[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 30th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
242/21:54:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
1
249/00:35:06
532 0
6 0
7 0
7
N/A -0
2 -0
1 223
0
000/00:00:13
064 0
2 -0
0 213
7
249/22:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
8
253/11:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 214
0
253/22:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2018/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2447798
95 A = 6778695
35 meter
Y = -3642098
16 meter E =
0019470
Z = -5183938
37 I = 51
70969
XDOT = 7014
740475 Wp = 103
13408
YDOT = 2721
304315 meter/sec RA = 12
75320 deg
ZDOT = 1400
485768 TA = 180
34749
MA = 180
34884
Ha = 223
389 n
mi
Hp = 213
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8030836
45 X = 2513524
64
Y = -11949140
96 feet Y = -3614358
12 meter
Z = -17007671
81 Z = -5171887
95
XDOT = 23014
240405 XDOT = 6976
985975
YDOT = 8928
163762 feet/sec YDOT = 2799
537023 meter/sec
ZDOT = 4594
769581 ZDOT = 1434
468772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12197262
89 X = -3717725
73
Y = 7769013
58 feet Y = 2367995
34 meter
Z = -16953064
91 Z = -5167294
19
XDOT = -17031
090070 XDOT = -5191
076253
YDOT = -16381
058741 feet/sec YDOT = -4992
946704 meter/sec
ZDOT = 4746
907721 ZDOT = 1446
857473
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 18241
51361455
00016717 00000-0 10270-3 0 9003
2 25544 51
6402 13
2838 0005737 109
8964 250
2807 15
53908674 9915
Satellite: ISS
Catalog Number: 25544
Epoch time: 18241
51361455 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 13
2838 deg
Eccentricity:
0005737
Arg of perigee: 109
8964 deg
Mean anomaly: 250
2807 deg
Mean motion: 15
53908674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 312
Coasting Arc #2 (Orbit 1006)
---------------------------------------
Vector Time (GMT): 2018/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3972946
77 A = 6781394
99 meter
Y = 3079428
85 meter E =
0013585
Z = 4540884
03 I = 51
68676
XDOT = -6166
610955 Wp = 84
85576
YDOT = -3333
222759 meter/sec RA = 7
76337 deg
ZDOT = -3125
662180 TA = 36
45754
MA = 36
36511
Ha = 223
549 n
mi
Hp = 213
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13034602
26 X = -4029143
67
Y = 10103113
01 feet Y = 3034686
75 meter
Z = 14897913
48 Z = 4521448
15
XDOT = -20231
663239 XDOT = -6113
696848
YDOT = -10935
770207 feet/sec YDOT = -3401
886467 meter/sec
ZDOT = -10254
797180 ZDOT = -3155
488554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15981083
89 X = 4871034
37
Y = -4379856
68 feet Y = -1334980
31 meter
Z = 14810246
04 Z = 4514162
99
XDOT = 14202
279897 XDOT = 4328
854913
YDOT = 16590
743200 feet/sec YDOT = 5056
858527 meter/sec
ZDOT = -10388
177800 ZDOT = -3166
316594
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 18242
54259903
00016717 00000-0 10270-3 0 9012
2 25544 51
6410 8
1555 0005805 113
1449 247
0316 15
53878703 10072
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
54259903 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 8
1555 deg
Eccentricity:
0005805
Arg of perigee: 113
1449 deg
Mean anomaly: 247
0316 deg
Mean motion: 15
53878703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1007
Checksum: 288
Coasting Arc #3 (Orbit 1012)
---------------------------------------
Vector Time (GMT): 2018/242/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 461306
65 A = 6778059
44 meter
Y = -4187881
32 meter E =
0020289
Z = -5326992
98 I = 51
66020
XDOT = 7611
935774 Wp = 95
28829
YDOT = 792
118666 meter/sec RA = 5
73531 deg
ZDOT = 34
733552 TA = 175
05328
MA = 175
03321
Ha = 223
385 n
mi
Hp = 213
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1513473
25 X = 533978
09
Y = -13739768
11 feet Y = -4182316
