[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 8th 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) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
040/08:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
5
042/08:58:45
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
6
042/12:24:48
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
6
043/19:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
6
048/05:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
6
052/22:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
7
Coasting Arc #1 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2018/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1935716
39 A = 6787233
71 meter
Y = -6079270
90 meter E =
0008787
Z = -2312645
11 I = 51
34474
XDOT = 5442
699076 Wp = 54
44526
YDOT = -309
113911 meter/sec RA = 304
51644 deg
ZDOT = 5387
663486 TA = 279
68095
MA = 279
78020
Ha = 222
228 n
mi
Hp = 213
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6350775
56 X = 2014786
04
Y = -19945114
51 feet Y = -6057182
37 meter
Z = -7587418
33 Z = -2303049
92
XDOT = 17856
624264 XDOT = 5419
581078
YDOT = -1014
153251 feet/sec YDOT = -248
378975 meter/sec
ZDOT = 17676
061307 ZDOT = 5414
045743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18339436
67 X = 5589860
30
Y = -10122532
88 feet Y = -3085348
02 meter
Z = -7543755
73 Z = -2299336
75
XDOT = 12864
517020 XDOT = 3921
104788
YDOT = 10094
601844 feet/sec YDOT = 3076
834642 meter/sec
ZDOT = 17793
512524 ZDOT = 5423
462617
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 18038
50457807
00016717 00000-0 10270-3 0 9003
2 25544 51
6413 305
2130 0003198 73
6773 286
4731 15
54076518 18349
Satellite: ISS
Catalog Number: 25544
Epoch time: 18038
50457807 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 305
2130 deg
Eccentricity:
0003198
Arg of perigee: 73
6773 deg
Mean anomaly: 286
4731 deg
Mean motion: 15
54076518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 306
Coasting Arc #2 (Orbit 1849)
---------------------------------------
Vector Time (GMT): 2018/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2851963
13 A = 6789399
53 meter
Y = 6118308
78 meter E =
0015391
Z = 666632
08 I = 51
33386
XDOT = -4615
896481 Wp = 119
09115
YDOT = -1493
945761 meter/sec RA = 299
52426 deg
ZDOT = -5939
546583 TA = 53
67803
MA = 53
53602
Ha = 222
247 n
mi
Hp = 213
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9356834
41 X = -2923405
85
Y = 20073191
52 feet Y = 6086016
72 meter
Z = 2187113
13 Z = 652604
75
XDOT = -15144
017325 XDOT = -4569
996925
YDOT = -4901
396855 feet/sec YDOT = -1545
307396 meter/sec
ZDOT = -19486
701389 ZDOT = -5961
857180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20444625
44 X = -6231521
84
Y = 8530761
18 feet Y = 2600176
01 meter
Z = 2123731
64 Z = 647313
40
XDOT = -7177
611758 XDOT = -2187
736064
YDOT = -12244
504752 feet/sec YDOT = -3732
125048 meter/sec
ZDOT = -19585
748687 ZDOT = -5969
736200
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 18039
53345236
00016717 00000-0 10270-3 0 9010
2 25544 51
6413 300
0852 0003111 79
5421 280
6082 15
54043852 18501
Satellite: ISS
Catalog Number: 25544
Epoch time: 18039
53345236 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 300
0852 deg
Eccentricity:
0003111
Arg of perigee: 79
5421 deg
Mean anomaly: 280
6082 deg
Mean motion: 15
54043852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1850
Checksum: 275
Coasting Arc #3 (Orbit 1862)
---------------------------------------
Vector Time (GMT): 2018/040/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4453664
41 A = 6778281
96 meter
Y = -184143
45 meter E =
0016799
Z = -5121553
73 I = 51
28226
XDOT = 2053
598762 Wp = 78
47087
YDOT = -7215
161926 meter/sec RA = 295
28129 deg
ZDOT = -1527
352915 TA = 176
71953
MA = 176
70850
Ha = 222
213 n
mi
Hp = 213
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14611759
87 X = -4426396
83
Y = -604145
19 feet Y = -233795
02 meter
Z = -16802997
79 Z = -5143121
