[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 13th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
132/22:08:25
874 0
6 1
1 1
1
N/A 0
7 -0
1 222
5
000/00:02:51
749 -0
6 -0
0 213
4
134/06:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
4
137/14:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
4
140/09:04:46
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
4
144/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
4
Coasting Arc #1 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2018/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1944991
77 A = 6776980
16 meter
Y = -3764022
40 meter E =
0005763
Z = 5284787
87 I = 51
48290
XDOT = 7045
182644 Wp = 68
42292
YDOT = 3006
980412 meter/sec RA = 200
44107 deg
ZDOT = -448
724706 TA = 25
87786
MA = 25
84905
Ha = 221
780 n
mi
Hp = 213
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6381206
59 X = 1961266
50
Y = -12349154
87 feet Y = -3742181
18 meter
Z = 17338542
88 Z = 5294275
60
XDOT = 23114
116287 XDOT = 7013
213850
YDOT = 9865
421299 feet/sec YDOT = 3085
585749 meter/sec
ZDOT = -1472
193918 ZDOT = -414
578861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5062031
59 X = -1542907
23
Y = -12888423
81 feet Y = -3928391
58 meter
Z = 17381336
56 Z = 5297831
38
XDOT = 21798
930442 XDOT = 6644
313999
YDOT = -10352
903253 feet/sec YDOT = -3155
564912 meter/sec
ZDOT = -1320
099394 ZDOT = -402
366295
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 18131
54756556
00016717 00000-0 10270-3 0 9004
2 25544 51
6403 201
3634 0003139 64
5899 295
5579 15
54271695 32818
Satellite: ISS
Catalog Number: 25544
Epoch time: 18131
54756556 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 201
3634 deg
Eccentricity:
0003139
Arg of perigee: 64
5899 deg
Mean anomaly: 295
5579 deg
Mean motion: 15
54271695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 326
Coasting Arc #2 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2018/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3614386
61 A = 6778790
78 meter
Y = 3028950
60 meter E =
0014759
Z = -4883159
63 I = 51
51947
XDOT = -6280
842806 Wp = 99
03632
YDOT = -3685
478608 meter/sec RA = 195
43233 deg
ZDOT = 2366
726991 TA = 194
19855
MA = 194
24007
Ha = 221
949 n
mi
Hp = 213
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11858223
77 X = -3624268
33
Y = 9937501
98 feet Y = 2988476
83 meter
Z = -16020864
94 Z = -4900741
33
XDOT = -20606
439651 XDOT = -6250
660469
YDOT = -12091
465248 feet/sec YDOT = -3755
546578 meter/sec
ZDOT = 7764
852332 ZDOT = 2336
289614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -120834
75 X = -36830
43
Y = 15389090
11 feet Y = 4690594
67 meter
Z = -16099715
35 Z = -4907193
24
XDOT = -21510
043060 XDOT = -6556
261125
YDOT = 7799
603545 feet/sec YDOT = 2377
319160 meter/sec
ZDOT = 7629
377142 ZDOT = 2325
434153
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 18132
51202398
00016717 00000-0 10270-3 0 9013
2 25544 51
6397 196
5550 0003311 66
9519 293
1983 15
54250347 32969
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
51202398 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 196
5550 deg
Eccentricity:
0003311
Arg of perigee: 66
9519 deg
Mean anomaly: 293
1983 deg
Mean motion: 15
54250347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 316
Coasting Arc #3 (Orbit 3302)
---------------------------------------
Vector Time (GMT): 2018/132/22:09:51
749
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5944074
98 A = 6785507
85 meter
Y = -1096682
98 meter E =
0016718
Z = 3068475
38 I = 51
55380
XDOT = 3427
593294 Wp = 91
72322
YDOT = 4807
768572 meter/sec RA = 193
31422 deg
ZDOT = -4898
828420 TA = 52
96844
MA = 52
81562
Ha = 222
469 n
mi
Hp = 213
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19501558
32 X = 5940991
30
Y = -3598041
26 feet Y = -1030229
52 meter