75 meter
Z = -17477011
09 Z = -5324575
29
XDOT = 24973
542564 XDOT = 7602
343633
YDOT = 2598
814521 feet/sec YDOT = 877
186976 meter/sec
ZDOT = 113
955223 ZDOT = 71
686273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11995938
73 X = 3656362
12
Y = -6897056
22 feet Y = -2102222
73 meter
Z = -17465560
84 Z = -5323502
94
XDOT = 12322
282535 XDOT = 3755
831717
YDOT = 20709
497393 feet/sec YDOT = 6312
254805 meter/sec
ZDOT = 279
675844 ZDOT = 85
245197
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 18242
92846568
00016717 00000-0 10270-3 0 9024
2 25544 51
6390 6
2365 0005639 109
3980 250
7782 15
53889982 10135
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
92846568 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 6
2365 deg
Eccentricity:
0005639
Arg of perigee: 109
3980 deg
Mean anomaly: 250
7782 deg
Mean motion: 15
53889982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1013
Checksum: 333
Coasting Arc #4 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2018/243/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2159349
32 A = 6779195
35 meter
Y = 3967958
03 meter E =
0009860
Z = 5046562
01 I = 51
63041
XDOT = -7274
938392 Wp = 83
28961
YDOT = -1574
820871 meter/sec RA =
73948 deg
ZDOT = -1870
341630 TA = 24
84339
MA = 24
79595
Ha = 223
353 n
mi
Hp = 213
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7084479
38 X = -2228073
20
Y = 13018235
02 feet Y = 3943426
76 meter
Z = 16556961
99 Z = 5035905
46
XDOT = -23867
908111 XDOT = -7247
702478
YDOT = -5166
735142 feet/sec YDOT = -1656
022106 meter/sec
ZDOT = -6136
291437 ZDOT = -1905
614538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14702971
33 X = -4481465
66
Y = 2255429
10 feet Y = 687454
79 meter
Z = 16508572
16 Z = 5031812
80
XDOT = -10296
777350 XDOT = -3138
457736
YDOT = -20949
872085 feet/sec YDOT = -6385
521012 meter/sec
ZDOT = -6294
347172 ZDOT = -1918
517018
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 18243
95744434
00016717 00000-0 10270-3 0 9038
2 25544 51
6382 1
1091 0005510 112
8738 247
2997 15
53911187 10293
Satellite: ISS
Catalog Number: 25544
Epoch time: 18243
95744434 = yrday
fracday
Element set: 903
Inclination: 51
6382 deg
RA of node: 1
1091 deg
Eccentricity:
0005510
Arg of perigee: 112
8738 deg
Mean anomaly: 247
2997 deg
Mean motion: 15
53911187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 305
Coasting Arc #5 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2018/244/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3712156
65 A = 6782217
82 meter
Y = -3704546
81 meter E =
0013833
Z = -4314904
28 I = 51
60745
XDOT = 6394
200758 Wp = 112
10895
YDOT = 2317
555882 meter/sec RA = 355
74682 deg
ZDOT = 3515
229339 TA = 193
73305
MA = 193
77072
Ha = 223
279 n
mi
Hp = 213
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12178991
64 X = 3774265
59
Y = -12154024
97 feet Y = -3662687
83 meter
Z = -14156510
10 Z = -4296720
86
XDOT = 20978
348943 XDOT = 6350
734813
YDOT = 7603
529797 feet/sec YDOT = 2388
817392 meter/sec
ZDOT = 11532
904657 ZDOT = 3546
184528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17157250
11 X = 5229529
83
Y = 1998832
06 feet Y = 609244
01 meter
Z = -14074387
29 Z = -4289873
25
XDOT = 7254
067522 XDOT = 2211
039781
YDOT = 19824
011636 feet/sec YDOT = 6042
358747 meter/sec
ZDOT = 11671
467705 ZDOT = 3557
463356
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 18244
92210856
00016717 00000-0 10270-3 0 9043
2 25544 51
6385 356
3020 0005487 116
1412 244
0305 15
53898391 10448
Satellite: ISS
Catalog Number: 25544
Epoch time: 18244
92210856 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 356
3020 deg
Eccentricity:
0005487
Arg of perigee: 116
1412 deg
Mean anomaly: 244
0305 deg
Mean motion: 15
53898391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 295
