[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 7th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16271 6957 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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
187/16:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 217
2
190/22:57:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 217
3
Coasting Arc #1 (Orbit 1808)
---------------------------------------
Vector Time (GMT): 2019/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -926620
03 A = 6797944
95 meter
Y = 6618005
86 meter E =
0015752
Z = -1221521
92 I = 51
27447
XDOT = -4680
054521 Wp = 129
03119
YDOT = -1718
168124 meter/sec RA = 269
54178 deg
ZDOT = -5819
009079 TA = 64
29443
MA = 64
13186
Ha = 228
540 n
mi
Hp = 217
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3040091
96 X = -994622
24
Y = 21712617
64 feet Y = 6607263
70 meter
Z = -4007617
85 Z = -1226187
16
XDOT = -15354
509584 XDOT = -4632
228702
YDOT = -5637
034527 feet/sec YDOT = -1770
235483 meter/sec
ZDOT = -19091
237136 ZDOT = -5841
626680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21855610
06 X = 6661589
95
Y = -1684316
47 feet Y = -513379
66 meter
Z = -4029430
67 Z = -1228170
47
XDOT = -2386
070838 XDOT = -727
274391
YDOT = 14484
023279 feet/sec YDOT = 4414
730295 meter/sec
ZDOT = -19193
639903 ZDOT = -5850
221442
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 19186
52989687
00016717 00000-0 10270-3 0 9006
2 25544 51
6419 270
2719 0007197 112
6297 247
5616 15
50949612 18099
Satellite: ISS
Catalog Number: 25544
Epoch time: 19186
52989687 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 270
2719 deg
Eccentricity:
0007197
Arg of perigee: 112
6297 deg
Mean anomaly: 247
5616 deg
Mean motion: 15
50949612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1809
Checksum: 349
Coasting Arc #2 (Orbit 1824)
---------------------------------------
Vector Time (GMT): 2019/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 852990
24 A = 6797150
38 meter
Y = -6485145
52 meter E =
0019352
Z = 1825678
53 I = 51
27338
XDOT = 4729
901472 Wp = 82
42436
YDOT = 2215
108958 meter/sec RA = 264
55932 deg
ZDOT = 5609
786166 TA = 297
73313
MA = 297
92928
Ha = 228
502 n
mi
Hp = 217
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2798524
40 X = 916577
64
Y = -21276724
15 feet Y = -6475251
47 meter
Z = 5989758
94 Z = 1829975
59
XDOT = 15518
049450 XDOT = 4677
531270
YDOT = 7267
417840 feet/sec YDOT = 2267
708520 meter/sec
ZDOT = 18404
810257 ZDOT = 5632
634886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21340454
01 X = -6504570
38
Y = 2207815
44 feet Y = 672942
15 meter
Z = 6009868
17 Z = 1831807
82
XDOT = 3695
338838 XDOT = 1126
339278
YDOT = -15096
646372 feet/sec YDOT = -4601
457814 meter/sec
ZDOT = 18508
224554 ZDOT = 5641
306844
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 19187
56083456
00016717 00000-0 10270-3 0 9011
2 25544 51
6420 265
1574 0007153 115
8194 244
3696 15
50957651 18259
Satellite: ISS
Catalog Number: 25544
Epoch time: 19187
56083456 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 265
1574 deg
Eccentricity:
0007153
Arg of perigee: 115
8194 deg
Mean anomaly: 244
3696 deg
Mean motion: 15
50957651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1825
Checksum: 324
Coasting Arc #3 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2019/187/16:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4133531
30 A = 6786678
71 meter
Y = -1076846
16 meter E =
0010011
Z = 5266160
61 I = 51
23648
XDOT = 1284
141855 Wp = 113
58192
YDOT = 7543
626775 meter/sec RA = 263
