[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 7th 2018
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) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
253/11:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
9
253/22:32:33
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 214
0
257/11:39:28
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
3
257/13:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
2
Coasting Arc #1 (Orbit 1131)
---------------------------------------
Vector Time (GMT): 2018/250/12:36:50
524
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5585673
62 A = 6783821
04 meter
Y = 98101
13 meter E =
0015527
Z = 3840059
37 I = 51
43995
XDOT = -2952
448702 Wp = 109
52527
YDOT = 5751
129674 meter/sec RA = 327
78023 deg
ZDOT = 4128
912099 TA = 296
89496
MA = 297
05355
Ha = 222
921 n
mi
Hp = 213
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18325700
86 X = 5565508
78
Y = 321854
09 feet Y = 160451
46 meter
Z = 12598619
98 Z = 3867143
26
XDOT = -9686
511489 XDOT = -3036
595784
YDOT = 18868
535677 feet/sec YDOT = 5717
643077 meter/sec
ZDOT = 13546
299539 ZDOT = 4114
365648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18139771
03 X = -5529002
21
Y = -1951342
15 feet Y = -594769
09 meter
Z = 12720106
06 Z = 3877088
33
XDOT = 11280
882719 XDOT = 3438
413053
YDOT = -16597
784415 feet/sec YDOT = -5059
004690 meter/sec
ZDOT = 13480
245838 ZDOT = 4108
778931
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 18250
58153555
00016717 00000-0 10270-3 0 9000
2 25544 51
6415 328
0985 0005000 136
2131 223
9419 15
53830749 11323
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
58153555 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 328
0985 deg
Eccentricity:
0005000
Arg of perigee: 136
2131 deg
Mean anomaly: 223
9419 deg
Mean motion: 15
53830749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1132
Checksum: 287
Coasting Arc #2 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2018/251/12:36:50
524
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4665224
68 A = 6780522
61 meter
Y = -1241421
06 meter E =
0014076
Z = -4773466
36 I = 51
40034
XDOT = 4220
934407 Wp = 90
53937
YDOT = -5829
051713 meter/sec RA = 322
77792 deg
ZDOT = -2616
108633 TA = 153
57485
MA = 153
50300
Ha = 222
986 n
mi
Hp = 213
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15305855
24 X = -4627809
38
Y = -4072903
74 feet Y = -1293382
02 meter
Z = -15660978
87 Z = -4796037
10
XDOT = 13848
209998 XDOT = 4298
510268
YDOT = -19124
185410 feet/sec YDOT = -5781
416758 meter/sec
ZDOT = -8583
033572 ZDOT = -2595
416204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14867603
79 X = 4531645
63
Y = 5160997
44 feet Y = 1573072
02 meter
Z = -15762057
98 Z = -4804275
27
XDOT = -14873
163397 XDOT = -4533
340204
YDOT = 16986
756804 feet/sec YDOT = 5177
563474 meter/sec
ZDOT = -8489
416062 ZDOT = -2587
574016
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 18251
54626176
00016717 00000-0 10270-3 0 9012
2 25544 51
6406 323
2923 0005003 139
5949 220
5576 15
53800482 11472
Satellite: ISS
Catalog Number: 25544
Epoch time: 18251
54626176 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 323
2923 deg
Eccentricity:
0005003
Arg of perigee: 139
5949 deg
Mean anomaly: 220
5576 deg
Mean motion: 15
53800482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 298
Coasting Arc #3 (Orbit 1162)
---------------------------------------
Vector Time (GMT): 2018/252/12:36:50
524
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3557113
35 A = 6778432
07 meter
Y = 2419994
25 meter E =
0008063
Z = 5233681
24 I = 51
36840
XDOT = -5141