Coasting Arc #6 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2018/245/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5002351
89 A = 6785845
34 meter
Y = 3330096
09 meter E =
0018098
Z = 3132261
56 I = 51
58780
XDOT = -5093
408246 Wp = 101
67338
YDOT = -3068
916325 meter/sec RA = 350
76030 deg
ZDOT = -4851
484902 TA = 42
17803
MA = 42
03893
Ha = 223
260 n
mi
Hp = 213
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16411915
63 X = -5054433
04
Y = 10925512
10 feet Y = 3273865
21 meter
Z = 10276448
70 Z = 3107835
27
XDOT = -16710
656975 XDOT = -5035
146248
YDOT = -10068
623115 feet/sec YDOT = -3125
548717 meter/sec
ZDOT = -15916
945215 ZDOT = -4876
085336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18925136
10 X = -5768381
48
Y = -5727761
57 feet Y = -1745821
73 meter
Z = 10166373
91 Z = 3098710
77
XDOT = -3248
475166 XDOT = -990
135231
YDOT = -17831
882698 feet/sec YDOT = -5435
157846 meter/sec
ZDOT = -16026
879455 ZDOT = -4884
992858
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 18245
95107851
00016717 00000-0 10270-3 0 9058
2 25544 51
6394 351
1737 0005431 118
9178 241
2519 15
53926114 10603
Satellite: ISS
Catalog Number: 25544
Epoch time: 18245
95107851 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 351
1737 deg
Eccentricity:
0005431
Arg of perigee: 118
9178 deg
Mean anomaly: 241
2519 deg
Mean motion: 15
53926114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 305
Coasting Arc #7 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2018/246/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5909899
58 A = 6788764
96 meter
Y = -2881241
51 meter E =
0009981
Z = -1690209
61 I = 51
56448
XDOT = 3463
687382 Wp = 70
24377
YDOT = 3783
008019 meter/sec RA = 345
78119 deg
ZDOT = 5692
898133 TA = 271
22308
MA = 271
33742
Ha = 223
193 n
mi
Hp = 213
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19389434
30 X = 5949889
31
Y = -9452892
11 feet Y = -2814929
35 meter
Z = -5545307
13 Z = -1661404
26
XDOT = 11363
803748 XDOT = 3393
474271
YDOT = 12411
443633 feet/sec YDOT = 3821
348872 meter/sec
ZDOT = 18677
487314 ZDOT = 5709
552897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19819798
78 X = 6041074
67
Y = 8596744
42 feet Y = 2620287
70 meter
Z = -5415655
52 Z = -1650691
80
XDOT = -1482
811890 XDOT = -451
961064
YDOT = 15166
541626 feet/sec YDOT = 4622
761888 meter/sec
ZDOT = 18751
666053 ZDOT = 5715
507813
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 18246
91573374
00016717 00000-0 10270-3 0 9063
2 25544 51
6387 346
3667 0005436 121
9779 238
1903 15
53922904 10750
Satellite: ISS
Catalog Number: 25544
Epoch time: 18246
91573374 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 346
3667 deg
Eccentricity:
0005436
Arg of perigee: 121
9779 deg
Mean anomaly: 238
1903 deg
Mean motion: 15
53922904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 337
Coasting Arc #8 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2018/247/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6395685
93 A = 6789918
02 meter
Y = 2255999
52 meter E =
0017432
Z = 35018
92 I = 51
53752
XDOT = -1625
806057 Wp = 131
51918
YDOT = -4485
989641 meter/sec RA = 340
80535 deg
ZDOT = -6006
202041 TA = 48
10298
MA = 47
95443
Ha = 223
072 n
mi
Hp = 213
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20983221
57 X = -6420607
91
Y = 7401573
24 feet Y = 2184339
19 meter
Z = 114891
48 Z = 3890
53
XDOT = -5334
009372 XDOT = -1546
346857
YDOT = -14717
813783 feet/sec YDOT = -4503
726319 meter/sec
ZDOT = -19705
387275 ZDOT = -6013
906550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19464113
44 X = -5932661
78
Y = -10781453
18 feet Y = -3286186
93 meter
Z = -25086
55 Z = -7646
38
XDOT = 6769
355167 XDOT = 2063
299455
YDOT = -12242
