[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 1st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19998 2692 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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
249/18:14:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 219
4
250/16:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 219
1
253/21:33:20
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 218
7
254/16:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 218
6
257/11:11:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 218
1
Coasting Arc #1 (Orbit 2677)
---------------------------------------
Vector Time (GMT): 2019/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6209229
55 A = 6797414
19 meter
Y = -1153407
99 meter E =
0004250
Z = -2521746
15 I = 51
60450
XDOT = 3009
868083 Wp = 25
74926
YDOT = -4647
505063 meter/sec RA = 352
07607 deg
ZDOT = -5285
040657 TA = 182
48978
MA = 182
49190
Ha = 227
803 n
mi
Hp = 220
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20371488
03 X = -6183621
32
Y = -3784146
96 feet Y = -1222700
93 meter
Z = -8273445
36 Z = -2551845
42
XDOT = 9874
895284 XDOT = 3087
285431
YDOT = -15247
720024 feet/sec YDOT = -4613
414030 meter/sec
ZDOT = -17339
372235 ZDOT = -5270
231834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17320895
59 X = 5279408
97
Y = 11270364
86 feet Y = 3435207
21 meter
Z = -8410270
08 Z = -2563450
32
XDOT = -14244
222478 XDOT = -4341
639011
YDOT = 9001
855639 feet/sec YDOT = 2743
765599 meter/sec
ZDOT = -17271
519542 ZDOT = -5264
359156
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 19242
52710408
00016717 00000-0 10270-3 0 9002
2 25544 51
6446 352
5097 0007378 343
1521 16
9383 15
50400537 26786
Satellite: ISS
Catalog Number: 25544
Epoch time: 19242
52710408 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 352
5097 deg
Eccentricity:
0007378
Arg of perigee: 343
1521 deg
Mean anomaly: 16
9383 deg
Mean motion: 15
50400537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2678
Checksum: 302
Coasting Arc #2 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2019/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6045240
93 A = 6796434
94 meter
Y = 994599
02 meter E =
0014502
Z = 2920617
25 I = 51
56942
XDOT = -3221
639673 Wp = 51
30946
YDOT = 4821
545171 meter/sec RA = 347
11723 deg
ZDOT = 5018
392941 TA = 342
01137
MA = 342
06264
Ha = 227
810 n
mi
Hp = 220
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19833467
62 X = 6019483
22
Y = 3263120
15 feet Y = 1062057
37 meter
Z = 9582077
60 Z = 2949919
69
XDOT = -10569
683967 XDOT = -3299
692355
YDOT = 15818
717752 feet/sec YDOT = 4785
082498 meter/sec
ZDOT = 16464
543770 ZDOT = 5002
553706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17194502
17 X = -5240884
26
Y = -10285571
98 feet Y = -3135042
34 meter
Z = 9715282
10 Z = 2961217
98
XDOT = 14987
493339 XDOT = 4568
187970
YDOT = -9547
259389 feet/sec YDOT = -2910
004662 meter/sec
ZDOT = 16391
998644 ZDOT = 4996
281187
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 19243
55841586
00016717 00000-0 10270-3 0 9019
2 25544 51
6455 347
3979 0007421 347
2636 12
8326 15
50417319 26944
Satellite: ISS
Catalog Number: 25544
Epoch time: 19243
55841586 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 347
3979 deg
Eccentricity:
0007421
Arg of perigee: 347
2636 deg
Mean anomaly: 12
8326 deg
Mean motion: 15
50417319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 327
Coasting Arc #3 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2019/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5873609
82 A = 6795463
99 meter
Y = -875445
86 meter E =
0007982
Z = -3314295
86 I = 51
53332
XDOT = 3393
621152 Wp = 25
72902
YDOT = -5006
139029 meter/sec RA = 342
15596 deg
ZDOT = -4689
085550 TA = 192
76463