53
XDOT = 6737
528746 XDOT = 2141
546991
YDOT = -23671
791097 feet/sec YDOT = -7191
705456 meter/sec
ZDOT = -5011
000376 ZDOT = -1517
163650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1926687
76 X = 587254
43
Y = -14384810
14 feet Y = -4384490
13 meter
Z = -16898945
65 Z = -5150798
63
XDOT = 21906
357141 XDOT = 6677
057657
YDOT = 8762
595487 feet/sec YDOT = 2670
839104 meter/sec
ZDOT = -4964
536768 ZDOT = -1513
190807
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 18040
36940892
00016717 00000-0 10270-3 0 9023
2 25544 51
6397 295
9164 0003117 79
5094 280
6409 15
54072086 18630
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
36940892 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 295
9164 deg
Eccentricity:
0003117
Arg of perigee: 79
5094 deg
Mean anomaly: 280
6409 deg
Mean motion: 15
54072086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1863
Checksum: 327
Coasting Arc #4 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2018/041/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3820633
53 A = 6777513
19 meter
Y = 1864620
71 meter E =
0005744
Z = 5273533
64 I = 51
26678
XDOT = -2934
310276 Wp = 76
70467
YDOT = 7079
936782 meter/sec RA = 290
25768 deg
ZDOT = -375
800440 TA = 16
90455
MA = 16
88542
Ha = 222
060 n
mi
Hp = 213
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12534886
92 X = 3773883
28
Y = 6117522
00 feet Y = 1907084
33 meter
Z = 17301619
57 Z = 5291979
07
XDOT = -9627
002217 XDOT = -3011
436552
YDOT = 23228
139047 feet/sec YDOT = 7046
692066 meter/sec
ZDOT = -1232
941076 ZDOT = -390
241482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7022980
14 X = -2140604
35
Y = 11932648
08 feet Y = 3637071
13 meter
Z = 17383416
38 Z = 5298465
31
XDOT = -21580
807013 XDOT = -6577
829978
YDOT = -10802
250599 feet/sec YDOT = -3292
525983 meter/sec
ZDOT = -1298
291065 ZDOT = -395
719117
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 18041
39827660
00016717 00000-0 10270-3 0 9035
2 25544 51
6397 290
7888 0003128 80
7539 279
3967 15
54087921 18791
Satellite: ISS
Catalog Number: 25544
Epoch time: 18041
39827660 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 290
7888 deg
Eccentricity:
0003128
Arg of perigee: 80
7539 deg
Mean anomaly: 279
3967 deg
Mean motion: 15
54087921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 360
Coasting Arc #5 (Orbit 1893)
---------------------------------------
Vector Time (GMT): 2018/042/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3133570
00 A = 6779197
84 meter
Y = -3487115
60 meter E =
0015194
Z = -4910796
51 I = 51
26141
XDOT = 3596
791885 Wp = 101
98946
YDOT = -6378
219918 meter/sec RA = 285
23363 deg
ZDOT = 2236
809245 TA = 189
99135
MA = 190
02159
Ha = 222
221 n
mi
Hp = 213
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10280741
46 X = -3070489
64
Y = -11440667
96 feet Y = -3521804
69 meter
Z = -16111537
12 Z = -4925864
75
XDOT = 11800
498312 XDOT = 3656
982520
YDOT = -20925
918367 feet/sec YDOT = -6337
661544 meter/sec
ZDOT = 7338
613009 ZDOT = 2254
427153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12003096
86 X = 3658543
92
Y = -9505788
57 feet Y = -2897364
36 meter
Z = -16178065
58 Z = -4931074
39
XDOT = 19528
557568 XDOT = 5952
304347
YDOT = 12049
744129 feet/sec YDOT = 3672
762011 meter/sec
ZDOT = 7417
980329 ZDOT = 2261
000404
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 18042
36283944
00016717 00000-0 10270-3 0 9045
2 25544 51
6393 285
9809 0003152 85
0655 275
0858 15
54077546 18941
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
36283944 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 285
9809 deg
Eccentricity:
0003152
Arg of perigee: 85
0655 deg
Mean anomaly: 275
0858 deg
Mean motion: 15
54077546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1894
Checksum: 340
Coasting Arc #6 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2018/042/08:58:45
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4450781
68 A = 6779829
92 meter
Y = -1962295
48 meter E =