324500 feet/sec YDOT = -3731
460508 meter/sec
ZDOT = -19739
311136 ZDOT = -6016
542034
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 18247
94469651
00016717 00000-0 10270-3 0 9070
2 25544 51
6396 341
2385 0005374 126
4306 233
7342 15
53926863 10912
Satellite: ISS
Catalog Number: 25544
Epoch time: 18247
94469651 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 341
2385 deg
Eccentricity:
0005374
Arg of perigee: 126
4306 deg
Mean anomaly: 233
7342 deg
Mean motion: 15
53926863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 326
Coasting Arc #9 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2018/248/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6423148
20 A = 6788758
76 meter
Y = -1512305
11 meter E =
0016748
Z = 1572253
78 I = 51
50330
XDOT = -215
685044 Wp = 79
76530
YDOT = 5091
980301 meter/sec RA = 335
82753 deg
ZDOT = 5729
837997 TA = 297
46091
MA = 297
63111
Ha = 222
994 n
mi
Hp = 213
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21073320
87 X = 6431944
73
Y = -4961630
94 feet Y = -1440427
80 meter
Z = 5158312
91 Z = 1603476
28
XDOT = -707
628097 XDOT = -300
441199
YDOT = 16705
972117 feet/sec YDOT = 5089
094577 meter/sec
ZDOT = 18798
681094 ZDOT = 5728
584325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17886852
53 X = 5451912
65
Y = 12136562
99 feet Y = 3699224
40 meter
Z = 5298600
91 Z = 1615013
56
XDOT = -11981
689612 XDOT = -3652
018994
YDOT = 9385
702585 feet/sec YDOT = 2860
762148 meter/sec
ZDOT = 18792
334725 ZDOT = 5727
903624
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 18248
97365368
00016717 00000-0 10270-3 0 9085
2 25544 51
6399 336
1109 0005316 130
2532 229
9087 15
53945861 11072
Satellite: ISS
Catalog Number: 25544
Epoch time: 18248
97365368 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 336
1109 deg
Eccentricity:
0005316
Arg of perigee: 130
2532 deg
Mean anomaly: 229
9087 deg
Mean motion: 15
53945861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 331
Coasting Arc #10 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2018/249/00:35:13
064
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -214112
15 A = 6778975
89 meter
Y = -4419275
23 meter E =
0017966
Z = -5152022
41 I = 51
46838
XDOT = 7227
913124 Wp = 109
03129
YDOT = -2053
452231 meter/sec RA = 335
24217 deg
ZDOT = 1459
460052 TA = 175
08501
MA = 175
06734
Ha = 222
984 n
mi
Hp = 213
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -702467
69 X = -139653
14
Y = -14498934
50 feet Y = -4421253
37 meter
Z = -16902960
66 Z = -5152881
54
XDOT = 23713
625736 XDOT = 7243
248993
YDOT = -6737
048001 feet/sec YDOT = -1972
538919 meter/sec
ZDOT = 4788
254765 ZDOT = 1494
607669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1184355
66 X = 360991
61
Y = -14463772
28 feet Y = -4408557
79 meter
Z = -16906189
24 Z = -5153006
48
XDOT = 23271
823124 XDOT = 7093
251688
YDOT = -3881
838453 feet/sec YDOT = -1183
184361 meter/sec
ZDOT = 4946
227797 ZDOT = 1507
610233
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 18249
03796329
00016717 00000-0 10270-3 0 9099
2 25544 51
6423 335
7912 0004807 132
9338 227
2219 15
53832528 11088
Satellite: ISS
Catalog Number: 25544
Epoch time: 18249
03796329 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 335
7912 deg
Eccentricity:
0004807
Arg of perigee: 132
9338 deg
Mean anomaly: 227
2219 deg
Mean motion: 15
53832528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1108
Checksum: 321
Coasting Arc #11 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2018/249/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3034253
86 A = 6778424
56 meter
Y = 3069361
89 meter E =
0008246
Z = 5222069
98 I = 51
43790
XDOT = -6198
892915 Wp = 129
71330
YDOT = 4408
171998 meter/sec RA = 330
62646 deg
ZDOT = 1004
624408 TA = 310