MA = 192
78485
Ha = 228
097 n
mi
Hp = 220
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19270373
41 X = -5847284
93
Y = -2872197
70 feet Y = -940981
79 meter
Z = -10873674
09 Z = -3342763
38
XDOT = 11133
927663 XDOT = 3472
125792
YDOT = -16424
340647 feet/sec YDOT = -4967
750621 meter/sec
ZDOT = -15384
138942 ZDOT = -4672
409661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16970454
41 X = 5172594
50
Y = 9421756
74 feet Y = 2871751
45 meter
Z = -11003080
32 Z = -3353738
88
XDOT = -15596
288969 XDOT = -4753
748878
YDOT = 10204
516771 feet/sec YDOT = 3110
336712 meter/sec
ZDOT = -15307
782380 ZDOT = -4665
812069
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 19244
52527058
00016717 00000-0 10270-3 0 9023
2 25544 51
6451 342
6063 0007512 350
8188 9
2824 15
50395231 27093
Satellite: ISS
Catalog Number: 25544
Epoch time: 19244
52527058 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 342
6063 deg
Eccentricity:
0007512
Arg of perigee: 350
8188 deg
Mean anomaly: 9
2824 deg
Mean motion: 15
50395231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 300
Coasting Arc #4 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2019/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5658093
54 A = 6794329
13 meter
Y = 782325
18 meter E =
0012727
Z = 3663837
07 I = 51
49804
XDOT = -3539
474555 Wp = 59
16667
YDOT = 5236
459653 meter/sec RA = 337
19119 deg
ZDOT = 4343
079639 TA = 344
45599
MA = 344
49504
Ha = 228
055 n
mi
Hp = 220
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18563299
02 X = 5631128
02
Y = 2566683
67 feet Y = 845447
49 meter
Z = 12020462
82 Z = 3691256
30
XDOT = -11612
449328 XDOT = -3618
863285
YDOT = 17179
985737 feet/sec YDOT = 5196
435208 meter/sec
ZDOT = 14248
948946 ZDOT = 4325
693034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16558564
89 X = -5047050
58
Y = -8601509
86 feet Y = -2621740
21 meter
Z = 12145098
55 Z = 3701826
04
XDOT = 16153
347718 XDOT = 4923
540384
YDOT = -11067
510588 feet/sec YDOT = -3373
377227 meter/sec
ZDOT = 14169
348627 ZDOT = 4318
817462
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 19245
55658018
00016717 00000-0 10270-3 0 9039
2 25544 51
6447 337
4945 0007539 354
9341 5
1732 15
50422601 27257
Satellite: ISS
Catalog Number: 25544
Epoch time: 19245
55658018 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 337
4945 deg
Eccentricity:
0007539
Arg of perigee: 354
9341 deg
Mean anomaly: 5
1732 deg
Mean motion: 15
50422601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 310
Coasting Arc #5 (Orbit 2739)
---------------------------------------
Vector Time (GMT): 2019/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5450628
58 A = 6793351
75 meter
Y = -731015
92 meter E =
0011652
Z = -4001181
70 I = 51
46325
XDOT = 3629
718536 Wp = 33
03102
YDOT = -5461
097534 meter/sec RA = 332
22387 deg
ZDOT = -3942
741920 TA = 195
74449
MA = 195
78075
Ha = 228
328 n
mi
Hp = 219
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17882639
71 X = -5422613
54
Y = -2398346
19 feet Y = -791812
30 meter
Z = -13127236
54 Z = -4027590
70
XDOT = 11908
525380 XDOT = 3709
667977
YDOT = -17916
986661 feet/sec YDOT = -5420
060690 meter/sec
ZDOT = -12935
504988 ZDOT = -3924
915591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16105290
55 X = 4908892
56
Y = 7936912
48 feet Y = 2419170
92 meter
Z = -13247273
05 Z = -4037768
83
XDOT = -16494
981521 XDOT = -5027
670368
YDOT = 11994
606564 feet/sec YDOT = 3655
956081 meter/sec
ZDOT = -12853
892915 ZDOT = -3917
866560
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 19246
52343456
00016717 00000-0 10270-3 0 9045
2 25544 51
6438 332
7028 0007552 357
9735 2
1384 15
50391374 27401
Satellite: ISS
Catalog Number: 25544
Epoch time: 19246
52343456 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 332
7028 deg
Eccentricity:
0007552
Arg of perigee: 357
9735 deg
Mean anomaly: 2
1384 deg
Mean motion: 15
50391374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2740
Checksum: 310
Coasting Arc #6 (Orbit 2755)
---------------------------------------
Vector Time (GMT): 2019/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5208009
80 A = 6792199
41 meter
Y = 717232
64 meter E =
0010537
Z = 4289555
42 I = 51
43142
XDOT = -3694
446743 Wp = 63
25364
YDOT = 5720
011420 meter/sec RA = 327
25236 deg
ZDOT = 3527
006220 TA = 350
70385
MA = 350
72334
Ha = 228
274 n
mi
Hp = 219
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17086646
33 X = 5178766
14
Y = 2353125
45 feet Y = 775308
96 meter
Z = 14073344
55 Z = 4314782
93
XDOT = -12120
888264 XDOT = -3775
267232
YDOT = 18766
441666 feet/sec YDOT = 5678
245779 meter/sec
ZDOT = 11571
542716 ZDOT = 3508
863414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15488145
98 X = -4720786
89
Y = -7373441
49 feet Y = -2247424
97 meter
Z = 14188002
11 Z = 4324503
04
XDOT = 16757
115528 XDOT = 5107
568813
YDOT = -13079
768678 feet/sec YDOT = -3986
713493 meter/sec
ZDOT = 11488
475205 ZDOT = 3501
687243
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 19247
55474177
00016717 00000-0 10270-3 0 9055
2 25544 51
6445 327
5902 0007659 1
7724 358
3453 15
50426760 27560
Satellite: ISS
Catalog Number: 25544
Epoch time: 19247
55474177 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 327
5902 deg
Eccentricity:
0007659
Arg of perigee: 1
7724 deg
Mean anomaly: 358
3453 deg
Mean motion: 15
50426760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2756
Checksum: 329
Coasting Arc #7 (Orbit 2770)
---------------------------------------
Vector Time (GMT): 2019/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4990388
57 A = 6791338
10 meter
Y = -742845
05 meter E =
0015123
Z = -4560687
18 I = 51
39977
XDOT = 3695
029409 Wp = 41
97278
YDOT = -5954
489129 meter/sec RA = 322
27925 deg
ZDOT = -3068
214873 TA = 197
12474
MA = 197
17582
Ha = 228
607 n
mi
Hp = 219
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16372665
92 X = -4959557
69
Y = -2437155
68 feet Y = -798478
84 meter
Z = -14962884
44 Z = -4584853
71
XDOT = 12122
799897 XDOT = 3776
243286
YDOT = -19535
725490 feet/sec YDOT = -5912
714705 meter/sec
ZDOT = -10066
321762 ZDOT = -3050
068374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14898676
50 X = 4541116
60
Y = 6981022
65 feet Y = 2127815
70 meter
Z = -15072710
08 Z = -4594162
03
XDOT = -16750
421604 XDOT = -5105
528505
YDOT = 14157
687444 feet/sec YDOT = 4315
263133 meter/sec
ZDOT = -9983
223710 ZDOT = -3042
886587
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 19248
52159361
00016717 00000-0 10270-3 0 9069
2 25544 51
6435 322
7984 0007762 5
7233 354
4005 15
50390741 27716
Satellite: ISS
Catalog Number: 25544
Epoch time: 19248
52159361 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 322
7984 deg
Eccentricity:
0007762
Arg of perigee: 5
7233 deg
Mean anomaly: 354
4005 deg
Mean motion: 15
50390741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2771
Checksum: 309
Coasting Arc #8 (Orbit 2786)
---------------------------------------
Vector Time (GMT): 2019/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4748651
29 A = 6790339
53 meter
Y = 812493
08 meter E =
0008704
Z = 4776898
48 I = 51
37098
XDOT = -3673
004256 Wp = 61
32570
YDOT = 6210
988643 meter/sec RA = 317
30285 deg
ZDOT = 2595
366329 TA = 3
00326
MA = 2
99803
Ha = 228
531 n
mi
Hp = 219
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15579564
62 X = 4716009
37
Y = 2665659
70 feet Y = 865413
42 meter
Z = 15672239
11 Z = 4799886
30
XDOT = -12050
538897 XDOT = -3754
791159
YDOT = 20377
259326 feet/sec YDOT = 6169
457275 meter/sec
ZDOT = 8514
981393 ZDOT = 2577
325521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14186617
