
ZDOT = -5855
218725 TA = 59
40158
MA = 59
22170
Ha = 223
034 n
mi
Hp = 212
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21437929
44 X = 6512559
84
Y = 4565294
29 feet Y = 1464450
99 meter
Z = 3833246
80 Z = 1200061
80
XDOT = 14
626893 XDOT = -22
498459
YDOT = 16253
487648 feet/sec YDOT = 4953
962291 meter/sec
ZDOT = -19210
035188 ZDOT = -5855
262436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20812312
05 X = -6343592
71
Y = 6795769
97 feet Y = 2071350
69 meter
Z = 3973120
84 Z = 1211007
23
XDOT = -7781
209741 XDOT = -2371
712729
YDOT = -12469
354495 feet/sec YDOT = -3800
659250 meter/sec
ZDOT = -19210
938917 ZDOT = -5855
494182
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 17207
77449327
00016717 00000-0 10270-3 0 9153
2 25544 51
6400 200
9930 0005993 73
1852 286
9958 15
54194168 27902
Satellite: ISS
Catalog Number: 25544
Epoch time: 17207
77449327 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 200
9930 deg
Eccentricity:
0005993
Arg of perigee: 73
1852 deg
Mean anomaly: 286
9958 deg
Mean motion: 15
54194168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 339
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