454259 Wp = 132
80782
YDOT = 5625
112125 meter/sec RA = 317
76639 deg
ZDOT = 887
191697 TA = 308
64343
MA = 308
71556
Ha = 222
762 n
mi
Hp = 213
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11670319
40 X = 3504365
76
Y = 7939613
67 feet Y = 2459477
97 meter
Z = 17170870
20 Z = 5250831
89
XDOT = -16868
288252 XDOT = -5208
283162
YDOT = 18455
092274 feet/sec YDOT = 5567
243248 meter/sec
ZDOT = 2910
733914 ZDOT = 862
053684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11101402
50 X = -3383707
48
Y = -8564814
24 feet Y = -2610555
38 meter
Z = 17247475
85 Z = 5257030
64
XDOT = 17252
800664 XDOT = 5258
653642
YDOT = -16688
404631 feet/sec YDOT = -5086
625731 meter/sec
ZDOT = 2797
222307 ZDOT = 852
593359
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 18252
57529764
00016717 00000-0 10270-3 0 9022
2 25544 51
6410 318
1652 0004883 142
2880 217
8615 15
53838078 11632
Satellite: ISS
Catalog Number: 25544
Epoch time: 18252
57529764 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 318
1652 deg
Eccentricity:
0004883
Arg of perigee: 142
2880 deg
Mean anomaly: 217
8615 deg
Mean motion: 15
53838078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1163
Checksum: 318
Coasting Arc #4 (Orbit 1176)
---------------------------------------
Vector Time (GMT): 2018/253/11:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2905941
02 A = 6778316
81 meter
Y = -3097135
07 meter E =
0018138
Z = -5298305
26 I = 51
34498
XDOT = 5365
644685 Wp = 104
27258
YDOT = -5454
206378 meter/sec RA = 313
08309 deg
ZDOT = 241
706982 TA = 168
06627
MA = 168
02323
Ha = 222
866 n
mi
Hp = 213
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9533927
23 X = -2845355
83
Y = -10161204
30 feet Y = -3129293
19 meter
Z = -17382891
26 Z = -5312273
69
XDOT = 17603
821145 XDOT = 5425
062272
YDOT = -17894
377880 feet/sec YDOT = -5393
871765 meter/sec
ZDOT = 793
001911 ZDOT = 267
916190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4051874
59 X = 1235011
37
Y = 13249918
84 feet Y = 4038575
26 meter
Z = -17445134
36 Z = -5317276
95
XDOT = -22668
770720 XDOT = -6909
441315
YDOT = 8147
867022 feet/sec YDOT = 2483
469868 meter/sec
ZDOT = 911
276848 ZDOT = 277
757183
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 18253
47570396
00016717 00000-0 10270-3 0 9030
2 25544 51
6407 313
6785 0004854 145
8306 214
3160 15
53808870 11774
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
47570396 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 313
6785 deg
Eccentricity:
0004854
Arg of perigee: 145
8306 deg
Mean anomaly: 214
3160 deg
Mean motion: 15
53808870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1177
Checksum: 318
Coasting Arc #5 (Orbit 1184)
---------------------------------------
Vector Time (GMT): 2018/253/22:32:33
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4270597
44 A = 6778994
32 meter
Y = 1291792
42 meter E =
0009476
Z = 5099398
10 I = 51
33726
XDOT = -3857
805429 Wp = 134
10679
YDOT = 6437
361041 meter/sec RA = 310
70366 deg
ZDOT = 1591
746490 TA = 300
43689
MA = 300
53048
Ha = 222
673 n
mi
Hp = 213
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14011146
46 X = 4231064
79
Y = 4238164
12 feet Y = 1339328
78 meter
Z = 16730308
73 Z = 5120046
91
XDOT = -12656
841959 XDOT = -3937
234897
YDOT = 21119
950922 feet/sec YDOT = 6393
776460 meter/sec
ZDOT = 5222
265386 ZDOT = 1572
813002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9380380
07 X = 2859139
84
Y = 11098693
31 feet Y = 3382881
72 meter
Z = 16822751
47 Z = 5127574
65
XDOT = -21306
135480 XDOT = -6494
110094
YDOT = 10180
711988 feet/sec YDOT = 3103
081014 meter/sec
ZDOT = 5136