0010402
Z = 4715859
25 I = 51
26413
XDOT = 297
687801 Wp = 108
96630
YDOT = 7177
276614 meter/sec RA = 285
15541 deg
ZDOT = 2697
336070 TA = 314
20530
MA = 314
29070
Ha = 222
014 n
mi
Hp = 213
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14602302
10 X = 4449487
10
Y = -6437977
28 feet Y = -1912530
95 meter
Z = 15471979
18 Z = 4737476
07
XDOT = 976
666014 XDOT = 204
305450
YDOT = 23547
495452 feet/sec YDOT = 7180
083470 meter/sec
ZDOT = 8849
527790 ZDOT = 2698
555195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7723000
84 X = 2353970
66
Y = 13857661
66 feet Y = 4223815
27 meter
Z = 15568474
20 Z = 4745270
94
XDOT = -22357
861557 XDOT = -6814
676203
YDOT = 2483
219501 feet/sec YDOT = 756
885304 meter/sec
ZDOT = 8853
867584 ZDOT = 2698
658840
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 18042
42714253
00016717 00000-0 10270-3 0 9055
2 25544 51
6397 285
6610 0003053 86
9527 273
1975 15
54105122 18952
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
42714253 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 285
6610 deg
Eccentricity:
0003053
Arg of perigee: 86
9527 deg
Mean anomaly: 273
1975 deg
Mean motion: 15
54105122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 311
Coasting Arc #7 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2018/042/12:24:48
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1016853
54 A = 6785396
11 meter
Y = 5954633
78 meter E =
0016107
Z = 3075222
82 I = 51
28275
XDOT = -4889
194041 Wp = 93
20633
YDOT = 3358
816153 meter/sec RA = 284
39454 deg
ZDOT = -4865
882361 TA = 51
24122
MA = 51
09741
Ha = 222
167 n
mi
Hp = 213
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3336133
66 X = 935254
13
Y = 19536200
07 feet Y = 5965548
73 meter
Z = 10089313
72 Z = 3079963
97
XDOT = -16040
662865 XDOT = -4902
754443
YDOT = 11019
738036 feet/sec YDOT = 3304
065936 meter/sec
ZDOT = -15964
180975 ZDOT = -4889
664879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7946808
96 X = -2422187
37
Y = 18144781
71 feet Y = 5530529
47 meter
Z = 10109514
14 Z = 3081379
91
XDOT = -18043
589677 XDOT = -5499
686133
YDOT = 1090
044087 feet/sec YDOT = 332
245438 meter/sec
ZDOT = -16070
524113 ZDOT = -4898
295750
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 18042
55575086
00016717 00000-0 10270-3 0 9069
2 25544 51
6412 285
0209 0003140 84
1101 276
0409 15
54096686 18973
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
55575086 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 285
0209 deg
Eccentricity:
0003140
Arg of perigee: 84
1101 deg
Mean anomaly: 276
0409 deg
Mean motion: 15
54096686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 306
Coasting Arc #8 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2018/043/12:24:48
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -191060
22 A = 6788388
09 meter
Y = -6596842
87 meter E =
0010225
Z = -1578447
04 I = 51
28552
XDOT = 4888
294087 Wp = 50
32753
YDOT = -1500
629184 meter/sec RA = 279
39380 deg
ZDOT = 5711
080938 TA = 292
32795
MA = 292
43630
Ha = 222
136 n
mi
Hp = 213
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -626838
00 X = -109611
25
Y = -21643185
27 feet Y = -6598524
06 meter
Z = -5178632
01 Z = -1579177
16
XDOT = 16037
710258 XDOT = 4876
970429
YDOT = -4923
324096 feet/sec YDOT = -1446
028118 meter/sec
ZDOT = 18737
142185 ZDOT = 5734
798569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11020991
76 X = 3359198
29
Y = -18636915
39 feet Y = -5680531
81 meter
Z = -5180902
39 Z = -1579139
05
XDOT = 14732
323457 XDOT = 4490
412190
YDOT = 3502
237421 feet/sec YDOT = 1067
481966 meter/sec
ZDOT = 18842
915910 ZDOT = 5743
320769
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 18043
52031029
00016717 00000-0 10270-3 0 9072
2 25544 51
6412 280
2128 0002959 87
0254 273
1237 15
54086717 19127
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
52031029 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 280
2128 deg
Eccentricity:
0002959
Arg of perigee: 87
0254 deg