52652 deg
ZDOT = 529
856388 TA = 331
30803
MA = 331
36307
Ha = 228
392 n
mi
Hp = 217
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13561454
40 X = 4119686
11
Y = -3532959
85 feet Y = -1030700
15 meter
Z = 17277429
81 Z = 5286205
61
XDOT = 4213
063829 XDOT = 1197
117722
YDOT = 24749
431677 feet/sec YDOT = 7557
500305 meter/sec
ZDOT = 1738
373977 ZDOT = 535
883680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13599217
90 X = -4145041
62
Y = 2881469
72 feet Y = 878271
97 meter
Z = 17368443
69 Z = 5293901
64
XDOT = -2796
707518 XDOT = -852
436452
YDOT = -23931
210555 feet/sec YDOT = -7294
232977 meter/sec
ZDOT = 1764
993058 ZDOT = 537
969884
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 19187
75413487
00016717 00000-0 10270-3 0 9024
2 25544 51
6394 264
1994 0007200 114
1621 246
0283 15
50960296 18287
Satellite: ISS
Catalog Number: 25544
Epoch time: 19187
75413487 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 264
1994 deg
Eccentricity:
0007200
Arg of perigee: 114
1621 deg
Mean anomaly: 246
0283 deg
Mean motion: 15
50960296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 315
Coasting Arc #4 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2019/188/16:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4221137
66 A = 6786672
70 meter
Y = 592868
69 meter E =
0021586
Z = -5299683
82 I = 51
24147
XDOT = -1342
567663 Wp = 99
94677
YDOT = -7525
239035 meter/sec RA = 258
53251 deg
ZDOT = 224
630548 TA = 172
22875
MA = 172
19525
Ha = 228
550 n
mi
Hp = 217
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13848876
85 X = -4201711
07
Y = 1945107
26 feet Y = 545774
11 meter
Z = -17387414
11 Z = -5320140
96
XDOT = -4404
749552 XDOT = -1259
409615
YDOT = -24689
104445 feet/sec YDOT = -7539
787624 meter/sec
ZDOT = 736
976863 ZDOT = 218
310203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13785149
09 X = 4201713
44
Y = -1519017
51 feet Y = -462996
54 meter
Z = -17480253
20 Z = -5327981
17
XDOT = 3534
411547 XDOT = 1077
288639
YDOT = 23808
211154 feet/sec YDOT = 7256
742760 meter/sec
ZDOT = 709
002586 ZDOT = 216
103988
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 19188
72063648
00016717 00000-0 10270-3 0 9033
2 25544 51
6397 259
4045 0007230 116
8414 243
3477 15
50942295 18437
Satellite: ISS
Catalog Number: 25544
Epoch time: 19188
72063648 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 259
4045 deg
Eccentricity:
0007230
Arg of perigee: 116
8414 deg
Mean anomaly: 243
3477 deg
Mean motion: 15
50942295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 324
Coasting Arc #5 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2019/189/16:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4328234
02 A = 6786875
60 meter
Y = -130801
15 meter E =
0009298
Z = 5217793
42 I = 51
24885
XDOT = 1396
961858 Wp = 100
74015
YDOT = 7479
640640 meter/sec RA = 253
53888 deg
ZDOT = -971
523432 TA = 358
60492
MA = 358
60751
Ha = 228
287 n
mi
Hp = 217
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14200242
85 X = 4304030
16
Y = -429137
64 feet Y = -82535
59 meter
Z = 17118744
82 Z = 5238759
31
XDOT = 4583
208195 XDOT = 1317
937613
YDOT = 24539
503413 feet/sec YDOT = 7494
820681 meter/sec
ZDOT = -3187
412835 ZDOT = -964
928874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14089372
01 X = -4294440
59
Y = 235277
14 feet Y = 71712
47 meter
Z = 17213852
60 Z = 5246782
27
XDOT = -4251
267289 XDOT = -1295
786270
YDOT = -23572
569470 feet/sec YDOT = -7184
919174 meter/sec
ZDOT = -3158
169352 ZDOT = -962
610019
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 19189
75156909