Z = 10067176
44 Z = 3097342
65
XDOT = 11245
384824 XDOT = 3397
373116
YDOT = 15773
518936 feet/sec YDOT = 4845
929377 meter/sec
ZDOT = -16072
271719 ZDOT = -4882
251397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16631174
08 X = -5069181
86
Y = 10679246
19 feet Y = 3255034
24 meter
Z = 10196198
74 Z = 3107801
38
XDOT = -15694
014428 XDOT = -4783
535598
YDOT = -9095
820004 feet/sec YDOT = -2772
405937 meter/sec
ZDOT = -15998
807802 ZDOT = -4876
436618
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 18132
96211146
00016717 00000-0 10270-3 0 9024
2 25544 51
6402 194
3131 0003873 78
2500 281
9094 15
54034568 33038
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
96211146 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 194
3131 deg
Eccentricity:
0003873
Arg of perigee: 78
2500 deg
Mean anomaly: 281
9094 deg
Mean motion: 15
54034568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3303
Checksum: 286
Coasting Arc #4 (Orbit 3317)
---------------------------------------
Vector Time (GMT): 2018/133/22:09:51
749
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6592585
64 A = 6788410
38 meter
Y = 299556
03 meter E =
0011078
Z = -1579354
17 I = 51
59627
XDOT = -1585
913834 Wp = 51
98923
YDOT = -4829
422532 meter/sec RA = 188
33403 deg
ZDOT = 5738
080871 TA = 290
73319
MA = 290
85187
Ha = 222
471 n
mi
Hp = 213
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21629217
99 X = -6587773
55
Y = 982795
39 feet Y = 225860
16 meter
Z = -5181608
18 Z = -1611367
64
XDOT = -5203
129376 XDOT = -1559
665198
YDOT = -15844
562112 feet/sec YDOT = -4847
010728 meter/sec
ZDOT = 18825
724643 ZDOT = 5730
440492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19460501
25 X = 5931560
78
Y = -9411456
64 feet Y = -2868611
98 meter
Z = -5324602
92 Z = -1622938
97
XDOT = 10452
648920 XDOT = 3185
967391
YDOT = 11043
226791 feet/sec YDOT = 3365
975526 meter/sec
ZDOT = 18792
163599 ZDOT = 5727
851465
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 18133
92669197
00016717 00000-0 10270-3 0 9035
2 25544 51
6404 189
5051 0003873 80
3970 279
7620 15
54058564 33180
Satellite: ISS
Catalog Number: 25544
Epoch time: 18133
92669197 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 189
5051 deg
Eccentricity:
0003873
Arg of perigee: 80
3970 deg
Mean anomaly: 279
7620 deg
Mean motion: 15
54058564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3318
Checksum: 329
Coasting Arc #5 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2018/134/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2524467
83 A = 6778736
65 meter
Y = -3741567
56 meter E =
0008963
Z = 5051113
88 I = 51
57234
XDOT = 7088
693316 Wp = 70
24167
YDOT = 2291
418300 meter/sec RA = 186
61402 deg
ZDOT = -1839
845558 TA = 37
61125
MA = 37
54860
Ha = 222
551 n
mi
Hp = 213
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8282374
77 X = 2541583
26
Y = -12275484
14 feet Y = -3713241
73 meter
Z = 16571895
92 Z = 5063418
56
XDOT = 23256
867835 XDOT = 7071
480395
YDOT = 7517
776575 feet/sec YDOT = 2370
592779 meter/sec
ZDOT = -6036
238707 ZDOT = -1805
452112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13505457
58 X = 4116463
47
Y = -5920234
15 feet Y = -1804487
37 meter
Z = 16627279
40 Z = 5067994
76
XDOT = 15120
393837 XDOT = 4608
696042
YDOT = 17919
094110 feet/sec YDOT = 5461
739885 meter/sec
ZDOT = -5882
909254 ZDOT = -1793
110741
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 18134
31252541
00016717 00000-0 10270-3 0 9041
2 25544 51
6380 187
5771 0003968 89
6898 270
4709 15
54016729 33246
Satellite: ISS
Catalog Number: 25544
Epoch time: 18134
31252541 = yrday
fracday
Element set: 904
Inclination: 51
6380 deg
RA of node: 187
5771 deg
Eccentricity:
0003968
Arg of perigee: 89
6898 deg
Mean anomaly: 270
4709 deg
Mean motion: 15
54016729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 331