Mean anomaly: 273
1237 deg
Mean motion: 15
54086717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 293
Coasting Arc #9 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3608113
87 A = 6779007
04 meter
Y = 2889377
16 meter E =
0008819
Z = 4952292
30 I = 51
25140
XDOT = -2653
760503 Wp = 71
11091
YDOT = 6892
233187 meter/sec RA = 277
98329 deg
ZDOT = -2081
901954 TA = 39
27922
MA = 39
21527
Ha = 222
158 n
mi
Hp = 213
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11837643
92 X = 3551480
84
Y = 9479583
87 feet Y = 2929409
03 meter
Z = 16247678
15 Z = 4969681
24
XDOT = -8706
563331 XDOT = -2720
521541
YDOT = 22612
313606 feet/sec YDOT = 6862
183682 meter/sec
ZDOT = -6830
386989 ZDOT = -2094
955017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13066852
35 X = 3982776
60
Y = -7532788
76 feet Y = -2295994
01 meter
Z = 16324638
81 Z = 4975749
91
XDOT = 17431
022482 XDOT = 5312
975653
YDOT = 15264
980594 feet/sec YDOT = 4652
766085 meter/sec
ZDOT = -6889
495501 ZDOT = -2099
918229
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 18043
84183171
00016717 00000-0 10270-3 0 9084
2 25544 51
6402 278
6047 0003234 99
2397 260
9122 15
54059746 19171
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
84183171 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 278
6047 deg
Eccentricity:
0003234
Arg of perigee: 99
2397 deg
Mean anomaly: 260
9122 deg
Mean motion: 15
54059746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 319
Coasting Arc #10 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2018/044/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3089479
61 A = 6782171
12 meter
Y = -4414494
60 meter E =
0010742
Z = -4130025
62 I = 51
25841
XDOT = 3305
892448 Wp = 107
14687
YDOT = -5808
247755 meter/sec RA = 272
96517 deg
ZDOT = 3740
308163 TA = 201
59675
MA = 201
64209
Ha = 222
184 n
mi
Hp = 213
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10136087
96 X = -3019824
94
Y = -14483249
99 feet Y = -4448653
97 meter
Z = -13549952
83 Z = -4144863
53
XDOT = 10846
103832 XDOT = 3352
428157
YDOT = -19055
930956 feet/sec YDOT = -5771
018662 meter/sec
ZDOT = 12271
352242 ZDOT = 3756
479878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17055131
77 X = -5198404
16
Y = 4455418
33 feet Y = 1358011
51 meter
Z = -13615350
11 Z = -4149958
71
XDOT = -13868
556400 XDOT = -4227
135991
YDOT = -15415
253950 feet/sec YDOT = -4698
569404 meter/sec
ZDOT = 12344
166340 ZDOT = 3762
501900
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 18044
80638712
00016717 00000-0 10270-3 0 9098
2 25544 51
6399 273
7977 0003119 101
8330 258
3173 15
54083504 19326
Satellite: ISS
Catalog Number: 25544
Epoch time: 18044
80638712 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 273
7977 deg
Eccentricity:
0003119
Arg of perigee: 101
8330 deg
Mean anomaly: 258
3173 deg
Mean motion: 15
54083504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 318
Coasting Arc #11 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2018/045/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2486686
13 A = 6786009
01 meter
Y = 5625727
48 meter E =
0016518
Z = 2848360
95 I = 51
26968
XDOT = -3891
147723 Wp = 100
67366
YDOT = 4282
392280 meter/sec RA = 267
95592 deg
ZDOT = -5039
047424 TA = 46
73316
MA = 46
59546
Ha = 222
179 n
mi
Hp = 213
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8158419
08 X = 2409757
44
Y = 18457111
15 feet Y = 5653105
33 meter
Z = 9345016
23 Z = 2860252
95
XDOT = -12766
232686 XDOT = -3914
268994
YDOT = 14049
843439 feet/sec YDOT = 4238
749249 meter/sec
ZDOT = -16532
307823 ZDOT = -5058
005163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20091637
28 X = 6123931
04
Y = -1604320
50 feet Y = -488996
89 meter
Z = 9397145
79 Z = 2864250
04
XDOT = 9010
959850 XDOT = 2746
540562
YDOT = 15095
033487 feet/sec YDOT = 4600
966207 meter/sec
ZDOT = -16617
290807 ZDOT = -5064
950238
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 18045
83524620
00016717 00000-0 10270-3 0 9106
2 25544 51