00016717 00000-0 10270-3 0 9041
2 25544 51
6384 254
2895 0007090 120
3202 239
8651 15
50964498 18598
Satellite: ISS
Catalog Number: 25544
Epoch time: 19189
75156909 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 254
2895 deg
Eccentricity:
0007090
Arg of perigee: 120
3202 deg
Mean anomaly: 239
8651 deg
Mean motion: 15
50964498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 343
Coasting Arc #6 (Orbit 1873)
---------------------------------------
Vector Time (GMT): 2019/190/16:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4506022
16 A = 6787604
87 meter
Y = -313268
65 meter E =
0020153
Z = -5084756
08 I = 51
26162
XDOT = -1411
340383 Wp = 110
07734
YDOT = -7321
568009 meter/sec RA = 248
54677 deg
ZDOT = 1700
518639 TA = 176
49245
MA = 176
47830
Ha = 228
446 n
mi
Hp = 217
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14783537
28 X = -4477485
48
Y = -1027784
29 feet Y = -363498
14 meter
Z = -16682270
61 Z = -5106575
20
XDOT = -4630
381833 XDOT = -1337
623727
YDOT = -24020
892417 feet/sec YDOT = -7336
938585 meter/sec
ZDOT = 5579
129394 ZDOT = 1693
841311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14674581
71 X = 4472812
50
Y = 977220
10 feet Y = 297856
69 meter
Z = -16781214
51 Z = -5114914
18
XDOT = 4823
629674 XDOT = 1470
242325
YDOT = 22933
842804 feet/sec YDOT = 6990
235287 meter/sec
ZDOT = 5549
478427 ZDOT = 1691
481024
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 19190
71806846
00016717 00000-0 10270-3 0 9052
2 25544 51
6385 249
4947 0007101 123
4777 236
7054 15
50942633 18744
Satellite: ISS
Catalog Number: 25544
Epoch time: 19190
71806846 = yrday
fracday
Element set: 905
Inclination: 51
6385 deg
RA of node: 249
4947 deg
Eccentricity:
0007101
Arg of perigee: 123
4777 deg
Mean anomaly: 236
7054 deg
Mean motion: 15
50942633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1874
Checksum: 330
Coasting Arc #7 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2019/190/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2872077
76 A = 6787776
04 meter
Y = 3572788
35 meter E =
0018167
Z = -5021608
25 I = 51
26963
XDOT = -4216
373654 Wp = 92
29777
YDOT = -6086
032480 meter/sec RA = 247
32415 deg
ZDOT = -1925
359477 TA = 158
91821
MA = 158
84323
Ha = 228
274 n
mi
Hp = 217
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9422827
31 X = -2887424
24
Y = 11721746
55 feet Y = 3540585
42 meter
Z = -16475092
68 Z = -5035596
57
XDOT = -13833
246895 XDOT = -4138
652264
YDOT = -19967
298163 feet/sec YDOT = -6132
748183 meter/sec
ZDOT = -6316
796186 ZDOT = -1945
652697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11873355
63 X = -3618998
80
Y = -9116328
26 feet Y = -2778656
85 meter
Z = -16538853
67 Z = -5041042
60
XDOT = 19071
663493 XDOT = 5813
043033
YDOT = -13253
675804 feet/sec YDOT = -4039
720385 meter/sec
ZDOT = -6408
320472 ZDOT = -1953
256080
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 19190
97580125
00016717 00000-0 10270-3 0 9060
2 25544 51
6425 248
2172 0006901 124
4552 235
7252 15
50988453 18788
Satellite: ISS
Catalog Number: 25544
Epoch time: 19190
97580125 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 248
2172 deg
Eccentricity:
0006901
Arg of perigee: 124
4552 deg
Mean anomaly: 235
7252 deg
Mean motion: 15
50988453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 322
Coasting Arc #8 (Orbit 1893)
---------------------------------------
Vector Time (GMT): 2019/191/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3038412
12 A = 6787023
48 meter
Y = -3149793
93 meter E =
0011021
Z = 5181088
72 I = 51
28173
XDOT = 4347
500831 Wp = 127
