[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 13th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
107/20:46:03
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 217
2
109/09:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 217
4
114/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 217
1
116/09:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 504)
---------------------------------------
Vector Time (GMT): 2019/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6061770
64 A = 6790649
95 meter
Y = -1297012
67 meter E =
0013119
Z = 2759306
11 I = 51
44496
XDOT = -1142
026171 Wp = 84
94606
YDOT = 5593
671356 meter/sec RA = 327
14369 deg
ZDOT = 5118
265096 TA = 306
38713
MA = 306
50808
Ha = 223
458 n
mi
Hp = 217
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19887698
96 X = 6062420
48
Y = -4255290
91 feet Y = -1229222
06 meter
Z = 9052841
56 Z = 2788753
56
XDOT = -3746
805024 XDOT = -1229
353058
YDOT = 18351
940144 feet/sec YDOT = 5580
412171 meter/sec
ZDOT = 16792
208319 ZDOT = 5112
505419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17266178
08 X = 5262731
08
Y = -10633729
72 feet Y = -3241160
82 meter
Z = 9186125
27 Z = 2799930
98
XDOT = 1718
319842 XDOT = 523
743888
YDOT = 17328
811341 feet/sec YDOT = 5281
821697 meter/sec
ZDOT = 16765
513424 ZDOT = 5110
128491
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 19102
55869405
00016717 00000-0 10270-3 0 9002
2 25544 51
6418 327
4592 0001297 185
2699 174
8440 15
52535132 5058
Satellite: ISS
Catalog Number: 25544
Epoch time: 19102
55869405 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 327
4592 deg
Eccentricity:
0001297
Arg of perigee: 185
2699 deg
Mean anomaly: 174
8440 deg
Mean motion: 15
52535132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 505
Checksum: 314
Coasting Arc #2 (Orbit 519)
---------------------------------------
Vector Time (GMT): 2019/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5650205
71 A = 6788010
32 meter
Y = 637995
70 meter E =
0005457
Z = -3712190
38 I = 51
40830
XDOT = 2133
284344 Wp = 90
04517
YDOT = -5983
340070 meter/sec RA = 322
15766 deg
ZDOT = -4280
801868 TA = 134
33450
MA = 134
28976
Ha = 223
415 n
mi
Hp = 217
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18537420
32 X = -5638888
29
Y = 2093161
75 feet Y = 574874
37 meter
Z = -12179102
29 Z = -3739609
45
XDOT = 6998
964384 XDOT = 2220
826937
YDOT = -19630
380807 feet/sec YDOT = -5958
994778 meter/sec
ZDOT = -14044
625550 ZDOT = -4270
226466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16553689
80 X = -5045564
65
Y = 8423541
43 feet Y = 2567495
43 meter
Z = -12303134
35 Z = -3749995
35
XDOT = 382
328599 XDOT = 116
533757
YDOT = -19664
962302 feet/sec YDOT = -5993
880510 meter/sec
ZDOT = -13996
124326 ZDOT = -4266
018694
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 19103
52421128
00016717 00000-0 10270-3 0 9017
2 25544 51
6413 322
6570 0001307 191
9417 168
1704 15
52537619 5208
Satellite: ISS
Catalog Number: 25544
Epoch time: 19103
52421128 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 322
6570 deg
Eccentricity:
0001307
Arg of perigee: 191
9417 deg
Mean anomaly: 168
1704 deg
Mean motion: 15
52537619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 520
Checksum: 279
Coasting Arc #3 (Orbit 535)
---------------------------------------
Vector Time (GMT): 2019/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5116539
60 A = 6785479
37 meter
Y = 106222
88 meter E =
0009378
Z = 4450939
43 I = 51
37320
XDOT = -2962
515531 Wp = 118
38018
YDOT = 6283
586660 meter/sec RA = 317
16544 deg
ZDOT = 3245
973164 TA = 298
76199
MA = 298
85617
Ha = 223
385 n
mi
Hp = 217
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16786547
23 X = 5093351
38
Y = 348500
27 feet Y = 163310