6392 268
6691 0003217 107
3962 252
7542 15
54074388 19481
Satellite: ISS
Catalog Number: 25544
Epoch time: 18045
83524620 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 268
6691 deg
Eccentricity:
0003217
Arg of perigee: 107
3962 deg
Mean anomaly: 252
7542 deg
Mean motion: 15
54074388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1948
Checksum: 321
Coasting Arc #12 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2018/046/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1849542
83 A = 6788722
30 meter
Y = -6396190
42 meter E =
0010341
Z = -1311298
75 I = 51
28213
XDOT = 4379
440718 Wp = 54
04974
YDOT = -2446
808726 meter/sec RA = 262
95610 deg
ZDOT = 5795
998424 TA = 291
61124
MA = 291
72138
Ha = 222
165 n
mi
Hp = 213
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6068053
90 X = -1771512
00
Y = -20984876
72 feet Y = -6416437
08 meter
Z = -4302161
27 Z = -1320093
00
XDOT = 14368
243826 XDOT = 4378
322922
YDOT = -8027
587685 feet/sec YDOT = -2397
840657 meter/sec
ZDOT = 19015
742862 ZDOT = 5817
269141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21822666
22 X = -6651548
66
Y = -791807
31 feet Y = -241342
87 meter
Z = -4340414
83 Z = -1322958
44
XDOT = -3252
369623 XDOT = -991
322261
YDOT = -14441
769928 feet/sec YDOT = -4401
851474 meter/sec
ZDOT = 19110
755865 ZDOT = 5824
958388
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 18046
79979810
00016717 00000-0 10270-3 0 9118
2 25544 51
6403 263
8613 0003104 106
8308 253
3185 15
54080142 19630
Satellite: ISS
Catalog Number: 25544
Epoch time: 18046
79979810 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 263
8613 deg
Eccentricity:
0003104
Arg of perigee: 106
8308 deg
Mean anomaly: 253
3185 deg
Mean motion: 15
54080142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 302
Coasting Arc #13 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2018/047/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1090733
78 A = 6789354
90 meter
Y = 6682739
82 meter E =
0014176
Z = -408090
85 I = 51
28874
XDOT = -4798
583553 Wp = 132
17003
YDOT = 427
556232 meter/sec RA = 257
96143 deg
ZDOT = -5966
789812 TA = 52
25171
MA = 52
12335
Ha = 222
149 n
mi
Hp = 213
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3578522
88 X = 1017906
75
Y = 21924999
40 feet Y = 6694529
92 meter
Z = -1338880
73 Z = -402970
02
XDOT = -15743
384359 XDOT = -4774
025134
YDOT = 1402
743544 feet/sec YDOT = 374
031980 meter/sec
ZDOT = -19576
082061 ZDOT = -5990
039499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22007919
12 X = 6708013
75
Y = 3036617
03 feet Y = 925560
87 meter
Z = -1316996
47 Z = -401420
52
XDOT = -3043
348853 XDOT = -927
612731
YDOT = 13728
075527 feet/sec YDOT = 4184
317421 meter/sec
ZDOT = -19679
625005 ZDOT = -5998
349701
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 18047
82865120
00016717 00000-0 10270-3 0 9122
2 25544 51
6396 258
7324 0003170 111
6372 248
5118 15
54096035 19798
Satellite: ISS
Catalog Number: 25544
Epoch time: 18047
82865120 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 258
7324 deg
Eccentricity:
0003170
Arg of perigee: 111
6372 deg
Mean anomaly: 248
5118 deg
Mean motion: 15
54096035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 314
Coasting Arc #14 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2018/048/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4191357
67 A = 6782584
58 meter
Y = 3541894
79 meter E =
0013697
Z = 3975637
02 I = 51
26771
XDOT = -1638
831294 Wp = 83
77035
YDOT = 6376
962283 meter/sec RA = 255
72718 deg
ZDOT = -3940
293499 TA = 47
45692
MA = 47
34136
Ha = 222
019 n
mi
Hp = 213
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13751173
46 X = 4132128
63
Y = 11620389
75 feet Y = 3588434
63 meter
Z = 13043428
54 Z = 3995852
54
XDOT = -5376
743092 XDOT = -1690
878978
YDOT = 20921
792267 feet/sec YDOT = 6358
344370 meter/sec
ZDOT = -12927
472108 ZDOT = -3948
381185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17576311
04 X = -5357259
61
Y = 3585893