11371
YDOT = 6200
506372 meter/sec RA = 242
33326 deg
ZDOT = 1211
654792 TA = 311
15597
MA = 311
25100
Ha = 228
161 n
mi
Hp = 217
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9968543
71 X = 3048241
46
Y = -10333969
59 feet Y = -3115761
87 meter
Z = 16998322
56 Z = 5195871
66
XDOT = 14263
454170 XDOT = 4271
956358
YDOT = 20342
868676 feet/sec YDOT = 6248
700651 meter/sec
ZDOT = 3975
245381 ZDOT = 1232
590416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10659699
42 X = 3249076
38
Y = 9499481
07 feet Y = 2895441
83 meter
Z = 17065650
55 Z = 5201610
29
XDOT = -19158
070638 XDOT = -5839
379930
YDOT = 14137
943162 feet/sec YDOT = 4309
245076 meter/sec
ZDOT = 4069
691568 ZDOT = 1240
441990
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 19192
00673021
00016717 00000-0 10270-3 0 9075
2 25544 51
6432 243
1024 0006909 128
6475 231
5295 15
50985163 18948
Satellite: ISS
Catalog Number: 25544
Epoch time: 19192
00673021 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 243
1024 deg
Eccentricity:
0006909
Arg of perigee: 128
6475 deg
Mean anomaly: 231
5295 deg
Mean motion: 15
50985163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1894
Checksum: 307
Coasting Arc #9 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2019/192/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3291566
12 A = 6786578
80 meter
Y = 2721291
86 meter E =
0020136
Z = -5291260
23 I = 51
29630
XDOT = -4422
409975 Wp = 100
29286
YDOT = -6224
187747 meter/sec RA = 237
34244 deg
ZDOT = -455
031645 TA = 165
36438
MA = 165
30600
Ha = 228
162 n
mi
Hp = 217
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10799101
44 X = -3296049
85
Y = 8928122
90 feet Y = 2684458
85 meter
Z = -17359777
67 Z = -5307259
92
XDOT = -14509
219079 XDOT = -4350
270360
YDOT = -20420
563475 feet/sec YDOT = -6273
238823 meter/sec
ZDOT = -1492
885973 ZDOT = -476
339547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9459676
20 X = -2883309
31
Y = -10213380
17 feet Y = -3113038
28 meter
Z = -17432591
40 Z = -5313453
86
XDOT = 18910
567969 XDOT = 5763
941117
YDOT = -14830
761409 feet/sec YDOT = -4520
416078 meter/sec
ZDOT = -1589
037535 ZDOT = -484
338641
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 19192
97322422
00016717 00000-0 10270-3 0 9088
2 25544 51
6427 238
3073 0006806 131
1140 229
0600 15
50994354 19097
Satellite: ISS
Catalog Number: 25544
Epoch time: 19192
97322422 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 238
3073 deg
Eccentricity:
0006806
Arg of perigee: 131
1140 deg
Mean anomaly: 229
0600 deg
Mean motion: 15
50994354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1909
Checksum: 299
Coasting Arc #10 (Orbit 1924)
---------------------------------------
Vector Time (GMT): 2019/193/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3553734
51 A = 6786499
60 meter
Y = -2324692
73 meter E =
0008442
Z = 5287246
54 I = 51
31428
XDOT = 4492
642231 Wp = 121
21055
YDOT = 6208
992346 meter/sec RA = 232
35351 deg
ZDOT = -293
638729 TA = 331
57784
MA = 331
62385
Ha = 228
005 n
mi
Hp = 217
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11659233
94 X = 3553783
40
Y = -7626944
66 feet Y = -2284952
87 meter
Z = 17346609
39 Z = 5304508
95
XDOT = 14739
639864 XDOT = 4424
303923
YDOT = 20370
709796 feet/sec YDOT = 6258
850162 meter/sec
ZDOT = -963
381657 ZDOT = -271
980358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8394406
93 X = 2558615
23
Y = 10995992
74 feet Y = 3351578
59 meter
Z = 17425124
22 Z = 5311177
86
XDOT = -18516
891672 XDOT = -5643
948582
YDOT = 15487
193108 feet/sec YDOT = 4720
496459 meter/sec