Coasting Arc #6 (Orbit 3338)
---------------------------------------
Vector Time (GMT): 2018/135/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4088699
71 A = 6781635
90 meter
Y = 3294992
14 meter E =
0012236
Z = -4303674
52 I = 51
61538
XDOT = -6109
137894 Wp = 105
53835
YDOT = -2972
625458 meter/sec RA = 181
61864 deg
ZDOT = 3533
248937 TA = 200
49589
MA = 200
54503
Ha = 222
492 n
mi
Hp = 213
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13414369
12 X = -4104335
88
Y = 10810341
66 feet Y = 3249182
33 meter
Z = -14119667
06 Z = -4323574
23
XDOT = -20043
103327 XDOT = -6092
606184
YDOT = -9752
708197 feet/sec YDOT = -3040
849833 meter/sec
ZDOT = 11592
024073 ZDOT = 3503
612158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17012816
35 X = -5185506
42
Y = 2200941
50 feet Y = 670846
97 meter
Z = -14208930
98 Z = -4330882
16
XDOT = -11837
390638 XDOT = -3608
036666
YDOT = -17625
657695 feet/sec YDOT = -5372
300465 meter/sec
ZDOT = 11460
000304 ZDOT = 3493
008093
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 18135
27710288
00016717 00000-0 10270-3 0 9055
2 25544 51
6382 182
7699 0003768 92
7381 267
4203 15
54045267 33394
Satellite: ISS
Catalog Number: 25544
Epoch time: 18135
27710288 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 182
7699 deg
Eccentricity:
0003768
Arg of perigee: 92
7381 deg
Mean anomaly: 267
4203 deg
Mean motion: 15
54045267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3339
Checksum: 333
Coasting Arc #7 (Orbit 3354)
---------------------------------------
Vector Time (GMT): 2018/136/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5368206
72 A = 6785453
15 meter
Y = -2758927
55 meter E =
0016809
Z = 3083960
89 I = 51
66144
XDOT = 4678
663200 Wp = 95
83554
YDOT = 3604
913544 meter/sec RA = 176
63357 deg
ZDOT = -4897
833332 TA = 48
70736
MA = 48
56275
Ha = 222
468 n
mi
Hp = 213
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17612226
77 X = 5383678
25
Y = -9051599
58 feet Y = -2698810
33 meter
Z = 10117981
93 Z = 3110075
66
XDOT = 15349
944883 XDOT = 4661
795930
YDOT = 11827
144174 feet/sec YDOT = 3657
139693 meter/sec
ZDOT = -16069
006995 ZDOT = -4875
146185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19706838
14 X = 6006644
27
Y = 1175422
08 feet Y = 358268
65 meter
Z = 10234962
54 Z = 3119616
58
XDOT = 7337
582665 XDOT = 2236
495196
YDOT = 16622
461728 feet/sec YDOT = 5066
526335 meter/sec
ZDOT = -15968
084611 ZDOT = -4867
072189
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 18136
30598436
00016717 00000-0 10270-3 0 9060
2 25544 51
6385 177
6406 0003855 96
8576 263
3020 15
54042322 33553
Satellite: ISS
Catalog Number: 25544
Epoch time: 18136
30598436 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 177
6406 deg
Eccentricity:
0003855
Arg of perigee: 96
8576 deg
Mean anomaly: 263
3020 deg
Mean motion: 15
54042322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3355
Checksum: 317
Coasting Arc #8 (Orbit 3369)
---------------------------------------
Vector Time (GMT): 2018/137/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6225860
54 A = 6788421
38 meter
Y = 2182510
67 meter E =
0010405
Z = -1591291
26 I = 51
70438
XDOT = -2916
164103 Wp = 57
08625
YDOT = -4155
562041 meter/sec RA = 171
66125 deg
ZDOT = 5742
634911 TA = 285
53029
MA = 285
64514
Ha = 222
502 n
mi
Hp = 213
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20426051
65 X = -6242073
47
Y = 7160468
08 feet Y = 2112798
33 meter
Z = -5220771
85 Z = -1621574
00
XDOT = -9567
467529 XDOT = -2897
373900
YDOT = -13633
733729 feet/sec YDOT = -4188
068147 meter/sec
ZDOT = 18840
665717 ZDOT = 5728
514148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21258794
92 X = -6479680
69
Y = -3889182
11 feet Y = -1185422
71 meter
Z = -5356327
92 Z = -1632608
75
XDOT = -1943
611876 XDOT = -592
412900