11 meter
Z = 14602819
67 Z = 4475737
27
XDOT = -9719
539144 XDOT = -3048
327295
YDOT = 20615
441798 feet/sec YDOT = 6249
978046 meter/sec
ZDOT = 10649
518253 ZDOT = 3231
373779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15656509
92 X = 4772104
23
Y = -5787660
81 feet Y = -1764079
02 meter
Z = 14714912
23 Z = 4485105
25
XDOT = -1980
663588 XDOT = -603
706262
YDOT = 21627
873406 feet/sec YDOT = 6592
175814 meter/sec
ZDOT = 10582
805450 ZDOT = 3225
639101
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 19104
55409374
00016717 00000-0 10270-3 0 9021
2 25544 51
6404 317
5353 0001208 188
1065 172
0067 15
52523121 5363
Satellite: ISS
Catalog Number: 25544
Epoch time: 19104
55409374 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 317
5353 deg
Eccentricity:
0001208
Arg of perigee: 188
1065 deg
Mean anomaly: 172
0067 deg
Mean motion: 15
52523121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 536
Checksum: 278
Coasting Arc #4 (Orbit 550)
---------------------------------------
Vector Time (GMT): 2019/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4503753
60 A = 6783250
95 meter
Y = -972765
59 meter E =
0012068
Z = -4989177
68 I = 51
34126
XDOT = 3632
519038 Wp = 80
06326
YDOT = -6427
664818 meter/sec RA = 312
16614 deg
ZDOT = -2028
017353 TA = 170
12059
MA = 170
09684
Ha = 223
340 n
mi
Hp = 217
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14776094
48 X = -4468306
53
Y = -3191488
15 feet Y = -1022931
79 meter
Z = -16368693
18 Z = -5010969
03
XDOT = 11917
713380 XDOT = 3713
975999
YDOT = -21088
139167 feet/sec YDOT = -6386
588105 meter/sec
ZDOT = -6653
600240 ZDOT = -2010
173779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14772729
85 X = -4502728
06
Y = 2655926
69 feet Y = 809526
45 meter
Z = -16467094
08 Z = -5019170
28
XDOT = 3186
280317 XDOT = 971
178241
YDOT = -22982
308532 feet/sec YDOT = -7005
007640 meter/sec
ZDOT = -6572
222915 ZDOT = -2003
213545
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 19105
51960183
00016717 00000-0 10270-3 0 9039
2 25544 51
6392 312
7333 0001340 199
7596 160
3505 15
52561278 5517
Satellite: ISS
Catalog Number: 25544
Epoch time: 19105
51960183 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 312
7333 deg
Eccentricity:
0001340
Arg of perigee: 199
7596 deg
Mean anomaly: 160
3505 deg
Mean motion: 15
52561278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 551
Checksum: 300
Coasting Arc #5 (Orbit 566)
---------------------------------------
Vector Time (GMT): 2019/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3846246
29 A = 6782133
09 meter
Y = 1890718
83 meter E =
0003426
Z = 5254616
28 I = 51
31609
XDOT = -4139
430023 Wp = 138
46517
YDOT = 6414
277200 meter/sec RA = 307
16202 deg
ZDOT = 719
180497 TA = 304
61773
MA = 304
65003
Ha = 223
240 n
mi
Hp = 217
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12618918
28 X = 3799293
85
Y = 6203145
76 feet Y = 1933468
10 meter
Z = 17239554
72 Z = 5273185
74
XDOT = -13580
807161 XDOT = -4214
342025
YDOT = 21044
216537 feet/sec YDOT = 6367
568389 meter/sec
ZDOT = 2359
516065 ZDOT = 698
890273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13939582
48 X = 4248784
74
Y = 714187
74 feet Y = 217684
42 meter
Z = 17323288
92 Z = 5280138
46
XDOT = -4043
043111 XDOT = -1232
319540
YDOT = 23701
011933 feet/sec YDOT = 7224
068437 meter/sec
ZDOT = 2267
099180 ZDOT = 691
011830
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 19106
54947392
00016717 00000-0 10270-3 0 9041
2 25544 51
6395 307
6110 0001299 201
0895 159
0203 15
52540449 5672
Satellite: ISS
Catalog Number: 25544
Epoch time: 19106
54947392 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 307
6110 deg
Eccentricity:
0001299
Arg of perigee: 201
0895 deg
Mean anomaly: 159
0203 deg
Mean motion: 15