61101
MA = 310
68271
Ha = 222
778 n
mi
Hp = 213
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9954901
13 X = 2974340
18
Y = 10070084
95 feet Y = 3102958
23 meter
Z = 17132775
51 Z = 5236663
49
XDOT = -20337
575179 XDOT = -6252
605473
YDOT = 14462
506554 feet/sec YDOT = 4338
551397 meter/sec
ZDOT = 3296
011838 ZDOT = 974
382111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3032211
64 X = 924218
11
Y = 13750618
89 feet Y = 4191188
64 meter
Z = 17197814
89 Z = 5241893
98
XDOT = -23924
225817 XDOT = -7292
104029
YDOT = 1298
336103 feet/sec YDOT = 395
732844 meter/sec
ZDOT = 3159
723592 ZDOT = 963
083751
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18250
00268079
00016717 00000-0 10270-3 0 9106
2 25544 51
6407 330
9843 0004773 136
5661 223
5868 15
53863511 11233
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
00268079 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 330
9843 deg
Eccentricity:
0004773
Arg of perigee: 136
5661 deg
Mean anomaly: 223
5868 deg
Mean motion: 15
53863511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 303
Coasting Arc #12 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2018/250/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1595697
41 A = 6778463
52 meter
Y = -3991467
37 meter E =
0018327
Z = -5257016
94 I = 51
40966
XDOT = 6628
165488 Wp = 106
40197
YDOT = -3738
882755 meter/sec RA = 325
61466 deg
ZDOT = 824
237160 TA = 171
53203
MA = 171
50106
Ha = 222
905 n
mi
Hp = 213
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5235227
71 X = -1525409
68
Y = -13095365
40 feet Y = -4008918
91 meter
Z = -17247430
90 Z = -5264597
19
XDOT = 21745
949763 XDOT = 6665
478445
YDOT = -12266
675704 feet/sec YDOT = -3664
553330 meter/sec
ZDOT = 2704
190156 ZDOT = 856
524882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2335715
74 X = 711926
16
Y = -13866704
28 feet Y = -4226571
46 meter
Z = -17280886
00 Z = -5267214
05
XDOT = 23931
591717 XDOT = 7294
349155
YDOT = 468
996767 feet/sec YDOT = 142
950215 meter/sec
ZDOT = 2849
546441 ZDOT = 868
541755
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18250
96739823
00016717 00000-0 10270-3 0 9112
2 25544 51
6411 326
1774 0004798 138
7840 221
3676 15
53835841 11382
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
96739823 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 326
1774 deg
Eccentricity:
0004798
Arg of perigee: 138
7840 deg
Mean anomaly: 221
3676 deg
Mean motion: 15
53835841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 328
Coasting Arc #13 (Orbit 1153)
---------------------------------------
Vector Time (GMT): 2018/251/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 170067
58 A = 6780418
52 meter
Y = 4798833
15 meter E =
0009389
Z = 4778918
31 I = 51
38946
XDOT = -6660
766006 Wp = 90
58989
YDOT = 2806
944405 meter/sec RA = 320
60459 deg
ZDOT = -2577
309821 TA = 24
88841
MA = 24
84316
Ha = 222
761 n
mi
Hp = 213
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 557964
51 X = 93179
90
Y = 15744203
26 feet Y = 4800305
50 meter
Z = 15678865
85 Z = 4779557
24
XDOT = -21852
906845 XDOT = -6679
139953
YDOT = 9209
135186 feet/sec YDOT = 2732
356129 meter/sec
ZDOT = -8455
740881 ZDOT = -2609
709959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7462760
52 X = -2274649
41
Y = 13871876
44 feet Y = 4228147
94 meter
Z = 15681082
37 Z = 4779593
91
XDOT = -22472
344222 XDOT = -6849
570519
YDOT = -2350
411898 feet/sec YDOT = -716
405546 meter/sec
ZDOT = -8601
458364 ZDOT = -2621
724509
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18251
99642492
00016717 00000-0 10270-3 0 9122
2 25544 51
6409 321
0510 0004689 142
9437 217
2040 15
53854227 11545
Satellite: ISS
Catalog Number: 25544
Epoch time: 18251
99642492 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 321
