[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 8th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
255/21:17:02
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 216
0
256/02:57:42
000 0
0 0
0 0
0
N/A 0
0 0
0 219
3
000/00:00:00
000 0
0 0
0 216
1
256/23:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
4
000/00:00:00
000 0
0 0
0 216
0
260/08:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
4
000/00:00:00
000 0
0 0
0 216
0
261/05:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 215
8
Coasting Arc #1 (Orbit 3470)
---------------------------------------
Vector Time (GMT): 2017/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6552958
21 A = 6789248
52 meter
Y = -1697515
89 meter E =
0008989
Z = 452999
68 I = 51
55307
XDOT = 806
617173 Wp = 42
25668
YDOT = 4727
168006 meter/sec RA = 342
43148 deg
ZDOT = 5983
126566 TA = 322
63404
MA = 322
69652
Ha = 219
816 n
mi
Hp = 216
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21499206
74 X = 6569252
81
Y = -5569277
86 feet Y = -1624145
08 meter
Z = 1486219
43 Z = 484871
70
XDOT = 2646
381801 XDOT = 724
633670
YDOT = 15509
081384 feet/sec YDOT = 4735
730467 meter/sec
ZDOT = 19629
680336 ZDOT = 5986
845172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22192261
39 X = -6764201
27
Y = 544132
04 feet Y = 165851
45 meter
Z = 1627589
94 Z = 496089
41
XDOT = 1109
841143 XDOT = 338
279580
YDOT = -14058
931708 feet/sec YDOT = -4285
162385 meter/sec
ZDOT = 19645
328016 ZDOT = 5987
895979
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 17251
56334920
00016717 00000-0 10270-3 0 9005
2 25544 51
6432 342
6933 0004212 247
0661 113
0048 15
54120621 34717
Satellite: ISS
Catalog Number: 25544
Epoch time: 17251
56334920 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 342
6933 deg
Eccentricity:
0004212
Arg of perigee: 247
0661 deg
Mean anomaly: 113
0048 deg
Mean motion: 15
54120621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3471
Checksum: 266
Coasting Arc #2 (Orbit 3485)
---------------------------------------
Vector Time (GMT): 2017/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6388983
83 A = 6787305
88 meter
Y = 822010
62 meter E =
0006124
Z = -2126472
13 I = 51
51462
XDOT = 1157
517711 Wp = 177
87375
YDOT = -5215
286619 meter/sec RA = 337
45330 deg
ZDOT = -5500
286552 TA = 25
73378
MA = 25
70332
Ha = 219
630 n
mi
Hp = 216
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20961233
04 X = -6387371
52
Y = 2696885
22 feet Y = 750573
42 meter
Z = -6976614
60 Z = -2157504
14
XDOT = 3797
630287 XDOT = 1242
468216
YDOT = -17110
520403 feet/sec YDOT = -5201
868099 meter/sec
ZDOT = -18045
559554 ZDOT = -5494
456746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21014377
60 X = 6405182
29
Y = 1762125
87 feet Y = 537095
97 meter
Z = -7114104
19 Z = -2168378
96
XDOT = -7298
206683 XDOT = -2224
493397
YDOT = 14373
542512 feet/sec YDOT = 4381
055758 meter/sec
ZDOT = -18018
863319 ZDOT = -5492
149540
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 17252
52787550
00016717 00000-0 10270-3 0 9014
2 25544 51
6418 337
8861 0004281 249
4806 110
5887 15
54138016 34866
Satellite: ISS
Catalog Number: 25544
Epoch time: 17252
52787550 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 337
8861 deg
Eccentricity:
0004281
Arg of perigee: 249
4806 deg
Mean anomaly: 110
5887 deg
Mean motion: 15
54138016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3486
Checksum: 324
Coasting Arc #3 (Orbit 3501)
---------------------------------------
Vector Time (GMT): 2017/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5766376
01 A = 6783680
60 meter
Y = 192658
83 meter E =
0008059
Z = 3562837
90 I = 51
47366
XDOT = -2935
283520 Wp = 102
92545
YDOT = 5518
860925 meter/sec RA = 332
46376 deg
ZDOT = 4442
006040 TA = 299
26592
MA = 299
34646
Ha = 219
445 n
mi
Hp = 216
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18918556
47 X = 5746486
44
Y = 632082
76 feet Y = 257031
51 meter
Z = 11689100
71 Z = 3590801
03
XDOT = -9630
195274 XDOT = -3018
355974
YDOT = 18106
499099 feet/sec YDOT = 5485
572535 meter/sec
ZDOT = 14573
510631 ZDOT = 4427
544929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18363191