52540449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 567
Checksum: 307
Coasting Arc #6 (Orbit 581)
---------------------------------------
Vector Time (GMT): 2019/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3190373
22 A = 6782019
12 meter
Y = -2859456
76 meter E =
0014323
Z = -5269950
37 I = 51
29468
XDOT = 4482
114467 Wp = 99
89732
YDOT = -6173
520031 meter/sec RA = 302
15399 deg
ZDOT = 635
370367 TA = 176
21333
MA = 176
20248
Ha = 223
316 n
mi
Hp = 217
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10467103
75 X = -3132562
22
Y = -9381419
80 feet Y = -2894810
93 meter
Z = -17289863
42 Z = -5285307
44
XDOT = 14705
099958 XDOT = 4547
729111
YDOT = -20254
330809 feet/sec YDOT = -6123
030962 meter/sec
ZDOT = 2084
548448 ZDOT = 657
302779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13305790
45 X = -4055604
93
Y = -4258246
56 feet Y = -1297913
55 meter
Z = -17358973
24 Z = -5291015
04
XDOT = 4682
199893 XDOT = 1427
134527
YDOT = -23547
569930 feet/sec YDOT = -7177
299315 meter/sec
ZDOT = 2184
344217 ZDOT = 665
788117
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 19107
51497239
00016717 00000-0 10270-3 0 9050
2 25544 51
6374 302
8078 0001301 201
3073 158
8025 15
52579682 5821
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
51497239 = yrday
fracday
Element set: 905
Inclination: 51
6374 deg
RA of node: 302
8078 deg
Eccentricity:
0001301
Arg of perigee: 201
3073 deg
Mean anomaly: 158
8025 deg
Mean motion: 15
52579682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 582
Checksum: 305
Coasting Arc #7 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2019/107/20:46:03
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1917495
32 A = 6792325
98 meter
Y = 6235611
25 meter E =
0014054
Z = 1864739
25 I = 51
32550
XDOT = -5236
713240 Wp = 119
00665
YDOT = 72
496450 meter/sec RA = 300
31890 deg
ZDOT = -5601
912695 TA = 40
38199
MA = 40
27774
Ha = 223
269 n
mi
Hp = 217
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6290995
16 X = -1996139
12
Y = 20458042
17 feet Y = 6213728
90 meter
Z = 6117910
92 Z = 1855233
19
XDOT = -17180
817715 XDOT = -5209
923535
YDOT = 237
849245 feet/sec YDOT = 14
085189 meter/sec
ZDOT = -18378
978657 ZDOT = -5627
285801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14016346
97 X = 4272182
56
Y = -16192037
02 feet Y = -4935332
89 meter
Z = 6074281
69 Z = 1851441
06
XDOT = 14535
044817 XDOT = 4430
281660
YDOT = 5612
823005 feet/sec YDOT = 1710
788452 meter/sec
ZDOT = -18493
672570 ZDOT = -5636
871399
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 19107
90117108
00016717 00000-0 10270-3 0 9068
2 25544 51
6400 300
8883 0001363 201
8471 158
2623 15
52600810 5880
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
90117108 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 300
8883 deg
Eccentricity:
0001363
Arg of perigee: 201
8471 deg
Mean anomaly: 158
2623 deg
Mean motion: 15
52600810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 282
Coasting Arc #8 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2019/108/20:46:03
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2360626
67 A = 6793726
41 meter
Y = -6325728
72 meter E =
0009249
Z = -715436
11 I = 51
31299
XDOT = 4731
243179 Wp = 41
75124
YDOT = 1100
884302 meter/sec RA = 295
33200 deg
ZDOT = 5928
392433 TA = 310
49055
MA = 310
57112
Ha = 223
317 n
mi
Hp = 217
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7744838
15 X = 2434662
55
Y = -20753703
16 feet Y = -6298916
63 meter
Z = -2347231
32 Z = -703788
64
XDOT = 15522
451374 XDOT = 4689
783954
YDOT = 3611
825138 feet/sec YDOT = 1153
561002 meter/sec
ZDOT = 19450
106408 ZDOT = 5951
274535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15167653
95 X = -4623100
92
Y = 16152039
64 feet Y = 4923141