0510 deg
Eccentricity:
0004689
Arg of perigee: 142
9437 deg
Mean anomaly: 217
2040 deg
Mean motion: 15
53854227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1154
Checksum: 301
Coasting Arc #14 (Orbit 1168)
---------------------------------------
Vector Time (GMT): 2018/252/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1137499
30 A = 6783776
67 meter
Y = -5454661
03 meter E =
0010390
Z = -3881532
41 I = 51
37647
XDOT = 6282
334480 Wp = 121
91336
YDOT = -1590
761188 meter/sec RA = 315
59824 deg
ZDOT = 4079
211837 TA = 191
06347
MA = 191
08634
Ha = 222
753 n
mi
Hp = 213
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3731953
09 X = 1217264
55
Y = -17895869
53 feet Y = -5441495
17 meter
Z = -12734686
39 Z = -3875812
55
XDOT = 20611
333597 XDOT = 6279
841428
YDOT = -5219
032768 feet/sec YDOT = -1520
521251 meter/sec
ZDOT = 13383
240935 ZDOT = 4109
723063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12001115
44 X = 3657939
98
Y = -13814270
97 feet Y = -4210589
79 meter
Z = -12708304
51 Z = -3873491
21
XDOT = 19476
517442 XDOT = 5936
442516
YDOT = 4490
389727 feet/sec YDOT = 1368
670789 meter/sec
ZDOT = 13520
307934 ZDOT = 4120
989858
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18252
96113374
00016717 00000-0 10270-3 0 9133
2 25544 51
6416 316
2435 0004704 145
6135 214
5323 15
53855037 11698
Satellite: ISS
Catalog Number: 25544
Epoch time: 18252
96113374 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 316
2435 deg
Eccentricity:
0004704
Arg of perigee: 145
6135 deg
Mean anomaly: 214
5323 deg
Mean motion: 15
53855037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1169
Checksum: 295
Coasting Arc #15 (Orbit 1176)
---------------------------------------
Vector Time (GMT): 2018/253/11:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2877757
43 A = 6778259
73 meter
Y = -3125444
85 meter E =
0017819
Z = -5296658
17 I = 51
34455
XDOT = 5384
941998 Wp = 105
66490
YDOT = -5433
939054 meter/sec RA = 313
08213 deg
ZDOT = 276
790905 TA = 167
01190
MA = 166
96595
Ha = 222
747 n
mi
Hp = 213
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9441461
39 X = -2816865
77
Y = -10254084
15 feet Y = -3157286
08 meter
Z = -17377487
43 Z = -5310488
95
XDOT = 17667
132539 XDOT = 5443
961098
YDOT = -17827
884035 feet/sec YDOT = -5373
390869 meter/sec
ZDOT = 908
106644 ZDOT = 303
092881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3928221
37 X = 1197321
87
Y = 13293270
66 feet Y = 4051788
90 meter
Z = -17439109
39 Z = -5315440
54
XDOT = -22692
946642 XDOT = -6916
810136
YDOT = 8069
779997 feet/sec YDOT = 2459
668943 meter/sec
ZDOT = 1026
794994 ZDOT = 312
967114
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18253
47564300
00016717 00000-0 10270-3 0 9140
2 25544 51
6402 313
6778 0004870 151
5809 208
5610 15
53830826 11772
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
47564300 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 313
6778 deg
Eccentricity:
0004870
Arg of perigee: 151
5809 deg
Mean anomaly: 208
5610 deg
Mean motion: 15
53830826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1177
Checksum: 306
Coasting Arc #16 (Orbit 1184)
---------------------------------------
Vector Time (GMT): 2018/253/22:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4373926
75 A = 6779134
31 meter
Y = 1115750
08 meter E =
0009786
Z = 5053742
88 I = 51
33747
XDOT = -3707
061393 Wp = 136
26274
YDOT = 6479
050080 meter/sec RA = 310
70614 deg
ZDOT = 1768
968528 TA = 296
51063
MA = 296
61095
Ha = 222
557 n
mi
Hp = 214
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14350153
38 X = 4336576
74
Y = 3660597
37 feet Y = 1164454
13 meter
Z = 16580521
26 Z = 5074898
94
XDOT = -12162
274913 XDOT = -3787
829090
YDOT = 21256
725984 feet/sec YDOT = 6437