59 X = -5597100
80
Y = -4265764
82 feet Y = -1300205
12 meter
Z = 11812824
73 Z = 3600548
98
XDOT = 12733
489540 XDOT = 3881
167612
YDOT = -14545
338249 feet/sec YDOT = -4433
419098 meter/sec
ZDOT = 14508
567267 ZDOT = 4422
211303
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 17253
55668940
00016717 00000-0 10270-3 0 9020
2 25544 51
6423 332
7569 0004288 254
7042 105
3637 15
54180758 35023
Satellite: ISS
Catalog Number: 25544
Epoch time: 17253
55668940 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 332
7569 deg
Eccentricity:
0004288
Arg of perigee: 254
7042 deg
Mean anomaly: 105
3637 deg
Mean motion: 15
54180758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3502
Checksum: 317
Coasting Arc #4 (Orbit 3516)
---------------------------------------
Vector Time (GMT): 2017/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4760780
00 A = 6779978
46 meter
Y = -1351895
33 meter E =
0006467
Z = -4640566
21 I = 51
43181
XDOT = 4406
508553 Wp = 63
97179
YDOT = -5556
454074 meter/sec RA = 327
46241 deg
ZDOT = -2902
318706 TA = 177
05447
MA = 177
05066
Ha = 219
442 n
mi
Hp = 215
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15619356
95 X = -4722767
14
Y = -4435352
12 feet Y = -1404921
44 meter
Z = -15224954
75 Z = -4663600
34
XDOT = 14457
049057 XDOT = 4482
412949
YDOT = -18229
836202 feet/sec YDOT = -5506
753315 meter/sec
ZDOT = -9522
042999 ZDOT = -2880
728286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14492263
95 X = 4417242
05
Y = 7106590
97 feet Y = 2166088
93 meter
Z = -15326661
65 Z = -4671566
47
XDOT = -16991
219243 XDOT = -5178
923625
YDOT = 14324
398301 feet/sec YDOT = 4366
076602 meter/sec
ZDOT = -9425
549057 ZDOT = -2872
907352
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 17254
52119356
00016717 00000-0 10270-3 0 9031
2 25544 51
6415 327
9491 0004223 259
8543 100
2133 15
54165051 35175
Satellite: ISS
Catalog Number: 25544
Epoch time: 17254
52119356 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 327
9491 deg
Eccentricity:
0004223
Arg of perigee: 259
8543 deg
Mean anomaly: 100
2133 deg
Mean motion: 15
54165051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3517
Checksum: 290
Coasting Arc #5 (Orbit 3532)
---------------------------------------
Vector Time (GMT): 2017/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3488726
51 A = 6777446
87 meter
Y = 2568221
99 meter E =
0002634
Z = 5213496
45 I = 51
39677
XDOT = -5467
432503 Wp = 204
39965
YDOT = 5270
524042 meter/sec RA = 322
44990 deg
ZDOT = 1060
177652 TA = 235
39728
MA = 235
42213
Ha = 219
221 n
mi
Hp = 216
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11445953
12 X = 3434423
91
Y = 8425925
16 feet Y = 2606932
00 meter
Z = 17104647
13 Z = 5230311
65
XDOT = -17937
770679 XDOT = -5531
112407
YDOT = 17291
745543 feet/sec YDOT = 5209
027494 meter/sec
ZDOT = 3478
273136 ZDOT = 1033
463406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9843534
18 X = -3000309
22
Y = -10127917
19 feet Y = -3086989
16 meter
Z = 17178624
49 Z = 5236044
74
XDOT = 19750
887041 XDOT = 6020
070370
YDOT = -13486
630929 feet/sec YDOT = -4110
725107 meter/sec
ZDOT = 3359
160491 ZDOT = 1023
872118
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 17255
54998663
00016717 00000-0 10270-3 0 9041
2 25544 51
6415 322
8204 0004213 264
3768 95
6904 15
54214132 35336
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
54998663 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 322
8204 deg
Eccentricity:
0004213
Arg of perigee: 264
3768 deg
Mean anomaly: 95
6904 deg
Mean motion: 15
54214132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3533
Checksum: 311
Coasting Arc #6 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2017/255/21:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 909096
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3083668
14 A = 6777104
87 meter
Y = 2924204
69 meter E =
0001830
Z = 5280606
37 I = 51
38490
XDOT = -5666
911475 Wp = 244
02625
YDOT = 5144
971183 meter/sec RA = 320
51217 deg
ZDOT = 459
497901 TA = 201
57133
MA = 201
57904
Ha = 219
192 n
mi
Hp = 216
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10117021