502944 ZDOT = 1565
606097
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 18253
99022181
00016717 00000-0 10270-3 0 9042
2 25544 51
6410 311
1170 0004747 144
1656 215
9816 15
53842358 11853
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
99022181 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 311
1170 deg
Eccentricity:
0004747
Arg of perigee: 144
1656 deg
Mean anomaly: 215
9816 deg
Mean motion: 15
53842358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1185
Checksum: 299
Coasting Arc #6 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2018/254/22:32:33
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3293787
54 A = 6778209
92 meter
Y = -2684067
07 meter E =
0017814
Z = -5296333
38 I = 51
31407
XDOT = 4608
978082 Wp = 104
13933
YDOT = -6108
032703 meter/sec RA = 305
68534 deg
ZDOT = 225
469051 TA = 168
04426
MA = 168
00192
Ha = 222
692 n
mi
Hp = 213
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10806389
57 X = -3237801
95
Y = -8805994
31 feet Y = -2720588
07 meter
Z = -17376421
84 Z = -5312197
16
XDOT = 15121
319166 XDOT = 4675
842040
YDOT = -20039
477371 feet/sec YDOT = -6056
118027 meter/sec
ZDOT = 739
727859 ZDOT = 248
020992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4433677
80 X = -1351384
99
Y = -13122522
92 feet Y = -3999744
99 meter
Z = -17447221
00 Z = -5317912
96
XDOT = 22457
748068 XDOT = 6845
121611
YDOT = -8722
550157 feet/sec YDOT = -2658
633288 meter/sec
ZDOT = 841
659003 ZDOT = 256
537664
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 18254
95494058
00016717 00000-0 10270-3 0 9056
2 25544 51
6412 306
3102 0004609 148
3325 211
8106 15
53844111 12006
Satellite: ISS
Catalog Number: 25544
Epoch time: 18254
95494058 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 306
3102 deg
Eccentricity:
0004609
Arg of perigee: 148
3325 deg
Mean anomaly: 211
8106 deg
Mean motion: 15
53844111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 276
Coasting Arc #7 (Orbit 1215)
---------------------------------------
Vector Time (GMT): 2018/255/22:32:33
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2266718
38 A = 6779463
96 meter
Y = 3996987
29 meter E =
0007131
Z = 4978336
92 I = 51
30047
XDOT = -5074
346526 Wp = 94
94314
YDOT = 5391
029631 meter/sec RA = 300
66623 deg
ZDOT = -2016
001956 TA = 14
74037
MA = 14
71958
Ha = 222
446 n
mi
Hp = 214
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7436740
10 X = 2197672
26
Y = 13113475
37 feet Y = 4021949
78 meter
Z = 16333126
38 Z = 4989179
77
XDOT = -16648
118522 XDOT = -5124
460666
YDOT = 17687
105090 feet/sec YDOT = 5334
004351 meter/sec
ZDOT = -6614
179647 ZDOT = -2040
773753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -437386
87 X = -133315
52
Y = 15016756
44 feet Y = 4577107
36 meter
Z = 16381241
59 Z = 4993002
44
XDOT = -22230
638746 XDOT = -6775
898690
YDOT = 6696
362001 feet/sec YDOT = 2041
051138 meter/sec
ZDOT = -6725
959801 ZDOT = -2050
072547
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 18255
98396976
00016717 00000-0 10270-3 0 9061
2 25544 51
6415 301
1825 0004471 152
5172 207
6217 15
53877809 12161
Satellite: ISS
Catalog Number: 25544
Epoch time: 18255
98396976 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 301
1825 deg
Eccentricity:
0004471
Arg of perigee: 152
5172 deg
Mean anomaly: 207
6217 deg
Mean motion: 15
53877809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1216
Checksum: 326
Coasting Arc #8 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2018/256/22:32:33
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1271847
72 A = 6782620
42 meter
Y = -5164944
38 meter E =
0011635
Z = -4220990