ZDOT = -865
618587 ZDOT = -263
840545
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 19194
00414985
00016717 00000-0 10270-3 0 9091
2 25544 51
6419 233
1931 0006825 135
6072 224
5627 15
50996120 19258
Satellite: ISS
Catalog Number: 25544
Epoch time: 19194
00414985 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 233
1931 deg
Eccentricity:
0006825
Arg of perigee: 135
6072 deg
Mean anomaly: 224
5627 deg
Mean motion: 15
50996120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1925
Checksum: 313
Coasting Arc #11 (Orbit 1939)
---------------------------------------
Vector Time (GMT): 2019/194/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3885960
05 A = 6786848
08 meter
Y = 1953918
70 meter E =
0019852
Z = -5227096
84 I = 51
33618
XDOT = -4484
168749 Wp = 111
05704
YDOT = -6107
288213 meter/sec RA = 227
36508 deg
ZDOT = 1046
952795 TA = 169
06077
MA = 169
01754
Ha = 228
027 n
mi
Hp = 217
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12749212
77 X = -3882130
40
Y = 6410494
44 feet Y = 1910485
40 meter
Z = -17149267
86 Z = -5245963
62
XDOT = -14711
839729 XDOT = -4420
627503
YDOT = -20037
034821 feet/sec YDOT = -6157
078216 meter/sec
ZDOT = 3434
884498 ZDOT = 1025
323933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7463365
96 X = -2274833
95
Y = -12041005
57 feet Y = -3670098
50 meter
Z = -17235040
09 Z = -5253240
22
XDOT = 17829
228682 XDOT = 5434
348902
YDOT = -15845
402874 feet/sec YDOT = -4829
678796 meter/sec
ZDOT = 3337
224927 ZDOT = 1017
186158
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 19194
97064212
00016717 00000-0 10270-3 0 9103
2 25544 51
6415 228
3978 0006713 139
1561 221
0094 15
50994218 19402
Satellite: ISS
Catalog Number: 25544
Epoch time: 19194
97064212 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 228
3978 deg
Eccentricity:
0006713
Arg of perigee: 139
1561 deg
Mean anomaly: 221
0094 deg
Mean motion: 15
50994218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1940
Checksum: 309
Coasting Arc #12 (Orbit 1955)
---------------------------------------
Vector Time (GMT): 2019/195/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216888
38 A = 6787443
32 meter
Y = -1624260
59 meter E =
0008598
Z = 5056665
37 I = 51
36206
XDOT = 4447
039831 Wp = 105
59110
YDOT = 5988
860447 meter/sec RA = 222
37917 deg
ZDOT = -1784
544362 TA = 1
74014
MA = 1
73715
Ha = 227
763 n
mi
Hp = 217
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13834935
62 X = 4210175
75
Y = -5328938
94 feet Y = -1577142
74 meter
Z = 16590109
48 Z = 5077132
62
XDOT = 14590
025691 XDOT = 4388
408385
YDOT = 19648
492280 feet/sec YDOT = 6038
262826 meter/sec
ZDOT = -5854
804337 ZDOT = -1763
083998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6705115
46 X = 2043719
19
Y = 13105319
99 feet Y = 3994501
53 meter
Z = 16683128
63 Z = 5085017
61
XDOT = -17091
072177 XDOT = -5209
358800
YDOT = 16075
273699 feet/sec YDOT = 4899
743423 meter/sec
ZDOT = -5757
876103 ZDOT = -1755
000636
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 19196
00156300
00016717 00000-0 10270-3 0 9110
2 25544 51
6417 223
2829 0006587 143
3862 216
7740 15
51014033 19568
Satellite: ISS
Catalog Number: 25544
Epoch time: 19196
00156300 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 223
2829 deg
Eccentricity:
0006587
Arg of perigee: 143
3862 deg
Mean anomaly: 216
7740 deg
Mean motion: 15
51014033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1956
Checksum: 292
Coasting Arc #13 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2019/196/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4593244