55 feet Y = 1092980
35 meter
Z = 13132932
47 Z = 4002917
82
XDOT = -12940
147848 XDOT = -3944
157064
YDOT = -15788
560017 feet/sec YDOT = -4812
353093 meter/sec
ZDOT = -12964
330220 ZDOT = -3951
527851
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 18048
27877403
00016717 00000-0 10270-3 0 9130
2 25544 51
6379 256
4914 0003022 101
5998 258
5494 15
54108334 19869
Satellite: ISS
Catalog Number: 25544
Epoch time: 18048
27877403 = yrday
fracday
Element set: 913
Inclination: 51
6379 deg
RA of node: 256
4914 deg
Eccentricity:
0003022
Arg of perigee: 101
5998 deg
Mean anomaly: 258
5494 deg
Mean motion: 15
54108334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 333
Coasting Arc #15 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2018/049/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3962510
22 A = 6786318
97 meter
Y = -4813217
02 meter E =
0007163
Z = -2683869
32 I = 51
28882
XDOT = 2620
622894 Wp = 75
04058
YDOT = -5025
374550 meter/sec RA = 250
72018 deg
ZDOT = 5156
689960 TA = 254
51306
MA = 254
59217
Ha = 222
096 n
mi
Hp = 213
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13000361
62 X = -3895356
46
Y = -15791394
44 feet Y = -4857153
33 meter
Z = -8805345
53 Z = -2702953
85
XDOT = 8597
844141 XDOT = 2651
575230
YDOT = -16487
449311 feet/sec YDOT = -4995
895360 meter/sec
ZDOT = 16918
274148 ZDOT = 5169
495470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20402284
40 X = 6218616
28
Y = -795231
27 feet Y = -242386
49 meter
Z = -8889659
66 Z = -2709568
26
XDOT = 7971
247387 XDOT = 2429
636204
YDOT = 15225
583627 feet/sec YDOT = 4640
757889 meter/sec
ZDOT = 16975
938214 ZDOT = 5174
265968
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 18049
24332187
00016717 00000-0 10270-3 0 9144
2 25544 51
6376 251
6835 0002981 106
2232 253
9249 15
54092151 20016
Satellite: ISS
Catalog Number: 25544
Epoch time: 18049
24332187 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 251
6835 deg
Eccentricity:
0002981
Arg of perigee: 106
2232 deg
Mean anomaly: 253
9249 deg
Mean motion: 15
54092151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 294
Coasting Arc #16 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2018/050/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3513037
27 A = 6788906
60 meter
Y = 5700465
30 meter E =
0016535
Z = 1072083
01 I = 51
31076
XDOT = -3636
830818 Wp = 120
86931
YDOT = 3354
850948 meter/sec RA = 245
72243 deg
ZDOT = -5862
046875 TA = 47
44503
MA = 47
30557
Ha = 222
066 n
mi
Hp = 213
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11525712
84 X = 3443824
50
Y = 18702313
99 feet Y = 5739363
62 meter
Z = 3517332
70 Z = 1088979
16
XDOT = -11931
859640 XDOT = -3645
601087
YDOT = 11006
728832 feet/sec YDOT = 3314
131758 meter/sec
ZDOT = -19232
437255 ZDOT = -5879
734710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21888066
48 X = -6671482
66
Y = -1732546
85 feet Y = -528080
28 meter
Z = 3591804
77 Z = 1094782
09
XDOT = -2058
182299 XDOT = -627
333965
YDOT = -14426
810860 feet/sec YDOT = -4397
291950 meter/sec
ZDOT = -19311
608182 ZDOT = -5886
178174
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 18050
27217021
00016717 00000-0 10270-3 0 9159
2 25544 51
6390 246
5541 0002966 109
6934 250
4539 15
54100435 20174
Satellite: ISS
Catalog Number: 25544
Epoch time: 18050
27217021 = yrday
fracday
Element set: 915
Inclination: 51
6390 deg
RA of node: 246
5541 deg
Eccentricity:
0002966
Arg of perigee: 109
6934 deg
Mean anomaly: 250
4539 deg
Mean motion: 15
54100435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 287
Coasting Arc #17 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2018/051/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2869793
32 A = 6789262
59 meter
Y = -6116335
18 meter E =
0014802
Z = 608487
98 I = 51
32610
XDOT = 4587
346623 Wp = 61
50002
YDOT = -1550
489595 meter/sec RA = 240
73004 deg
ZDOT = 5946
668762 TA = 305
09764
MA = 305
23633
Ha = 222
070 n
mi
Hp = 213
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9415332