143762 meter/sec
ZDOT = 5803
702520 ZDOT = 1750
764044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9953215
91 X = 3033740
21
Y = 10821722
80 feet Y = 3298461
11 meter
Z = 16675262
18 Z = 5082619
91
XDOT = -21015
216798 XDOT = -6405
438080
YDOT = 10467
522490 feet/sec YDOT = 3190
500855 meter/sec
ZDOT = 5721
204262 ZDOT = 1743
823059
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18253
99015365
00016717 00000-0 10270-3 0 9150
2 25544 51
6404 311
1162 0004738 149
9584 210
1841 15
53861933 11855
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
99015365 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 311
1162 deg
Eccentricity:
0004738
Arg of perigee: 149
9584 deg
Mean anomaly: 210
1841 deg
Mean motion: 15
53861933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1185
Checksum: 309
Coasting Arc #17 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2018/254/22:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3411670
14 A = 6778118
90 meter
Y = -2524533
04 meter E =
0017404
Z = -5299596
11 I = 51
31357
XDOT = 4498
741318 Wp = 104
05440
YDOT = -6194
118269 meter/sec RA = 305
68776 deg
ZDOT = 50
533965 TA = 166
45352
MA = 166
40675
Ha = 222
554 n
mi
Hp = 214
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11193143
51 X = -3357443
90
Y = -8282588
72 feet Y = -2562382
13 meter
Z = -17387126
33 Z = -5316036
81
XDOT = 14759
649993 XDOT = 4567
425844
YDOT = -20321
910332 feet/sec YDOT = -6143
426179 meter/sec
ZDOT = 165
793847 ZDOT = 72
554845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5007312
50 X = -1526228
85
Y = -12894048
64 feet Y = -3930106
02 meter
Z = -17460533
52 Z = -5321970
62
XDOT = 22342
227513 XDOT = 6809
910946
YDOT = -9053
495482 feet/sec YDOT = -2759
505423 meter/sec
ZDOT = 265
354421 ZDOT = 80
880027
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18254
95485787
00016717 00000-0 10270-3 0 9167
2 25544 51
6407 306
3093 0004599 154
3865 205
7516 15
53868427 12006
Satellite: ISS
Catalog Number: 25544
Epoch time: 18254
95485787 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 306
3093 deg
Eccentricity:
0004599
Arg of perigee: 154
3865 deg
Mean anomaly: 205
7516 deg
Mean motion: 15
53868427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 337
Coasting Arc #18 (Orbit 1215)
---------------------------------------
Vector Time (GMT): 2018/255/22:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2390976
78 A = 6779184
52 meter
Y = 3862728
11 meter E =
0006361
Z = 5026154
09 I = 51
29935
XDOT = -5000
858099 Wp = 98
76099
YDOT = 5514
574792 meter/sec RA = 300
66804 deg
ZDOT = -1858
083578 TA = 9
32224
MA = 9
31044
Ha = 222
299 n
mi
Hp = 214
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7844412
00 X = 2323190
48
Y = 12672992
47 feet Y = 3889087
18 meter
Z = 16490006
84 Z = 5037603
61
XDOT = -16407
014762 XDOT = -5053
126305
YDOT = 18092
436982 feet/sec YDOT = 5458
359282 meter/sec
ZDOT = -6096
074731 ZDOT = -1882
503637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 101882
73 X = 31053
85
Y = 14847539
75 feet Y = 4525530
12 meter
Z = 16540859
92 Z = 5041654
10
XDOT = -22264
028480 XDOT = -6786
075881
YDOT = 7070
758486 feet/sec YDOT = 2155
167186 meter/sec
ZDOT = -6206
293272 ZDOT = -1891
678189
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18255
98387061
00016717 00000-0 10270-3 0 9178
2 25544 51
6410 301
1815 0004474 158
8206 201
3132 15
53902739 12163
Satellite: ISS
Catalog Number: 25544
Epoch time: 18255
98387061 = yrday
fracday
Element set: 917
Inclination: 51
6410 deg
RA of node: 301
1815 deg
Eccentricity:
0004474
Arg of perigee: 158
8206 deg
Mean anomaly: 201
3132 deg
Mean motion: 15
53902739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1216
Checksum: 295
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