68 meter
Z = -2293926
06 Z = -699188
66
XDOT = -11627
748161 XDOT = -3544
137639
YDOT = -8166
482407 feet/sec YDOT = -2489
143838 meter/sec
ZDOT = 19553
413534 ZDOT = 5959
880445
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 19108
86666532
00016717 00000-0 10270-3 0 9075
2 25544 51
6392 296
0864 0001319 208
0544 152
0537 15
52544729 6036
Satellite: ISS
Catalog Number: 25544
Epoch time: 19108
86666532 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 296
0864 deg
Eccentricity:
0001319
Arg of perigee: 208
0544 deg
Mean anomaly: 152
0537 deg
Mean motion: 15
52544729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 603
Checksum: 315
Coasting Arc #9 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2019/109/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324376
80 A = 6782255
20 meter
Y = 473003
23 meter E =
0003855
Z = 5201716
32 I = 51
26901
XDOT = -2106
829625 Wp = 140
59320
YDOT = 7292
260418 meter/sec RA = 292
69792 deg
ZDOT = 1085
012328 TA = 298
93644
MA = 298
97509
Ha = 223
060 n
mi
Hp = 217
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14187587
92 X = 4293498
73
Y = 1551847
88 feet Y = 521189
13 meter
Z = 17065998
43 Z = 5222647
79
XDOT = -6912
170686 XDOT = -2193
487633
YDOT = 23924
738904 feet/sec YDOT = 7268
215909 meter/sec
ZDOT = 3559
751732 ZDOT = 1074
567041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13504226
44 X = 4116088
22
Y = 4253875
23 feet Y = 1296581
17 meter
Z = 17160553
57 Z = 5230536
73
XDOT = -11135
738899 XDOT = -3394
173216
YDOT = 21139
925120 feet/sec YDOT = 6443
449177 meter/sec
ZDOT = 3511
785272 ZDOT = 1070
392151
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 19109
44595930
00016717 00000-0 10270-3 0 9084
2 25544 51
6405 293
2066 0001185 217
3159 142
7910 15
52574640 6126
Satellite: ISS
Catalog Number: 25544
Epoch time: 19109
44595930 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 293
2066 deg
Eccentricity:
0001185
Arg of perigee: 217
3159 deg
Mean anomaly: 142
7910 deg
Mean motion: 15
52574640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 304
Coasting Arc #10 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2019/110/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3949843
95 A = 6781806
42 meter
Y = -1588751
65 meter E =
0014034
Z = -5291172
75 I = 51
25523
XDOT = 2533
868302 Wp = 95
61739
YDOT = -7219
013678 meter/sec RA = 287
68599 deg
ZDOT = 275
373674 TA = 177
03010
MA = 177
02176
Ha = 223
100 n
mi
Hp = 217
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12958805
61 X = -3906082
51
Y = -5212439
79 feet Y = -1632677
10 meter
Z = -17359490
66 Z = -5310253
58
XDOT = 8313
216215 XDOT = 2613
067408
YDOT = -23684
428078 feet/sec YDOT = -7190
235347 meter/sec
ZDOT = 903
456937 ZDOT = 287
875127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11715786
80 X = -3570971
82
Y = -7405717
23 feet Y = -2257262
61 meter
Z = -17445566
17 Z = -5317408
57
XDOT = 11830
459233 XDOT = 3605
923974
YDOT = -20984
304545 feet/sec YDOT = -6396
016025 meter/sec
ZDOT = 960
698979 ZDOT = 292
821049
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 19110
41144378
00016717 00000-0 10270-3 0 9090
2 25544 51
6397 288
4028 0001178 225
7473 134
3582 15
52611583 6270
Satellite: ISS
Catalog Number: 25544
Epoch time: 19110
41144378 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 288
4028 deg
Eccentricity:
0001178
Arg of perigee: 225
7473 deg
Mean anomaly: 134
3582 deg
Mean motion: 15
52611583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 314
Coasting Arc #11 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2019/111/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3580797
72 A = 6782667
14 meter
Y = 2694186
71 meter E =
0003841
Z = 5089267
52 I = 51
24888
XDOT = -2890
687120 Wp = 56
73779