46 A = 6788508
09 meter
Y = 1344825
66 meter E =
0017401
Z = -4830804
41 I = 51
38898
XDOT = -4318
634118 Wp = 121
74101
YDOT = -5802
677289 meter/sec RA = 217
39448 deg
ZDOT = 2488
551477 TA = 172
87468
MA = 172
84991
Ha = 227
899 n
mi
Hp = 217
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15069699
66 X = -4584476
32
Y = 4412157
67 feet Y = 1293510
57 meter
Z = -15849095
84 Z = -4853094
81
XDOT = -14168
747105 XDOT = -4265
513756
YDOT = -19037
655148 feet/sec YDOT = -5850
674665 meter/sec
ZDOT = 8164
538966 ZDOT = 2467
701597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6167537
04 X = -1879865
29
Y = -14328422
14 feet Y = -4367303
07 meter
Z = -15950380
18 Z = -4861675
88
XDOT = 16156
157435 XDOT = 4924
396786
YDOT = -15946
612259 feet/sec YDOT = -4860
527417 meter/sec
ZDOT = 8070
342188 ZDOT = 2459
840299
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 19196
96805139
00016717 00000-0 10270-3 0 9127
2 25544 51
6399 218
4866 0006648 146
0859 214
0719 15
50994996 19716
Satellite: ISS
Catalog Number: 25544
Epoch time: 19196
96805139 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 218
4866 deg
Eccentricity:
0006648
Arg of perigee: 146
0859 deg
Mean anomaly: 214
0719 deg
Mean motion: 15
50994996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 367
Coasting Arc #14 (Orbit 1986)
---------------------------------------
Vector Time (GMT): 2019/197/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4950351
45 A = 6789672
41 meter
Y = -1110056
72 meter E =
0011553
Z = 4501268
70 I = 51
42027
XDOT = 4144
604052 Wp = 101
85979
YDOT = 5624
002137 meter/sec RA = 212
41481 deg
ZDOT = -3166
598974 TA = 20
03986
MA = 19
99454
Ha = 227
607 n
mi
Hp = 218
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16241310
54 X = 4940532
27
Y = -3641918
38 feet Y = -1054753
99 meter
Z = 14767941
92 Z = 4525291
18
XDOT = 13597
782324 XDOT = 4096
788096
YDOT = 18451
450582 feet/sec YDOT = 5670
083119 meter/sec
ZDOT = -10389
104244 ZDOT = -3146
581729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5811127
30 X = 1771231
60
Y = 15493191
81 feet Y = 4722324
86 meter
Z = 14877084
83 Z = 4534535
46
XDOT = -15281
703921 XDOT = -4657
863355
YDOT = 15635
205520 feet/sec YDOT = 4765
610642 meter/sec
ZDOT = -10298
648738 ZDOT = -3139
028135
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 19197
99896962
00016717 00000-0 10270-3 0 9136
2 25544 51
6398 213
3724 0006529 150
5951 209
5569 15
51019836 19874
Satellite: ISS
Catalog Number: 25544
Epoch time: 19197
99896962 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 213
3724 deg
Eccentricity:
0006529
Arg of perigee: 150
5951 deg
Mean anomaly: 209
5569 deg
Mean motion: 15
51019836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1987
Checksum: 364
Coasting Arc #15 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2019/198/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5323374
51 A = 6791150
14 meter
Y = 939983
98 meter E =
0013200
Z = -4125484
03 I = 51
45307
XDOT = -3881
269182 Wp = 130
73917
YDOT = -5405
112358 meter/sec RA = 207
43645 deg
ZDOT = 3776
235752 TA = 178
39164
MA = 178
38739
Ha = 227
738 n
mi
Hp = 218
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17465139
45 X = -5313451
16
Y = 3083936
95 feet Y = 880510
30 meter
Z = -13535052
59 Z = -4151318
21
XDOT = -12733
822774 XDOT = -3838
881661
YDOT = -17733
308262 feet/sec YDOT = -5448
278924 meter/sec
ZDOT = 12389
224907 ZDOT = 3757
484647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5714718
42 X = -1741846
17
Y = -16694093
19 feet Y = -5088359
61 meter
Z = -13652423