46 X = 3025088
99
Y = 9593847
42 feet Y = 2958361
13 meter
Z = 17324824
06 Z = 5295443
51
XDOT = -18592
229250 XDOT = -5726
254760
YDOT = 16879
826717 feet/sec YDOT = 5081
268134 meter/sec
ZDOT = 1507
539046 ZDOT = 431
825243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -810049
50 X = -246903
09
Y = 13837546
68 feet Y = 4217684
23 meter
Z = 17389987
97 Z = 5300468
33
XDOT = -23905
028694 XDOT = -7286
252746
YDOT = -3141
690760 feet/sec YDOT = -957
587344 meter/sec
ZDOT = 1384
209377 ZDOT = 421
907018
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 17255
93578282
00016717 00000-0 10270-3 0 9056
2 25544 51
6406 320
8990 0004175 270
9201 89
1473 15
54232416 35398
Satellite: ISS
Catalog Number: 25544
Epoch time: 17255
93578282 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 320
8990 deg
Eccentricity:
0004175
Arg of perigee: 270
9201 deg
Mean anomaly: 89
1473 deg
Mean motion: 15
54232416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 318
Coasting Arc #7 (Orbit 3541)
---------------------------------------
Vector Time (GMT): 2017/256/02:57:42
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3085330
25 A = 6786196
10 meter
Y = -5434200
95 meter E =
0003083
Z = -2641406
58 I = 51
40770
XDOT = 5598
521022 Wp = 355
62218
YDOT = 654
283011 meter/sec RA = 319
30108 deg
ZDOT = 5195
974454 TA = 334
50145
MA = 334
51666
Ha = 219
338 n
mi
Hp = 216
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10122474
58 X = 3158698
33
Y = -17828743
28 feet Y = -5399288
60 meter
Z = -8666032
08 Z = -2626240
45
XDOT = 18367
851122 XDOT = 5565
548958
YDOT = 2146
597804 feet/sec YDOT = 716
705404 meter/sec
ZDOT = 17047
160283 ZDOT = 5223
090329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2193968
21 X = -668721
51
Y = -20412975
97 feet Y = -6221875
08 meter
Z = -8598000
12 Z = -2620670
44
XDOT = 14565
564634 XDOT = 4439
584100
YDOT = -8792
660339 feet/sec YDOT = -2680
002871 meter/sec
ZDOT = 17167
044584 ZDOT = 5232
515189
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 17256
12867915
00016717 00000-0 10270-3 0 9063
2 25544 51
6394 319
9354 0004249 270
6864 89
3802 15
54203646 35426
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
12867915 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 319
9354 deg
Eccentricity:
0004249
Arg of perigee: 270
6864 deg
Mean anomaly: 89
3802 deg
Mean motion: 15
54203646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3542
Checksum: 333
Coasting Arc #8 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2017/256/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2207279
32 A = 6785109
99 meter
Y = -5640885
14 meter E =
0001828
Z = -3055047
76 I = 51
38749
XDOT = 5888
722001 Wp = 5
64532
YDOT = -345
992214 meter/sec RA = 315
12373 deg
ZDOT = 4895
495186 TA = 319
16322
MA = 319
17692
Ha = 219
360 n
mi
Hp = 216
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7241730
05 X = 2285033
08
Y = -18506841
02 feet Y = -5615767
24 meter
Z = -10023122
59 Z = -3044136
35
XDOT = 19319
954073 XDOT = 5868
373378
YDOT = -1135
145060 feet/sec YDOT = -280
254053 meter/sec
ZDOT = 16061
335911 ZDOT = 4924
051390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13894645
37 X = 4235087
91
Y = -14243213
90 feet Y = -4341331
60 meter
Z = -9973890
57 Z = -3040041
85
XDOT = 17119
769917 XDOT = 5218
105871
YDOT = 5369
930505 feet/sec YDOT = 1636
754818 meter/sec
ZDOT = 16187
761393 ZDOT = 4934
029673
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 17256
96456337
00016717 00000-0 10270-3 0 9078
2 25544 51
6428 315
7699 0004111 275
3834 84
6849 15
54231196 35551
Satellite: ISS
Catalog Number: 25544
Epoch time: 17256
96456337 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 315
7699 deg
Eccentricity:
0004111
Arg of perigee: 275
3834 deg
Mean anomaly: 84
6849 deg
Mean motion: 15
54231196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 343
Coasting Arc #9 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2017/257/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3298917
38 A = 6788220
69 meter
Y = 5740261
77 meter E =
0010239
Z = 1473691
88 I = 51
37484
XDOT = -4892
815274 Wp = 126
19730