YDOT = 6914
159604 meter/sec RA = 282
67619 deg
ZDOT = -1623
415442 TA = 49
03082
MA = 48
99759
Ha = 222
943 n
mi
Hp = 217
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11748024
00 X = 3525683
17
Y = 8839195
24 feet Y = 2733921
60 meter
Z = 16697071
91 Z = 5106528
08
XDOT = -9483
881627 XDOT = -2959
902592
YDOT = 22684
250669 feet/sec YDOT = 6881
446886 meter/sec
ZDOT = -5326
166147 ZDOT = -1637
625768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10069842
07 X = 3069287
86
Y = 10589789
84 feet Y = 3227767
94 meter
Z = 16774810
96 Z = 5112962
38
XDOT = -12186
835625 XDOT = -3714
547499
YDOT = 20143
585590 feet/sec YDOT = 6139
764888 meter/sec
ZDOT = -5391
092388 ZDOT = -1643
204960
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 19111
44129036
00016717 00000-0 10270-3 0 9100
2 25544 51
6395 283
2811 0001205 229
2920 130
8127 15
52609888 6437
Satellite: ISS
Catalog Number: 25544
Epoch time: 19111
44129036 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 283
2811 deg
Eccentricity:
0001205
Arg of perigee: 229
2920 deg
Mean anomaly: 130
8127 deg
Mean motion: 15
52609888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 291
Coasting Arc #12 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2019/112/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3252854
76 A = 6784549
10 meter
Y = -3744382
54 meter E =
0009851
Z = -4638884
24 I = 51
24811
XDOT = 3187
155554 Wp = 115
83697
YDOT = -6338
239465 meter/sec RA = 277
66729 deg
ZDOT = 2881
756441 TA = 183
01322
MA = 183
01916
Ha = 223
021 n
mi
Hp = 217
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10672095
68 X = -3188208
79
Y = -12284719
62 feet Y = -3780396
74 meter
Z = -15219436
49 Z = -4654528
65
XDOT = 10456
547093 XDOT = 3243
796491
YDOT = -20794
748902 feet/sec YDOT = -6302
281790 meter/sec
ZDOT = 9454
581499 ZDOT = 2897
376191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8702246
80 X = -2652444
82
Y = -13672344
00 feet Y = -4167330
45 meter
Z = -15289771
74 Z = -4660322
43
XDOT = 12265
724510 XDOT = 3738
592831
YDOT = -18457
541315 feet/sec YDOT = -5625
858593 meter/sec
ZDOT = 9525
812987 ZDOT = 2903
467798
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 19112
40676792
00016717 00000-0 10270-3 0 9114
2 25544 51
6386 278
4783 0001280 232
7327 127
3709 15
52617991 6581
Satellite: ISS
Catalog Number: 25544
Epoch time: 19112
40676792 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 278
4783 deg
Eccentricity:
0001280
Arg of perigee: 232
7327 deg
Mean anomaly: 127
3709 deg
Mean motion: 15
52617991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 329
Coasting Arc #13 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2019/113/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2935121
44 A = 6787058
32 meter
Y = 4688754
63 meter E =
0009777
Z = 3925168
71 I = 51
25439
XDOT = -3475
951190 Wp = 82
03263
YDOT = 5538
097807 meter/sec RA = 272
66285 deg
ZDOT = -4006
317540 TA = 50
06695
MA = 49
98108
Ha = 222
826 n
mi
Hp = 217
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9629663
52 X = 2863405
79
Y = 15383053
25 feet Y = 4721176
13 meter
Z = 12877850
09 Z = 3939252
53
XDOT = -11404
039336 XDOT = -3518
160739
YDOT = 18169
612229 feet/sec YDOT = 5498
991383 meter/sec
ZDOT = -13144
086417 ZDOT = -4023
304986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7526899
70 X = 2294199
03
Y = 16464593
27 feet Y = 5018408
03 meter
Z = 12941047
84 Z = 3944431
38
XDOT = -12316
030479 XDOT = -3753
926090
YDOT = 16047
767116 feet/sec YDOT = 4891
359417 meter/sec
ZDOT = -13221
414362 ZDOT = -4029
887097
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 19113
43660380
00016717 00000-0 10270-3 0 9125
2 25544 51
6396 273
3557 0001322 245
0281 115
0734 15
52643896 6741
Satellite: ISS
Catalog Number: 25544