YDOT = -15093
532443 feet/sec YDOT = -4600
508689 meter/sec
ZDOT = 18778
067842 ZDOT = 5723
555078
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 18137
27055745
00016717 00000-0 10270-3 0 9079
2 25544 51
6387 172
8330 0003882 97
3524 262
8070 15
54050061 33702
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
27055745 = yrday
fracday
Element set: 907
Inclination: 51
6387 deg
RA of node: 172
8330 deg
Eccentricity:
0003882
Arg of perigee: 97
3524 deg
Mean anomaly: 262
8070 deg
Mean motion: 15
54050061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3370
Checksum: 305
Coasting Arc #9 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2018/137/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -994349
27 A = 6777587
39 meter
Y = -4086250
76 meter E =
0006392
Z = 5309588
04 I = 51
67581
XDOT = 7518
161723 Wp = 97
84181
YDOT = -1518
609347 meter/sec RA = 169
98664 deg
ZDOT = 238
140725 TA = 349
88470
MA = 349
89756
Ha = 222
574 n
mi
Hp = 213
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3262300
76 X = -974373
37
Y = -13406334
50 feet Y = -4097259
16 meter
Z = 17419908
26 Z = 5304805
82
XDOT = 24665
884918 XDOT = 7533
427681
YDOT = -4982
314130 feet/sec YDOT = -1434
450757 meter/sec
ZDOT = 781
301590 ZDOT = 274
698819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13201239
16 X = -4023737
70
Y = 4102050
91 feet Y = 1250305
12 meter
Z = 17399025
20 Z = 5303222
88
XDOT = -6017
944106 XDOT = -1834
269364
YDOT = -23389
797748 feet/sec YDOT = -7129
210354 meter/sec
ZDOT = 944
826409 ZDOT = 287
983089
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 18137
65638569
00016717 00000-0 10270-3 0 9083
2 25544 51
6353 170
9130 0003885 93
7255 266
4342 15
54054330 33767
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
65638569 = yrday
fracday
Element set: 908
Inclination: 51
6353 deg
RA of node: 170
9130 deg
Eccentricity:
0003885
Arg of perigee: 93
7255 deg
Mean anomaly: 266
4342 deg
Mean motion: 15
54054330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 324
Coasting Arc #10 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2018/138/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -764948
12 A = 6778478
12 meter
Y = 4391511
20 meter E =
0017418
Z = -5122199
54 I = 51
71130
XDOT = -7445
378847 Wp = 101
40573
YDOT = 638
652203 meter/sec RA = 164
99199 deg
ZDOT = 1660
869051 TA = 184
63298
MA = 184
64912
Ha = 222
562 n
mi
Hp = 213
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2509672
32 X = -789117
16
Y = 14407845
14 feet Y = 4382822
49 meter
Z = -16805116
62 Z = -5125973
62
XDOT = -24427
095955 XDOT = -7460
034779
YDOT = 2095
315626 feet/sec YDOT = 555
310709 meter/sec
ZDOT = 5449
045444 ZDOT = 1624
666098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14541244
20 X = 4432171
23
Y = 1360851
39 feet Y = 414787
50 meter
Z = -16822505
81 Z = -5127499
77
XDOT = 3941
028890 XDOT = 1201
225606
YDOT = 23189
414620 feet/sec YDOT = 7068
133576 meter/sec
ZDOT = 5287
182890 ZDOT = 1611
533345
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 18138
62095767
00016717 00000-0 10270-3 0 9099
2 25544 51
6357 166
1052 0003913 96
6676 263
4922 15
54040150 33915
Satellite: ISS
Catalog Number: 25544
Epoch time: 18138
62095767 = yrday
fracday
Element set: 909
Inclination: 51
6357 deg
RA of node: 166
1052 deg
Eccentricity:
0003913
Arg of perigee: 96
6676 deg
Mean anomaly: 263
4922 deg
Mean motion: 15
54040150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 318
Coasting Arc #11 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2018/139/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2423431
04 A = 6781251
82 meter
Y = -4560429
47 meter E =
0012847
Z = 4385435
20 I = 51
75303
XDOT = 6865
805438 Wp = 78
95453
YDOT = 360
560121 meter/sec RA = 160
00422 deg
ZDOT = -3408
297793 TA = 45
53829
MA = 45
43329
Ha = 222
421 n
mi