YDOT = -1329
000618 meter/sec RA = 310
13049 deg
ZDOT = -5754
032871 TA = 37
65532
MA = 37
58369
Ha = 219
477 n
mi
Hp = 216
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10823219
75 X = -3370019
78
Y = 18832879
82 feet Y = 5702973
55 meter
Z = 4834947
11 Z = 1457493
81
XDOT = -16052
543550 XDOT = -4849
640208
YDOT = -4360
238247 feet/sec YDOT = -1383
474312 meter/sec
ZDOT = -18878
060601 ZDOT = -5777
695640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17062934
95 X = -5200782
57
Y = 13467471
09 feet Y = 4104885
19 meter
Z = 4762314
04 Z = 1451553
32
XDOT = -12194
482054 XDOT = -3716
878130
YDOT = -8711
571722 feet/sec YDOT = -2655
287061 meter/sec
ZDOT = -18982
552194 ZDOT = -5785
881909
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 17257
99333423
00016717 00000-0 10270-3 0 9083
2 25544 51
6424 310
6415 0003962 278
6635 81
4068 15
54202946 35712
Satellite: ISS
Catalog Number: 25544
Epoch time: 17257
99333423 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 310
6415 deg
Eccentricity:
0003962
Arg of perigee: 278
6635 deg
Mean anomaly: 81
4068 deg
Mean motion: 15
54202946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 319
Coasting Arc #10 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2017/258/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4064618
89 A = 6788947
79 meter
Y = -5423596
54 meter E =
0010853
Z = 252763
30 I = 51
35708
XDOT = 3699
305234 Wp = 29
38101
YDOT = 3055
906307 meter/sec RA = 305
14044 deg
ZDOT = 5983
627136 TA = 333
35388
MA = 333
40962
Ha = 219
411 n
mi
Hp = 215
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13335363
82 X = 4123737
11
Y = -17793951
90 feet Y = -5377812
63 meter
Z = 829275
92 Z = 272651
79
XDOT = 12136
828196 XDOT = 3635
792988
YDOT = 10025
939326 feet/sec YDOT = 3096
919749 meter/sec
ZDOT = 19631
322625 ZDOT = 6001
442634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18774149
83 X = 5722360
87
Y = -11909349
40 feet Y = -3629969
70 meter
Z = 918175
22 Z = 279859
81
XDOT = 6802
193874 XDOT = 2073
308693
YDOT = 12265
540396 feet/sec YDOT = 3738
536713 meter/sec
ZDOT = 19709
658224 ZDOT = 6007
503827
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 17259
02209467
00016717 00000-0 10270-3 0 9090
2 25544 51
6420 305
5123 0004157 284
4520 75
6171 15
54249183 35873
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
02209467 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 305
5123 deg
Eccentricity:
0004157
Arg of perigee: 284
4520 deg
Mean anomaly: 75
6171 deg
Mean motion: 15
54249183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 307
Coasting Arc #11 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2017/259/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924327
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4527747
97 A = 6787339
52 meter
Y = 4652061
59 meter E =
0003989
Z = -1972995
22 I = 51
33380
XDOT = -2410
696993 Wp = 176
06836
YDOT = -4700
481086 meter/sec RA = 300
14888 deg
ZDOT = -5555
475055 TA = 25
79712
MA = 25
77723
Ha = 219
460 n
mi
Hp = 215
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14854816
18 X = -4569848
28
Y = 15262669
25 feet Y = 4601193
65 meter
Z = -6473081
42 Z = -1995092
11
XDOT = -7909
110868 XDOT = -2330
970219
YDOT = -15421
525874 feet/sec YDOT = -4726
993854 meter/sec
ZDOT = -18226
624197 ZDOT = -5566
991330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19104286
89 X = -5822986
64
Y = 9346417
81 feet Y = 2848788
15 meter
Z = -6571614
42 Z = -2003028
08
XDOT = -1426
564877 XDOT = -434
816975
YDOT = -15756
260775 feet/sec YDOT = -4802
508284 meter/sec
ZDOT = -18276
825996 ZDOT = -5570
776563
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 17259
98655169
00016717 00000-0 10270-3 0 9101
2 25544 51
6422 300
7045 0004244 286
0581 74
0104 15
54226957 36028
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
98655169 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 300
7045 deg
Eccentricity:
0004244
Arg of perigee: 286
0581 deg
Mean anomaly: 74
0104 deg
Mean motion: 15
54226957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 303