89 I = 51
29387
XDOT = 5249
909499 Wp = 125
58450
YDOT = -4244
834878 meter/sec RA = 295
65163 deg
ZDOT = 3612
648350 TA = 181
61323
MA = 181
61699
Ha = 222
564 n
mi
Hp = 214
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4172728
73 X = -1193493
88
Y = -16945355
58 feet Y = -5178729
34 meter
Z = -13848395
30 Z = -4226978
35
XDOT = 17224
112531 XDOT = 5279
437794
YDOT = -13926
623617 feet/sec YDOT = -4185
961325 meter/sec
ZDOT = 11852
520834 ZDOT = 3638
222831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4903590
54 X = 1494614
40
Y = -16726782
30 feet Y = -5098323
25 meter
Z = -13874593
57 Z = -4228976
12
XDOT = 20583
616957 XDOT = 6273
886449
YDOT = -3891
699277 feet/sec YDOT = -1186
189939 meter/sec
ZDOT = 11967
744435 ZDOT = 3647
768504
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 18256
94868553
00016717 00000-0 10270-3 0 9074
2 25544 51
6408 296
3753 0004473 155
2075 204
9293 15
53834879 12313
Satellite: ISS
Catalog Number: 25544
Epoch time: 18256
94868553 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 296
3753 deg
Eccentricity:
0004473
Arg of perigee: 155
2075 deg
Mean anomaly: 204
9293 deg
Mean motion: 15
53834879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 341
Coasting Arc #9 (Orbit 1239)
---------------------------------------
Vector Time (GMT): 2018/257/11:39:28
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1595169
42 A = 6782334
33 meter
Y = 5014406
12 meter E =
0011341
Z = 4268469
78 I = 51
28376
XDOT = -5019
760219 Wp = 97
32781
YDOT = 4607
428092 meter/sec RA = 292
91438 deg
ZDOT = -3530
009969 TA = 28
82942
MA = 28
76680
Ha = 222
493 n
mi
Hp = 214
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5233495
47 X = 1518244
28
Y = 16451463
65 feet Y = 5031814
64 meter
Z = 14004165
94 Z = 4276031
36
XDOT = -16469
029589 XDOT = -5053
761647
YDOT = 15116
233899 feet/sec YDOT = 4551
103257 meter/sec
ZDOT = -11581
397535 ZDOT = -3554
477319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1424531
70 X = -434197
26
Y = -17177823
25 feet Y = -5235800
53 meter
Z = 14037446
09 Z = 4278613
57
XDOT = 18043
557348 XDOT = 5499
676280
YDOT = -11068
396484 feet/sec YDOT = -3373
647248 meter/sec
ZDOT = -11691
697340 ZDOT = -3563
629349
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 18257
52751328
00016717 00000-0 10270-3 0 9081
2 25544 51
6390 293
4896 0004734 157
8026 202
3332 15
53859690 12407
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
52751328 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 293
4896 deg
Eccentricity:
0004734
Arg of perigee: 157
8026 deg
Mean anomaly: 202
3332 deg
Mean motion: 15
53859690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1240
Checksum: 322
Coasting Arc #10 (Orbit 1240)
---------------------------------------
Vector Time (GMT): 2018/257/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3756009
91 A = 6778323
85 meter
Y = -2012038
47 meter E =
0017409
Z = -5286343
98 I = 51
26845
XDOT = 3195
624067 Wp = 107
07616
YDOT = -6946
792425 meter/sec RA = 292
48199 deg
ZDOT = 369
489509 TA = 166
49438
MA = 166
44773
Ha = 222
641 n
mi
Hp = 214
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12322867
17 X = -3707553
16
Y = -6601176
07 feet Y = -2053770
25 meter
Z = -17343648
24 Z = -5304471
63
XDOT = 10484
330929 XDOT = 3271
272726
YDOT = -22791
313729 feet/sec YDOT = -6910
633734 meter/sec
ZDOT = 1212
235923 ZDOT = 385
197118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13733265
42 X = 4185899
30
Y = 2002095
47 feet Y = 610238
70 meter
Z = -17424687
94 Z = -5311044
88
XDOT = -1854
012026 XDOT = -565
102866
YDOT = 24002
297665 feet/sec YDOT = 7315