Epoch time: 19113
43660380 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 273
3557 deg
Eccentricity:
0001322
Arg of perigee: 245
0281 deg
Mean anomaly: 115
0734 deg
Mean motion: 15
52643896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 300
Coasting Arc #14 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2019/114/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2652402
81 A = 6789784
38 meter
Y = -5470290
88 meter E =
0003350
Z = -3025367
89 I = 51
26100
XDOT = 3754
360493 Wp = 76
04938
YDOT = -4530
723207 meter/sec RA = 267
66326 deg
ZDOT = 4906
042399 TA = 249
11805
MA = 249
15392
Ha = 222
985 n
mi
Hp = 217
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8702108
96 X = -2576339
65
Y = -17947148
54 feet Y = -5499526
51 meter
Z = -9925747
67 Z = -3038067
80
XDOT = 12317
455687 XDOT = 3780
914272
YDOT = -14864
577452 feet/sec YDOT = -4488
591003 meter/sec
ZDOT = 16095
939630 ZDOT = 4924
344178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6627114
91 X = -2019944
62
Y = -18782327
20 feet Y = -5724853
33 meter
Z = -9982626
95 Z = -3042704
69
XDOT = 12387
456995 XDOT = 3775
696892
YDOT = -12960
469527 feet/sec YDOT = -3950
351112 meter/sec
ZDOT = 16179
105601 ZDOT = 4931
391387
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 19114
40207212
00016717 00000-0 10270-3 0 9135
2 25544 51
6377 268
5531 0001206 238
8271 121
2763 15
52624953 6898
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
40207212 = yrday
fracday
Element set: 913
Inclination: 51
6377 deg
RA of node: 268
5531 deg
Eccentricity:
0001206
Arg of perigee: 238
8271 deg
Mean anomaly: 121
2763 deg
Mean motion: 15
52624953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 297
Coasting Arc #15 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2019/114/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4060771
77 A = 6782367
59 meter
Y = 1762125
90 meter E =
0012957
Z = -5150171
50 I = 51
23618
XDOT = -1446
832750 Wp = 82
17580
YDOT = -7388
988135 meter/sec RA = 267
43759 deg
ZDOT = -1388
628500 TA = 174
38091
MA = 174
36636
Ha = 223
086 n
mi
Hp = 217
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13322742
03 X = -4055157
69
Y = 5781252
94 feet Y = 1716747
06 meter
Z = -16896888
11 Z = -5169883
67
XDOT = -4746
826609 XDOT = -1357
354213
YDOT = -24242
087056 feet/sec YDOT = -7404
667282 meter/sec
ZDOT = -4555
867781 ZDOT = -1395
439631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11638830
21 X = -3547515
45
Y = 8510645
10 feet Y = 2594044
63 meter
Z = -16986162
60 Z = -5177382
36
XDOT = -9247
426668 XDOT = -2818
615648
YDOT = -21791
029736 feet/sec YDOT = -6641
905864 meter/sec
ZDOT = -4585
943914 ZDOT = -1397
795705
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 19114
46643767
00016717 00000-0 10270-3 0 9141
2 25544 51
6376 268
2321 0001105 224
3514 135
7550 15
52631050 6901
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
46643767 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 268
2321 deg
Eccentricity:
0001105
Arg of perigee: 224
3514 deg
Mean anomaly: 135
7550 deg
Mean motion: 15
52631050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 286
Coasting Arc #16 (Orbit 705)
---------------------------------------
Vector Time (GMT): 2019/115/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4204415
43 A = 6781831
05 meter
Y = -590223
60 meter E =
0001767
Z = 5287089
56 I = 51
23556
XDOT = 1031
976512 Wp = 117
02901
YDOT = 7597
865026 meter/sec RA = 262
42560 deg
ZDOT = 26
738710 TA = 332
71010
MA = 332
71938
Ha = 222
974 n
mi
Hp = 217
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13794013
87 X = 4185021
12
Y = -1936429
12 feet Y = -543315
47 meter
Z = 17346094
35 Z = 5307466
01
XDOT = 3385
749710 XDOT = 946
808443
YDOT = 24927
378694 feet/sec YDOT = 7608