96 X = -4324081
16
Y = -6729294
07 feet Y = -2051088
83 meter
Z = 15776695
67 Z = 4808736
84
XDOT = 16650
607611 XDOT = 5075
105200
YDOT = -15336
930457 feet/sec YDOT = -4674
696403 meter/sec
ZDOT = 8432
349251 ZDOT = 2570
180052
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 19249
55290013
00016717 00000-0 10270-3 0 9074
2 25544 51
6434 317
6862 0007794 9
5511 350
5787 15
50421952 27879
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
55290013 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 317
6862 deg
Eccentricity:
0007794
Arg of perigee: 9
5511 deg
Mean anomaly: 350
5787 deg
Mean motion: 15
50421952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2787
Checksum: 327
Coasting Arc #9 (Orbit 2790)
---------------------------------------
Vector Time (GMT): 2019/249/18:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4109083
59 A = 6788983
70 meter
Y = 1719850
52 meter E =
0007587
Z = 5117323
58 I = 51
35687
XDOT = -4461
612446 Wp = 45
41671
YDOT = 6038
225781 meter/sec RA = 316
00485 deg
ZDOT = 1557
012507 TA = 29
53513
MA = 29
49229
Ha = 228
745 n
mi
Hp = 219
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13481245
38 X = 4064689
29
Y = 5642554
18 feet Y = 1765553
05 meter
Z = 16789119
37 Z = 5137176
06
XDOT = -14637
836109 XDOT = -4536
365114
YDOT = 19810
452037 feet/sec YDOT = 5987
914948 meter/sec
ZDOT = 5108
308750 ZDOT = 1535
158060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8266931
93 X = -2519760
85
Y = 11925028
15 feet Y = 3634748
58 meter
Z = 16879231
74 Z = 5144789
83
XDOT = -15508
351098 XDOT = -4726
945415
YDOT = -17822
545455 feet/sec YDOT = -5432
311855 meter/sec
ZDOT = 5008
353983 ZDOT = 1526
546294
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 19249
81072858
00016717 00000-0 10270-3 0 9089
2 25544 51
6404 316
4094 0008171 11
1014 349
0315 15
50401765 27912
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
81072858 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 316
4094 deg
Eccentricity:
0008171
Arg of perigee: 11
1014 deg
Mean anomaly: 349
0315 deg
Mean motion: 15
50401765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2791
Checksum: 295
Coasting Arc #10 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2019/250/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5442220
92 A = 6794259
14 meter
Y = 1672591
01 meter E =
0012032
Z = -3722570
76 I = 51
35326
XDOT = 987
798607 Wp = 40
70748
YDOT = -6275
420475 meter/sec RA = 311
39412 deg
ZDOT = -4262
619686 TA = 183
77446
MA = 183
78354
Ha = 228
978 n
mi
Hp = 219
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17855055
52 X = -5442437
77
Y = 5487503
30 feet Y = 1611730
98 meter
Z = -12213158
66 Z = -3749007
43
XDOT = 3240
809077 XDOT = 1078
604072
YDOT = -20588
649854 feet/sec YDOT = -6263
866560 meter/sec
ZDOT = -13984
972724 ZDOT = -4257
600709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6138527
18 X = 1871023
08
Y = -17557888
92 feet Y = -5351644
54 meter
Z = -12333530
12 Z = -3759259
98
XDOT = 13305
914162 XDOT = 4055
642637
YDOT = 14461
789023 feet/sec YDOT = 4407
953294 meter/sec
ZDOT = -13961
562405 ZDOT = -4255
484221
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 19250
71312157
00016717 00000-0 10270-3 0 9090
2 25544 51
6409 311
9362 0008126 15
5832 344
5568 15
50393568 28058
Satellite: ISS
Catalog Number: 25544
Epoch time: 19250
71312157 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 311
9362 deg
Eccentricity:
0008126
Arg of perigee: 15
5832 deg
Mean anomaly: 344
5568 deg
Mean motion: 15
50393568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 312
Coasting Arc #11 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2019/251/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5207428
81 A = 6793097
11 meter
Y = -1618050
48 meter E =