900328 meter/sec
ZDOT = 1283
545981 ZDOT = 391
224815
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 18257
59182790
00016717 00000-0 10270-3 0 9090
2 25544 51
6387 293
1695 0004757 157
1106 203
0259 15
53815190 12418
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
59182790 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 293
1695 deg
Eccentricity:
0004757
Arg of perigee: 157
1106 deg
Mean anomaly: 203
0259 deg
Mean motion: 15
53815190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 322
Coasting Arc #11 (Orbit 1256)
---------------------------------------
Vector Time (GMT): 2018/258/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3042109
30 A = 6779742
30 meter
Y = 3512207
07 meter E =
0007000
Z = 4930738
40 I = 51
26123
XDOT = -3795
389994 Wp = 98
14578
YDOT = 6311
507330 meter/sec RA = 287
45989 deg
ZDOT = -2152
453534 TA = 12
94171
MA = 12
92376
Ha = 222
409 n
mi
Hp = 214
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9980673
57 X = 2978657
68
Y = 11522989
08 feet Y = 3545871
59 meter
Z = 16176963
26 Z = 4945361
65
XDOT = -12452
066909 XDOT = -3855
229399
YDOT = 20707
045047 feet/sec YDOT = 6268
729926 meter/sec
ZDOT = -7061
855426 ZDOT = -2171
036065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13359444
33 X = -4071958
63
Y = -7197674
85 feet Y = -2193851
29 meter
Z = 16242105
37 Z = 4950593
72
XDOT = 3594
690779 XDOT = 1095
661749
YDOT = -22809
630002 feet/sec YDOT = -6952
375225 meter/sec
ZDOT = -7145
968035 ZDOT = -2178
091057
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 18258
62085442
00016717 00000-0 10270-3 0 9103
2 25544 51
6381 288
0414 0004693 160
4839 199
6494 15
53844118 12573
Satellite: ISS
Catalog Number: 25544
Epoch time: 18258
62085442 = yrday
fracday
Element set: 910
Inclination: 51
6381 deg
RA of node: 288
0414 deg
Eccentricity:
0004693
Arg of perigee: 160
4839 deg
Mean anomaly: 199
6494 deg
Mean motion: 15
53844118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1257
Checksum: 330
Coasting Arc #12 (Orbit 1271)
---------------------------------------
Vector Time (GMT): 2018/259/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2327613
82 A = 6782940
18 meter
Y = -4855217
20 meter E =
0011048
Z = -4137520
15 I = 51
26293
XDOT = 4210
281689 Wp = 128
58155
YDOT = -5196
358910 meter/sec RA = 282
44423 deg
ZDOT = 3729
188860 TA = 180
05259
MA = 180
05270
Ha = 222
507 n
mi
Hp = 214
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7636528
30 X = -2253050
48
Y = -15929190
27 feet Y = -4880829
51 meter
Z = -13574541
18 Z = -4148645
56
XDOT = 13813
260134 XDOT = 4249
961403
YDOT = -17048
421621 feet/sec YDOT = -5149
054550 meter/sec
ZDOT = 12234
871587 ZDOT = 3749
737683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12981691
74 X = 3956819
64
Y = 11924364
72 feet Y = 3634546
37 meter
Z = -13623840
91 Z = -4152546
71
XDOT = -5445
385138 XDOT = -1659
753390
YDOT = 20012
786569 feet/sec YDOT = 6099
897346 meter/sec
ZDOT = 12327
655917 ZDOT = 3757
469523
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 18259
58556550
00016717 00000-0 10270-3 0 9113
2 25544 51
6383 283
2349 0004590 162
1696 197
9618 15
53817841 12724
Satellite: ISS
Catalog Number: 25544
Epoch time: 18259
58556550 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 283
2349 deg
Eccentricity:
0004590
Arg of perigee: 162
1696 deg
Mean anomaly: 197
9618 deg
Mean motion: 15
53817841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1272
Checksum: 341
Coasting Arc #13 (Orbit 1287)
---------------------------------------
Vector Time (GMT): 2018/260/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1602907