41 X = -2804141
19
Y = -20066716
47 feet Y = -6148060
04 meter
Z = 1996351
65 Z = 594707
76
XDOT = 15050
349813 XDOT = 4575
458239
YDOT = -5086
908119 feet/sec YDOT = -1499
256605 meter/sec
ZDOT = 19510
068117 ZDOT = 5968
923515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21836629
72 X = 6655804
74
Y = 3836839
64 feet Y = 1169468
72 meter
Z = 1935788
79 Z = 590028
42
XDOT = -4147
935394 XDOT = -1264
290708
YDOT = 13537
143883 feet/sec YDOT = 4126
121455 meter/sec
ZDOT = 19609
335708 ZDOT = 5976
925524
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 18051
30101547
00016717 00000-0 10270-3 0 9160
2 25544 51
6388 241
4254 0002960 111
1901 248
9568 15
54101510 20339
Satellite: ISS
Catalog Number: 25544
Epoch time: 18051
30101547 = yrday
fracday
Element set: 916
Inclination: 51
6388 deg
RA of node: 241
4254 deg
Eccentricity:
0002960
Arg of perigee: 111
1901 deg
Mean anomaly: 248
9568 deg
Mean motion: 15
54101510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2033
Checksum: 273
Coasting Arc #18 (Orbit 2047)
---------------------------------------
Vector Time (GMT): 2018/052/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1948340
05 A = 6787211
22 meter
Y = 6089780
01 meter E =
0008767
Z = -2272613
40 I = 51
33729
XDOT = -5424
170426 Wp = 129
69927
YDOT = -275
870462 meter/sec RA = 235
73692 deg
ZDOT = -5408
880370 TA = 75
69925
MA = 75
60192
Ha = 222
038 n
mi
Hp = 213
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6392191
77 X = 1891136
74
Y = 19979593
20 feet Y = 6111247
63 meter
Z = -7456080
69 Z = -2263288
61
XDOT = -17795
834731 XDOT = -5394
409181
YDOT = -905
086817 feet/sec YDOT = -336
361345 meter/sec
ZDOT = -17745
670504 ZDOT = -5435
156558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20150268
86 X = -6141801
95
Y = -5883609
42 feet Y = -1793324
15 meter
Z = -7415335
76 Z = -2260194
34
XDOT = 10244
241357 XDOT = 3122
444766
YDOT = -12652
510841 feet/sec YDOT = -3856
485304 meter/sec
ZDOT = -17862
614254 ZDOT = -5444
524825
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 18052
26555600
00016717 00000-0 10270-3 0 9170
2 25544 51
6398 236
6175 0002931 115
5719 244
5737 15
54110598 20483
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
26555600 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 236
6175 deg
Eccentricity:
0002931
Arg of perigee: 115
5719 deg
Mean anomaly: 244
5737 deg
Mean motion: 15
54110598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2048
Checksum: 317
Coasting Arc #19 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2018/052/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -115018
60 A = 6781874
20 meter
Y = 5331602
85 meter E =
0010174
Z = -4199317
86 I = 51
33253
XDOT = -6028
204023 Wp = 84
06134
YDOT = -3000
522844 meter/sec RA = 232
17626 deg
ZDOT = -3651
075060 TA = 148
34510
MA = 148
28388
Ha = 222
038 n
mi
Hp = 213
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -377357
60 X = -154231
57
Y = 17492135
32 feet Y = 5330097
04 meter
Z = -13777289
57 Z = -4199972
24
XDOT = -19777
572255 XDOT = -5976
468481
YDOT = -9844
235053 feet/sec YDOT = -3067
645381 meter/sec
ZDOT = -11978
592717 ZDOT = -3680
231854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13001714
47 X = 3962922
57
Y = -11703587
00 feet Y = -3567253
32 meter
Z = -13780869
98 Z = -4200409
17
XDOT = 5354
682382 XDOT = 1632
107190
YDOT = 20180
149311 feet/sec YDOT = 6150
909510 meter/sec
ZDOT = -12108
027148 ZDOT = -3690
526675
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 18052
97288324
00016717 00000-0 10270-3 0 9185
2 25544 51
6392 233
0911 0003105 120
5317 239
6142 15
54123424 20599
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
97288324 = yrday
fracday
Element set: 918
Inclination: 51
6392 deg
RA of node: 233
0911 deg
Eccentricity:
0003105
Arg of perigee: 120
5317 deg
Mean anomaly: 239
6142 deg
Mean motion: 15
54123424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 288
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