0013983
Z = 4035777
90 I = 51
32870
XDOT = -974
230875 Wp = 66
76032
YDOT = 6546
614619 meter/sec RA = 306
41689 deg
ZDOT = 3876
476200 TA = 342
87693
MA = 342
92406
Ha = 228
840 n
mi
Hp = 219
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17084740
18 X = 5205531
90
Y = -5308564
57 feet Y = -1559827
87 meter
Z = 13240741
13 Z = 4061068
83
XDOT = -3196
295522 XDOT = -1066
194203
YDOT = 21478
394419 feet/sec YDOT = 6535
205963 meter/sec
ZDOT = 12718
097770 ZDOT = 3871
520302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5530740
11 X = -1685769
59
Y = 16923872
84 feet Y = 5158396
44 meter
Z = 13355892
78 Z = 4070876
12
XDOT = -14362
027945 XDOT = -4377
546118
YDOT = -14725
677274 feet/sec YDOT = -4488
386433 meter/sec
ZDOT = 12694
962924 ZDOT = 3869
424699
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 19251
74442562
00016717 00000-0 10270-3 0 9100
2 25544 51
6411 306
8246 0008147 18
0649 342
0790 15
50427390 28211
Satellite: ISS
Catalog Number: 25544
Epoch time: 19251
74442562 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 306
8246 deg
Eccentricity:
0008147
Arg of perigee: 18
0649 deg
Mean anomaly: 342
0790 deg
Mean motion: 15
50427390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 295
Coasting Arc #12 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2019/252/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5009410
85 A = 6792150
46 meter
Y = 1527296
31 meter E =
0015643
Z = -4341580
94 I = 51
30563
XDOT = 914
869330 Wp = 46
34870
YDOT = -6772
459658 meter/sec RA = 301
43642 deg
ZDOT = -3435
257559 TA = 188
50780
MA = 188
53435
Ha = 229
186 n
mi
Hp = 218
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16435074
98 X = -5005028
46
Y = 5010814
67 feet Y = 1471301
92 meter
Z = -14244031
94 Z = -4365903
90
XDOT = 3001
539798 XDOT = 1007
219321
YDOT = -22219
355833 feet/sec YDOT = -6761
712689 meter/sec
ZDOT = -11270
530049 ZDOT = -3430
589010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5112988
04 X = 1558438
75
Y = -16306758
23 feet Y = -4970299
91 meter
Z = -14354768
85 Z = -4375333
54
XDOT = 15391
555928 XDOT = 4691
346247
YDOT = 14736
167304 feet/sec YDOT = 4491
583794 meter/sec
ZDOT = -11248
698045 ZDOT = -3428
603164
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 19252
71127485
00016717 00000-0 10270-3 0 9113
2 25544 51
6404 302
0317 0008295 22
3817 337
7694 15
50395863 28368
Satellite: ISS
Catalog Number: 25544
Epoch time: 19252
71127485 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 302
0317 deg
Eccentricity:
0008295
Arg of perigee: 22
3817 deg
Mean anomaly: 337
7694 deg
Mean motion: 15
50395863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 315
Coasting Arc #13 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2019/253/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4799632
85 A = 6791070
84 meter
Y = -1393570
38 meter E =
0011702
Z = 4586270
74 I = 51
28556
XDOT = -818
217341 Wp = 70
01071
YDOT = 7017
339641 meter/sec RA = 296
45525 deg
ZDOT = 2986
257904 TA = 350
04538
MA = 350
06854
Ha = 228
991 n
mi
Hp = 218
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15746826
95 X = 4792582
16
Y = -4572081
31 feet Y = -1339936
72 meter
Z = 15046820
00 Z = 4609568
20
XDOT = -2684
440096 XDOT = -911
131852
YDOT = 23022
767850 feet/sec YDOT = 7007
670378 meter/sec
ZDOT = 9797
434068 ZDOT = 2982
057367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4815200
74 X = -1467673
19
Y = 15571687
27 feet Y = 4746250
28 meter
Z = 15152876
82 Z = 4618596
86
XDOT = -16553
059050 XDOT = -5045
372399
YDOT = -14640
684481 feet/sec YDOT = -4462
480630 meter/sec
ZDOT = 9777
727774 ZDOT = 2980
251426
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 19253
74257873
00016717 00000-0 10270-3 0 9123
2 25544 51
6400 296
9204 0008187 24
7655 335
3888 15
50430152 28524