Hp = 213
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7950889
25 X = 2452944
66
Y = -14962038
95 feet Y = -4533164
47 meter
Z = 14387910
75 Z = 4397278
61
XDOT = 22525
608393 XDOT = 6877
819071
YDOT = 1182
940030 feet/sec YDOT = 437
405841 meter/sec
ZDOT = -11182
079373 ZDOT = -3374
916698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15598976
52 X = -4754568
04
Y = -6496872
73 feet Y = -1980246
81 meter
Z = 14441391
96 Z = 4401736
27
XDOT = -1301
876898 XDOT = -396
812079
YDOT = -21477
326177 feet/sec YDOT = -6546
289019 meter/sec
ZDOT = -11032
921164 ZDOT = -3362
834371
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 18139
64983078
00016717 00000-0 10270-3 0 9105
2 25544 51
6361 160
9761 0003819 99
3184 260
8401 15
54075718 34077
Satellite: ISS
Catalog Number: 25544
Epoch time: 18139
64983078 = yrday
fracday
Element set: 910
Inclination: 51
6361 deg
RA of node: 160
9761 deg
Eccentricity:
0003819
Arg of perigee: 99
3184 deg
Mean anomaly: 260
8401 deg
Mean motion: 15
54075718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 326
Coasting Arc #12 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2018/140/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1519510
47 A = 6780142
19 meter
Y = -4680148
54 meter E =
0011114
Z = 4656372
57 I = 51
77633
XDOT = 7071
794957 Wp = 76
84891
YDOT = -613
004060 meter/sec RA = 156
17143 deg
ZDOT = -2915
552630 TA = 42
11633
MA = 42
03097
Ha = 222
314 n
mi
Hp = 213
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4985270
56 X = 1549113
98
Y = -15354818
06 feet Y = -4662991
28 meter
Z = 15276812
90 Z = 4663825
27
XDOT = 23201
427024 XDOT = 7092
286396
YDOT = -2011
168177 feet/sec YDOT = -533
807511 meter/sec
ZDOT = -9565
461386 ZDOT = -2881
150507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1223103
99 X = 372802
10
Y = -16065217
07 feet Y = -4896678
16 meter
Z = 15310688
74 Z = 4666697
93
XDOT = 21006
841623 XDOT = 6402
885327
YDOT = -7396
186385 feet/sec YDOT = -2254
357610 meter/sec
ZDOT = -9411
604235 ZDOT = -2868
656971
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 18140
42148285
00016717 00000-0 10270-3 0 9117
2 25544 51
6391 157
1289 0003639 104
9727 255
1829 15
54105278 34198
Satellite: ISS
Catalog Number: 25544
Epoch time: 18140
42148285 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 157
1289 deg
Eccentricity:
0003639
Arg of perigee: 104
9727 deg
Mean anomaly: 255
1829 deg
Mean motion: 15
54105278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3419
Checksum: 319
Coasting Arc #13 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2018/141/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2987984
24 A = 6783775
77 meter
Y = 4899105
39 meter E =
0009425
Z = -3628017
91 I = 51
81729
XDOT = -6234
169868 Wp = 103
48477
YDOT = -536
529184 meter/sec RA = 151
19483 deg
ZDOT = 4417
367906 TA = 213
68356
MA = 213
74349
Ha = 222
437 n
mi
Hp = 213
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9803097
88 X = -3024922
29
Y = 16073180
41 feet Y = 4865485
45 meter
Z = -11902945
89 Z = -3642621
83
XDOT = -20453
313216 XDOT = -6249
164179
YDOT = -1760
266352 feet/sec YDOT = -606
328159 meter/sec
ZDOT = 14492
676857 ZDOT = 4387
047977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5459871
73 X = -1664168
90
Y = 17974008
49 feet Y = 5478477
79 meter
Z = -11968826
04 Z = -3648098
18
XDOT = -19037
156365 XDOT = -5802
525260
YDOT = 3761
289049 feet/sec YDOT = 1146
440902 meter/sec
ZDOT = 14357
186585 ZDOT = 4376
070471
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 18141
38605055
00016717 00000-0 10270-3 0 9127
2 25544 51
6383 152
3216 0003953 108
5387 251
6196 15
54099925 34343
Satellite: ISS
Catalog Number: 25544
Epoch time: 18141
38605055 = yrday
fracday
Element set: 912
Inclination: 51
6383 deg
RA of node: 152
3216 deg
Eccentricity:
0003953