929104 meter/sec
ZDOT = 87
725426 ZDOT = 31
545043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12845336
44 X = 3915258
55
Y = -5080931
58 feet Y = -1548667
95 meter
Z = 17438263
43 Z = 5315182
69
XDOT = 8751
548756 XDOT = 2667
472061
YDOT = 22507
310473 feet/sec YDOT = 6860
228232 meter/sec
ZDOT = 108
737109 ZDOT = 33
143071
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 19115
49626564
00016717 00000-0 10270-3 0 9152
2 25544 51
6365 263
1096 0001112 228
9333 131
1723 15
52590023 7063
Satellite: ISS
Catalog Number: 25544
Epoch time: 19115
49626564 = yrday
fracday
Element set: 915
Inclination: 51
6365 deg
RA of node: 263
1096 deg
Eccentricity:
0001112
Arg of perigee: 228
9333 deg
Mean anomaly: 131
1723 deg
Mean motion: 15
52590023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 706
Checksum: 289
Coasting Arc #17 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2019/116/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4114096
60 A = 6781804
12 meter
Y = -1052510
38 meter E =
0001644
Z = 5286424
98 I = 51
24124
XDOT = 1745
619023 Wp = 119
45615
YDOT = 7465
141673 meter/sec RA = 257
60041 deg
ZDOT = 126
953903 TA = 329
32239
MA = 329
33200
Ha = 222
893 n
mi
Hp = 217
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13497692
26 X = 4099881
71
Y = -3453118
04 feet Y = -1006583
26 meter
Z = 17343913
96 Z = 5306375
23
XDOT = 5727
096531 XDOT = 1661
395274
YDOT = 24491
934623 feet/sec YDOT = 7484
191480 meter/sec
ZDOT = 416
515429 ZDOT = 135
229071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13253977
34 X = 4039812
29
Y = -3911995
19 feet Y = -1192376
13 meter
Z = 17434203
47 Z = 5313945
22
XDOT = 6281
301339 XDOT = 1914
540648
YDOT = 23313
182062 feet/sec YDOT = 7105
857893 meter/sec
ZDOT = 453
240284 ZDOT = 138
147639
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 19116
46172185
00016717 00000-0 10270-3 0 9166
2 25544 51
6369 258
3080 0001121 242
1398 117
9640 15
52601317 7211
Satellite: ISS
Catalog Number: 25544
Epoch time: 19116
46172185 = yrday
fracday
Element set: 916
Inclination: 51
6369 deg
RA of node: 258
3080 deg
Eccentricity:
0001121
Arg of perigee: 242
1398 deg
Mean anomaly: 117
9640 deg
Mean motion: 15
52601317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 291
Coasting Arc #18 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2019/117/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4390880
70 A = 6782153
15 meter
Y = -110118
86 meter E =
0013284
Z = -5179568
41 I = 51
25198
XDOT = -1285
045395 Wp = 102
44186
YDOT = -7443
679160 meter/sec RA = 252
58881 deg
ZDOT = 1247
538272 TA = 179
61838
MA = 179
61736
Ha = 222
993 n
mi
Hp = 217
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14405776
57 X = -4364163
46
Y = -361282
35 feet Y = -159071
33 meter
Z = -16993334
69 Z = -5200832
82
XDOT = -4216
028199 XDOT = -1207
772411
YDOT = -24421
519555 feet/sec YDOT = -7457
617388 meter/sec
ZDOT = 4092
973333 ZDOT = 1241
483610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14291194
18 X = -4355955
99
Y = 377217
97 feet Y = 114976
04 meter
Z = -17089465
26 Z = -5208869
01
XDOT = -5473
241518 XDOT = -1668
244015
YDOT = -23126
965551 feet/sec YDOT = -7049
099100 meter/sec
ZDOT = 4066
264845 ZDOT = 1239
397525
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 19117
42717172
00016717 00000-0 10270-3 0 9175
2 25544 51
6377 253
5056 0001028 240
1382 119
9668 15
52657484 7361
Satellite: ISS
Catalog Number: 25544
Epoch time: 19117
42717172 = yrday
fracday
Element set: 917
Inclination: 51
6377 deg
RA of node: 253
5056 deg
Eccentricity:
0001028
Arg of perigee: 240
1382 deg
Mean anomaly: 119
9668 deg
Mean motion: 15
52657484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 320
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list