76 A = 6786433
94 meter
Y = 5896178
11 meter E =
0015339
Z = 2933047
69 I = 51
26756
XDOT = -4510
654763 Wp = 113
45760
YDOT = 3709
763570 meter/sec RA = 277
43640 deg
ZDOT = -4977
772693 TA = 32
84860
MA = 32
75335
Ha = 222
235 n
mi
Hp = 214
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5258883
73 X = 1522608
72
Y = 19344416
37 feet Y = 5913654
11 meter
Z = 9622859
89 Z = 2940638
73
XDOT = -14798
736099 XDOT = -4527
623706
YDOT = 12171
140322 feet/sec YDOT = 3659
227159 meter/sec
ZDOT = -16331
275241 ZDOT = -4999
725323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12359732
51 X = -3767246
47
Y = -15762507
00 feet Y = -4804412
13 meter
Z = 9656195
95 Z = 2943208
53
XDOT = 7596
904421 XDOT = 2315
536468
YDOT = -16051
624043 feet/sec YDOT = -4892
535008 meter/sec
ZDOT = -16430
168828 ZDOT = -5007
915459
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 18260
61458856
00016717 00000-0 10270-3 0 9120
2 25544 51
6369 278
1070 0004432 167
5272 192
5991 15
53860834 12888
Satellite: ISS
Catalog Number: 25544
Epoch time: 18260
61458856 = yrday
fracday
Element set: 912
Inclination: 51
6369 deg
RA of node: 278
1070 deg
Eccentricity:
0004432
Arg of perigee: 167
5272 deg
Mean anomaly: 192
5991 deg
Mean motion: 15
53860834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1288
Checksum: 332
Coasting Arc #14 (Orbit 1302)
---------------------------------------
Vector Time (GMT): 2018/261/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -911551
01 A = 6789168
33 meter
Y = -6561847
13 meter E =
0006261
Z = -1483735
23 I = 51
27338
XDOT = 4689
559018 Wp = 71
21170
YDOT = -1944
297958 meter/sec RA = 272
43776 deg
ZDOT = 5739
536707 TA = 272
51957
MA = 272
59125
Ha = 222
319 n
mi
Hp = 214
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2990652
92 X = -830899
67
Y = -21528369
85 feet Y = -6571589
86 meter
Z = -4867897
74 Z = -1487966
98
XDOT = 15385
692317 XDOT = 4683
072551
YDOT = -6378
930310 feet/sec YDOT = -1891
892012 meter/sec
ZDOT = 18830
501008 ZDOT = 5762
301280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11476777
62 X = 3498121
82
Y = 18453202
92 feet Y = 5624536
25 meter
Z = -4886104
72 Z = -1489284
72
XDOT = -9989
657197 XDOT = -3044
847514
YDOT = 11207
083417 feet/sec YDOT = 3415
919026 meter/sec
ZDOT = 18932
823528 ZDOT = 5770
724611
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 18261
57929802
00016717 00000-0 10270-3 0 9131
2 25544 51
6368 273
3008 0004653 169
4970 190
6280 15
53858274 13039
Satellite: ISS
Catalog Number: 25544
Epoch time: 18261
57929802 = yrday
fracday
Element set: 913
Inclination: 51
6368 deg
RA of node: 273
3008 deg
Eccentricity:
0004653
Arg of perigee: 169
4970 deg
Mean anomaly: 190
6280 deg
Mean motion: 15
53858274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1303
Checksum: 324
Coasting Arc #15 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2018/262/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 190328
84 A = 6790124
82 meter
Y = 6777454
49 meter E =
0015524
Z = -140029
32 I = 51
27690
XDOT = -4801
330659 Wp = 145
69427
YDOT = 18
181644 meter/sec RA = 267
44256 deg
ZDOT = -5983
138868 TA = 35
82232
MA = 35
71831
Ha = 222
137 n
mi
Hp = 214
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 624438
46 X = 115207
51
Y = 22235743
07 feet Y = 6779162
84 meter
Z = -459413
80 Z = -139287
65
XDOT = -15752
397174 XDOT = -4772
114282
YDOT = 59
651062 feet/sec YDOT = -35
347175 meter/sec
ZDOT = -19629
720694 ZDOT = -6006
391032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9980065
86 X = -3041924
08
Y = -19880110
96 feet Y = -6059457
82 meter
Z = -456867
13 Z = -139253
10