Arg of perigee: 108
5387 deg
Mean anomaly: 251
6196 deg
Mean motion: 15
54099925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 314
Coasting Arc #14 (Orbit 3449)
---------------------------------------
Vector Time (GMT): 2018/142/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4181524
51 A = 6787300
99 meter
Y = -4865430
25 meter E =
0017613
Z = 2190423
72 I = 51
85815
XDOT = 5027
934580 Wp = 109
31610
YDOT = 1832
125991 meter/sec RA = 146
22933 deg
ZDOT = -5498
505796 TA = 46
42649
MA = 46
28039
Ha = 222
328 n
mi
Hp = 213
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13718912
43 X = 4224980
36
Y = -15962697
68 feet Y = -4818426
72 meter
Z = 7186429
52 Z = 2210841
40
XDOT = 16495
848359 XDOT = 5033
782448
YDOT = 6010
912045 feet/sec YDOT = 1888
384850 meter/sec
ZDOT = -18039
717180 ZDOT = -5474
067473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8986572
73 X = 2739107
37
Y = -18998124
63 feet Y = -5790628
39 meter
Z = 7278311
33 Z = 2218429
29
XDOT = 16225
443435 XDOT = 4945
515159
YDOT = 768
106769 feet/sec YDOT = 234
118943 meter/sec
ZDOT = -17930
665791 ZDOT = -5465
266933
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 18142
41491768
00016717 00000-0 10270-3 0 9137
2 25544 51
6390 147
1926 0003740 109
8984 250
2571 15
54109696 34509
Satellite: ISS
Catalog Number: 25544
Epoch time: 18142
41491768 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 147
1926 deg
Eccentricity:
0003740
Arg of perigee: 109
8984 deg
Mean anomaly: 250
2571 deg
Mean motion: 15
54109696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3450
Checksum: 320
Coasting Arc #15 (Orbit 3464)
---------------------------------------
Vector Time (GMT): 2018/143/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4982874
12 A = 6789387
36 meter
Y = 4570416
19 meter E =
0012596
Z = -571545
66 I = 51
89148
XDOT = -3576
834383 Wp = 57
65309
YDOT = -3162
366264 meter/sec RA = 141
27367 deg
ZDOT = 5998
379329 TA = 296
20180
MA = 296
33126
Ha = 222
440 n
mi
Hp = 213
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16348012
20 X = -5030835
15
Y = 14994803
77 feet Y = 4514426
12 meter
Z = -1875149
80 Z = -595867
12
XDOT = -11735
020943 XDOT = -3570
343195
YDOT = -10375
217403 feet/sec YDOT = -3202
328879 meter/sec
ZDOT = 19679
722209 ZDOT = 5981
019846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11486921
42 X = -3501213
65
Y = 18966558
99 feet Y = 5781007
18 meter
Z = -1984466
20 Z = -604865
30
XDOT = -12910
675480 XDOT = -3935
173886
YDOT = -5801
577953 feet/sec YDOT = -1768
320960 meter/sec
ZDOT = 19602
477933 ZDOT = 5974
835274
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 18143
37947968
00016717 00000-0 10270-3 0 9142
2 25544 51
6391 142
3849 0003797 110
7964 249
3595 15
54053697 34652
Satellite: ISS
Catalog Number: 25544
Epoch time: 18143
37947968 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 142
3849 deg
Eccentricity:
0003797
Arg of perigee: 110
7964 deg
Mean anomaly: 249
3595 deg
Mean motion: 15
54053697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3465
Checksum: 358
Coasting Arc #16 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2018/144/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907493
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5415952
34 A = 6788890
61 meter
Y = -3918586
61 meter E =
0013020
Z = -1156402
94 I = 51
91538
XDOT = 1994
611441 Wp = 134
63069
YDOT = 4481
388732 meter/sec RA = 136
32199 deg
ZDOT = -5893
542335 TA = 57
87647
MA = 57
75018
Ha = 222
439 n
mi
Hp = 213
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17768872
51 X = 5464985
76
Y = -12856255
28 feet Y = -3857747
49 meter
Z = -3793972
90 Z = -1129974
98
XDOT = 6544
000790 XDOT = 1972
979035
YDOT = 14702
718937 feet/sec YDOT = 4503
573151 meter/sec
ZDOT = -19335
768814 ZDOT = -5883
905473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13185326