14 Z = -4161258
57
XDOT = 14336
334924 XDOT = 4369
714885
YDOT = -14971
453032 feet/sec YDOT = -4563
298884 meter/sec
ZDOT = 12304
477966 ZDOT = 3750
404884
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 19198
96545543
00016717 00000-0 10270-3 0 9141
2 25544 51
6392 208
5759 0006640 154
6502 205
4976 15
50998546 20022
Satellite: ISS
Catalog Number: 25544
Epoch time: 19198
96545543 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 208
5759 deg
Eccentricity:
0006640
Arg of perigee: 154
6502 deg
Mean anomaly: 205
4976 deg
Mean motion: 15
50998546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 337
Coasting Arc #16 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2019/199/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5657572
13 A = 6792601
34 meter
Y = -807744
73 meter E =
0014964
Z = 3654517
73 I = 51
48888
XDOT = 3561
274970 Wp = 109
82633
YDOT = 5218
348668 meter/sec RA = 202
46244 deg
ZDOT = -4350
282091 TA = 26
66293
MA = 26
58606
Ha = 227
451 n
mi
Hp = 218
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18561588
34 X = 5648432
86
Y = -2650081
15 feet Y = -744529
30 meter
Z = 11989887
55 Z = 3681977
19
XDOT = 11683
972998 XDOT = 3523
787995
YDOT = 17120
566496 feet/sec YDOT = 5257
964228 meter/sec
ZDOT = -14272
579038 ZDOT = -4333
073603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5762411
41 X = 1756383
00
Y = 17757897
01 feet Y = 5412607
01 meter
Z = 12114644
18 Z = 3692543
55
XDOT = -13564
770441 XDOT = -4134
542030
YDOT = 14106
757687 feet/sec YDOT = 4299
739743 meter/sec
ZDOT = -14194
801834 ZDOT = -4326
575599
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 19199
99636908
00016717 00000-0 10270-3 0 9152
2 25544 51
6398 203
4603 0006473 158
2235 201
9192 15
51023146 20181
Satellite: ISS
Catalog Number: 25544
Epoch time: 19199
99636908 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 203
4603 deg
Eccentricity:
0006473
Arg of perigee: 158
2235 deg
Mean anomaly: 201
9192 deg
Mean motion: 15
51023146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2018
Checksum: 317
Coasting Arc #17 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2019/200/22:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5978517
48 A = 6794150
67 meter
Y = 743438
73 meter E =
0008608
Z = -3153155
93 I = 51
52314
XDOT = -3169
014940 Wp = 130
11056
YDOT = -5021
843811 meter/sec RA = 197
49216 deg
ZDOT = 4827
891647 TA = 193
56696
MA = 193
59012
Ha = 227
632 n
mi
Hp = 218
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19614558
68 X = -5971070
56
Y = 2439103
46 feet Y = 676624
69 meter
Z = -10344999
78 Z = -3182178
54
XDOT = -10397
030642 XDOT = -3136
074415
YDOT = -16475
865523 feet/sec YDOT = -5057
098229 meter/sec
ZDOT = 15839
539524 ZDOT = 4812
577633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6059370
61 X = -1846896
16
Y = -18740823
13 feet Y = -5712202
89 meter
Z = -10476866
63 Z = -3193348
95
XDOT = 12846
937543 XDOT = 3915
746563
YDOT = -12963
935967 feet/sec YDOT = -3951
407683 meter/sec
ZDOT = 15770
333530 ZDOT = 4806
797660
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 19200
96285162
00016717 00000-0 10270-3 0 9165
2 25544 51
6379 198
6646 0006716 161
2548 198
8851 15
50995132 20338
Satellite: ISS
Catalog Number: 25544
Epoch time: 19200
96285162 = yrday
fracday
Element set: 916
Inclination: 51
6379 deg
RA of node: 198
6646 deg
Eccentricity:
0006716
Arg of perigee: 161
2548 deg
Mean anomaly: 198
8851 deg
Mean motion: 15
50995132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2033
Checksum: 337
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