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
74257873 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 296
9204 deg
Eccentricity:
0008187
Arg of perigee: 24
7655 deg
Mean anomaly: 335
3888 deg
Mean motion: 15
50430152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 321
Coasting Arc #14 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2019/253/21:33:20
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -517388
15 A = 6797071
11 meter
Y = 6198880
62 meter E =
0017496
Z = 2732123
17 I = 51
30504
XDOT = -5401
374781 Wp = 73
90204
YDOT = 1819
777373 meter/sec RA = 295
36956 deg
ZDOT = -5119
544890 TA = 75
08438
MA = 74
89071
Ha = 229
260 n
mi
Hp = 218
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1697467
68 X = -599938
34
Y = 20337534
83 feet Y = 6192633
39 meter
Z = 8963658
70 Z = 2729409
12
XDOT = -17721
045869 XDOT = -5396
455022
YDOT = 5970
398205 feet/sec YDOT = 1759
402646 meter/sec
ZDOT = -16796
407119 ZDOT = -5145
770556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16275479
98 X = -4960766
30
Y = 12322178
23 feet Y = 3755799
92 meter
Z = 8950786
12 Z = 2728199
61
XDOT = -15330
219031 XDOT = -4672
650761
YDOT = -7884
159300 feet/sec YDOT = -2403
091755 meter/sec
ZDOT = -16915
814053 ZDOT = -5155
940123
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 19253
93595023
00016717 00000-0 10270-3 0 9137
2 25544 51
6431 295
9631 0008256 26
1488 334
0068 15
50393796 28559
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
93595023 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 295
9631 deg
Eccentricity:
0008256
Arg of perigee: 26
1488 deg
Mean anomaly: 334
0068 deg
Mean motion: 15
50393796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 330
Coasting Arc #15 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2019/254/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1657566
21 A = 6792649
74 meter
Y = -5059909
18 meter E =
0012425
Z = -4224788
09 I = 51
27675
XDOT = 4919
909460 Wp = 68
17400
YDOT = -4618
901570 meter/sec RA = 291
37180 deg
ZDOT = 3614
762551 TA = 239
00976
MA = 239
13188
Ha = 229
302 n
mi
Hp = 218
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5438209
35 X = -1580340
22
Y = -16600751
90 feet Y = -5078013
73 meter
Z = -13860853
30 Z = -4232651
93
XDOT = 16141
435235 XDOT = 4953
635398
YDOT = -15153
876541 feet/sec YDOT = -4563
694868 meter/sec
ZDOT = 11859
457187 ZDOT = 3638
743545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17141491
53 X = 5224726
62
Y = 3216760
53 feet Y = 980468
61 meter
Z = -13896188
65 Z = -4235558
30
XDOT = 5897
475450 XDOT = 1797
550517
YDOT = 20092
700961 feet/sec YDOT = 6124
255253 meter/sec
ZDOT = 11968
885312 ZDOT = 3648
116243
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 19254
70942687
00016717 00000-0 10270-3 0 9146
2 25544 51
6404 292
1277 0008343 28
5727 331
5880 15
50391039 28678
Satellite: ISS
Catalog Number: 25544
Epoch time: 19254
70942687 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 292
1277 deg
Eccentricity:
0008343
Arg of perigee: 28
5727 deg
Mean anomaly: 331
5880 deg
Mean motion: 15
50391039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 328
Coasting Arc #16 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2019/255/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1694730
14 A = 6793700
32 meter
Y = 5299859
49 meter E =
0017856
Z = 3891669
99 I = 51
26954
XDOT = -4706
065684 Wp = 59
79166
YDOT = 4494
250194 meter/sec RA = 286
38837 deg
ZDOT = -4048
289532 TA = 72
92655
MA = 72
73103
Ha = 229
361 n
mi
Hp = 218
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5560138
26 X = 1616436
25
Y = 17387990
44 feet Y = 5318373
70 meter
Z = 12767946
17 Z = 3899711
68
XDOT = -15439
848046 XDOT = -4736
307786
YDOT = 14744
915334 feet/sec YDOT = 4441
454227 meter/sec
ZDOT = -13281