XDOT = 12678
911759 XDOT = 3864
532304
YDOT = -5937
024335 feet/sec YDOT = -1809
605017 meter/sec
ZDOT = -19734
007849 ZDOT = -6014
925592
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 18262
60831797
00016717 00000-0 10270-3 0 9142
2 25544 51
6375 268
1722 0004387 173
8108 186
3100 15
53853124 13197
Satellite: ISS
Catalog Number: 25544
Epoch time: 18262
60831797 = yrday
fracday
Element set: 914
Inclination: 51
6375 deg
RA of node: 268
1722 deg
Eccentricity:
0004387
Arg of perigee: 173
8108 deg
Mean anomaly: 186
3100 deg
Mean motion: 15
53853124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 313
Coasting Arc #16 (Orbit 1334)
---------------------------------------
Vector Time (GMT): 2018/263/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 519363
90 A = 6788767
88 meter
Y = -6544288
59 meter E =
0012755
Z = 1714589
20 I = 51
27440
XDOT = 4823
977722 Wp = 83
73614
YDOT = 1873
999458 meter/sec RA = 262
44840 deg
ZDOT = 5656
498076 TA = 295
16352
MA = 295
29576
Ha = 222
048 n
mi
Hp = 214
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1703949
79 X = 584176
81
Y = -21470763
09 feet Y = -6538118
19 meter
Z = 5625292
65 Z = 1717269
98
XDOT = 15826
698564 XDOT = 4775
187442
YDOT = 6148
292186 feet/sec YDOT = 1927
672135 meter/sec
ZDOT = 18558
064555 ZDOT = 5679
812546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7923362
11 X = 2415040
77
Y = 20024328
60 feet Y = 6103415
36 meter
Z = 5638051
70 Z = 1718478
16
XDOT = -15348
744507 XDOT = -4678
297326
YDOT = 786
437008 feet/sec YDOT = 239
706000 meter/sec
ZDOT = 18662
423112 ZDOT = 5688
306565
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 18263
63733444
00016717 00000-0 10270-3 0 9157
2 25544 51
6366 263
0454 0004584 179
1541 180
9620 15
53891948 13353
Satellite: ISS
Catalog Number: 25544
Epoch time: 18263
63733444 = yrday
fracday
Element set: 915
Inclination: 51
6366 deg
RA of node: 263
0454 deg
Eccentricity:
0004584
Arg of perigee: 179
1541 deg
Mean anomaly: 180
9620 deg
Mean motion: 15
53891948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1335
Checksum: 324
Coasting Arc #17 (Orbit 1349)
---------------------------------------
Vector Time (GMT): 2018/264/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1295779
58 A = 6785862
57 meter
Y = 5859743
83 meter E =
0006758
Z = -3164958
33 I = 51
26985
XDOT = -4749
295594 Wp = 140
94451
YDOT = -3634
423508 meter/sec RA = 257
44733 deg
ZDOT = -4795
266114 TA = 75
78061
MA = 75
70555
Ha = 221
930 n
mi
Hp = 214
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4251245
33 X = -1345834
92
Y = 19224881
32 feet Y = 5844973
36 meter
Z = -10383721
55 Z = -3171374
85
XDOT = -15581
678459 XDOT = -4685
008707
YDOT = -11923
961640 feet/sec YDOT = -3687
174402 meter/sec
ZDOT = -15732
500375 ZDOT = -4818
179981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5005269
92 X = -1525606
27
Y = -19026416
47 feet Y = -5799251
74 meter
Z = -10413144
15 Z = -3173926
34
XDOT = 17817
091101 XDOT = 5430
649368
YDOT = 3960
011761 feet/sec YDOT = 1207
011585 meter/sec
ZDOT = -15834
878914 ZDOT = -4826
471093
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 18264
60204009
00016717 00000-0 10270-3 0 9166
2 25544 51
6367 258
2375 0004328 182
5350 177
5781 15
53851189 13504
Satellite: ISS
Catalog Number: 25544
Epoch time: 18264
60204009 = yrday
fracday
Element set: 916
Inclination: 51
6367 deg
RA of node: 258
2375 deg
Eccentricity:
0004328
Arg of perigee: 182
5350 deg
Mean anomaly: 177
5781 deg
Mean motion: 15
53851189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1350
Checksum: 314
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