39 X = 4018887
48
Y = -17551344
59 feet Y = -5349649
83 meter
Z = -3675300
20 Z = -1120231
50
XDOT = 9448
178686 XDOT = 2879
804864
YDOT = 11102
779392 feet/sec YDOT = 3384
127159 meter/sec
ZDOT = -19293
220687 ZDOT = -5880
573665
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 18144
40834297
00016717 00000-0 10270-3 0 9158
2 25544 51
6393 137
2562 0003894 115
9184 244
2370 15
54095439 34811
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
40834297 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 137
2562 deg
Eccentricity:
0003894
Arg of perigee: 115
9184 deg
Mean anomaly: 244
2370 deg
Mean motion: 15
54095439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3481
Checksum: 323
Coasting Arc #17 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2018/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922207
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3059339
73 A = 6786999
82 meter
Y = -5570356
57 meter E =
0017492
Z = 2358363
83 I = 51
90900
XDOT = 5397
419030 Wp = 108
27988
YDOT = 660
785313 meter/sec RA = 135
68701 deg
ZDOT = -5413
470239 TA = 45
48518
MA = 45
34238
Ha = 222
320 n
mi
Hp = 213
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10037203
85 X = 3109945
82
Y = -18275448
06 feet Y = -5535862
07 meter
Z = 7737414
12 Z = 2373347
84
XDOT = 17708
067683 XDOT = 5415
924809
YDOT = 2167
930817 feet/sec YDOT = 721
246677 meter/sec
ZDOT = -17760
729130 ZDOT = -5387
206245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11192402
44 X = -3411444
26
Y = -17561759
65 feet Y = -5352824
34 meter
Z = 7805111
51 Z = 2378997
99
XDOT = 9214
611055 XDOT = 2808
613450
YDOT = -13753
713821 feet/sec YDOT = -4192
131973 meter/sec
ZDOT = -17643
350705 ZDOT = -5377
693295
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 18144
53694984
00016717 00000-0 10270-3 0 9160
2 25544 51
6361 136
6154 0003728 113
7534 246
3999 15
54105418 34838
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
53694984 = yrday
fracday
Element set: 916
Inclination: 51
6361 deg
RA of node: 136
6154 deg
Eccentricity:
0003728
Arg of perigee: 113
7534 deg
Mean anomaly: 246
3999 deg
Mean motion: 15
54105418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3483
Checksum: 332
Coasting Arc #18 (Orbit 3497)
---------------------------------------
Vector Time (GMT): 2018/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922207
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3937462
12 A = 6789099
79 meter
Y = 5475459
15 meter E =
0011691
Z = -752824
58 I = 51
93892
XDOT = -4245
328672 Wp = 59
67175
YDOT = -2241
443550 meter/sec RA = 130
73455 deg
ZDOT = 5976
375582 TA = 292
22844
MA = 292
35242
Ha = 222
355 n
mi
Hp = 213
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12918182
81 X = -3994740
69
Y = 17964104
82 feet Y = 5431107
51 meter
Z = -2469896
90 Z = -772090
48
XDOT = -13928
243673 XDOT = -4248
979147
YDOT = -7353
817420 feet/sec YDOT = -2288
938448 meter/sec
ZDOT = 19607
531438 ZDOT = 5955
744018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9855747
59 X = 3004031
87
Y = 19799398
31 feet Y = 6034856
60 meter
Z = -2556749
14 Z = -779297
14
XDOT = -11624
215460 XDOT = -3543
060872
YDOT = 8275
803338 feet/sec YDOT = 2522
464857 meter/sec
ZDOT = 19515
533338 ZDOT = 5948
334562
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 18145
50150824
00016717 00000-0 10270-3 0 9179
2 25544 51
6360 131
8080 0003981 119
9947 240
1601 15
54117083 34988
Satellite: ISS
Catalog Number: 25544
Epoch time: 18145
50150824 = yrday
fracday
Element set: 917
Inclination: 51
6360 deg
RA of node: 131
8080 deg
Eccentricity:
0003981
Arg of perigee: 119
9947 deg
Mean anomaly: 240
1601 deg
Mean motion: 15
54117083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3498
Checksum: 301
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