789803 ZDOT = -4071
223413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17952267
11 X = -5471851
02
Y = -3170064
34 feet Y = -966235
61 meter
Z = 12804085
13 Z = 3902685
15
XDOT = -6225
735954 XDOT = -1897
604319
YDOT = -19113
337482 feet/sec YDOT = -5825
745265 meter/sec
ZDOT = -13386
431188 ZDOT = -4080
184226
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 19255
74072881
00016717 00000-0 10270-3 0 9152
2 25544 51
6405 287
0150 0008438 31
7184 328
4481 15
50421073 28832
Satellite: ISS
Catalog Number: 25544
Epoch time: 19255
74072881 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 287
0150 deg
Eccentricity:
0008438
Arg of perigee: 31
7184 deg
Mean anomaly: 328
4481 deg
Mean motion: 15
50421073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 308
Coasting Arc #17 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2019/256/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1817790
57 A = 6794779
15 meter
Y = -5487321
82 meter E =
0011912
Z = -3574045
15 I = 51
26387
XDOT = 4492
336541 Wp = 58
06620
YDOT = -4353
508966 meter/sec RA = 281
40588 deg
ZDOT = 4416
271524 TA = 259
54319
MA = 259
67744
Ha = 229
456 n
mi
Hp = 218
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5963879
83 X = -1738934
05
Y = -18003024
35 feet Y = -5507209
06 meter
Z = -11725869
92 Z = -3582683
18
XDOT = 14738
636945 XDOT = 4519
233218
YDOT = -14283
165900 feet/sec YDOT = -4303
121684 meter/sec
ZDOT = 14489
079802 ZDOT = 4438
159188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18737779
52 X = 5711275
20
Y = 2767624
44 feet Y = 843571
93 meter
Z = -11764720
44 Z = -3585886
79
XDOT = 6450
038363 XDOT = 1965
971693
YDOT = 18109
047785 feet/sec YDOT = 5519
637765 meter/sec
ZDOT = 14588
938349 ZDOT = 4446
708409
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 19256
70757433
00016717 00000-0 10270-3 0 9163
2 25544 51
6398 282
2228 0008452 35
1549 325
0158 15
50393578 28983
Satellite: ISS
Catalog Number: 25544
Epoch time: 19256
70757433 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 282
2228 deg
Eccentricity:
0008452
Arg of perigee: 35
1549 deg
Mean anomaly: 325
0158 deg
Mean motion: 15
50393578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 340
Coasting Arc #18 (Orbit 2909)
---------------------------------------
Vector Time (GMT): 2019/257/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 951418
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4107851
13 A = 6788389
17 meter
Y = -1242736
63 meter E =
0020466
Z = -5276370
78 I = 51
24014
XDOT = 1490
794032 Wp = 75
21611
YDOT = -7476
765446 meter/sec RA = 277
60855 deg
ZDOT = 607
462867 TA = 200
58876
MA = 200
67135
Ha = 229
475 n
mi
Hp = 218
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13477201
86 X = -4068019
61
Y = -4077219
91 feet Y = -1288451
34 meter
Z = -17310927
77 Z = -5296228
23
XDOT = 4891
056534 XDOT = 1571
339881
YDOT = -24530
070362 feet/sec YDOT = -7459
643914 meter/sec
ZDOT = 1992
988410 ZDOT = 614
900947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11160010
89 X = 3401571
32
Y = 8401309
72 feet Y = 2560719
20 meter
Z = -17401122
50 Z = -5303862
14
XDOT = -12359
572057 XDOT = -3767
197563
YDOT = 20569
146594 feet/sec YDOT = 6269
475882 meter/sec
ZDOT = 2027
372422 ZDOT = 617
943114
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 19257
48105039
00016717 00000-0 10270-3 0 9179
2 25544 51
6419 278
3880 0008258 39
0785 321
0961 15
50391251 29105
Satellite: ISS
Catalog Number: 25544
Epoch time: 19257
48105039 = yrday
fracday
Element set: 917
Inclination: 51
6419 deg
RA of node: 278
3880 deg
Eccentricity:
0008258
Arg of perigee: 39
0785 deg
Mean anomaly: 321
0961 deg
Mean motion: 15
50391251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2910
Checksum: 318
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