Coasting Arc #12 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2017/260/08:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 399416
40 A = 6784913
36 meter
Y = -6021852
84 meter E =
0002252
Z = -3098022
61 I = 51
31864
XDOT = 5538
561107 Wp = 7
61183
YDOT = -2128
498768 meter/sec RA = 298
06148 deg
ZDOT = 4853
981733 TA = 316
58441
MA = 316
60214
Ha = 219
408 n
mi
Hp = 215
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1310421
24 X = 481773
24
Y = -19756735
05 feet Y = -6016926
11 meter
Z = -10164116
18 Z = -3095881
77
XDOT = 18171
132241 XDOT = 5538
372816
YDOT = -6983
263675 feet/sec YDOT = -2066
563384 meter/sec
ZDOT = 15925
136918 ZDOT = 4880
885896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16538994
55 X = -5041085
54
Y = 10895850
26 feet Y = 3321055
16 meter
Z = -10153676
56 Z = -3094840
62
XDOT = -15718
648989 XDOT = -4791
044212
YDOT = -8915
896651 feet/sec YDOT = -2717
565299 meter/sec
ZDOT = 16044
532054 ZDOT = 4890
373370
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 17260
37233109
00016717 00000-0 10270-3 0 9113
2 25544 51
6417 298
7775 0004164 284
0475 76
0215 15
54249682 36080
Satellite: ISS
Catalog Number: 25544
Epoch time: 17260
37233109 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 298
7775 deg
Eccentricity:
0004164
Arg of perigee: 284
0475 deg
Mean anomaly: 76
0215 deg
Mean motion: 15
54249682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 317
Coasting Arc #13 (Orbit 3621)
---------------------------------------
Vector Time (GMT): 2017/261/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2787611
88 A = 6788899
33 meter
Y = -6182688
96 meter E =
0010923
Z = 59877
51 I = 51
31805
XDOT = 4346
858589 Wp = 28
32803
YDOT = 2022
130927 meter/sec RA = 293
86435 deg
ZDOT = 5986
912771 TA = 332
31997
MA = 332
37807
Ha = 219
515 n
mi
Hp = 215
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9145708
28 X = 2856250
32
Y = -20284412
59 feet Y = -6151132
19 meter
Z = 196448
52 Z = 73586
19
XDOT = 14261
347076 XDOT = 4294
842202
YDOT = 6634
287818 feet/sec YDOT = 2070
450302 meter/sec
ZDOT = 19642
102267 ZDOT = 6007
901764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16319875
09 X = -4974297
93
Y = -15123988
68 feet Y = -4609791
75 meter
Z = 258088
28 Z = 78665
31
XDOT = 9685
400380 XDOT = 2952
110036
YDOT = -10095
709149 feet/sec YDOT = -3077
172148 meter/sec
ZDOT = 19734
659003 ZDOT = 6015
124064
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 17261
27248086
00016717 00000-0 10270-3 0 9124
2 25544 51
6399 294
2867 0003812 287
3693 72
7042 15
54276334 36220
Satellite: ISS
Catalog Number: 25544
Epoch time: 17261
27248086 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 294
2867 deg
Eccentricity:
0003812
Arg of perigee: 287
3693 deg
Mean anomaly: 72
7042 deg
Mean motion: 15
54276334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3622
Checksum: 328
Coasting Arc #14 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2017/262/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3429661
70 A = 6787428
59 meter
Y = 5569942
97 meter E =
0004404
Z = -1802256
85 I = 51
29987
XDOT = -3421
832648 Wp = 167
37054
YDOT = -3925
212009 meter/sec RA = 288
87005 deg
ZDOT = -5626
163864 TA = 32
52831
MA = 32
50118
Ha = 219
555 n
mi
Hp = 215
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11252170
92 X = -3482936
93
Y = 18274091
12 feet Y = 5531292
04 meter
Z = -5912916
18 Z = -1819047
15
XDOT = -11226
485066 XDOT = -3350
356501
YDOT = -12877
992157 feet/sec YDOT = -3963
078358 meter/sec
ZDOT = -18458
542860 ZDOT = -5642
611901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14036067
89 X = 4278193
49
Y = 16206419
72 feet Y = 4939716
73 meter
Z = -5988079
19 Z = -1825166
54
XDOT = -14449
262064 XDOT = -4404
135077
YDOT = 5675
528196 feet/sec YDOT = 1729
900994 meter/sec
ZDOT = -18530
712614 ZDOT = -5648
161205
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 17262
23691896
00016717 00000-0 10270-3 0 9133
2 25544 51
6387 289
4781 0003856 291
1616 68
9124 15
54295498 36370
Satellite: ISS
Catalog Number: 25544
Epoch time: 17262
23691896 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 289
4781 deg
Eccentricity:
0003856
Arg of perigee: 291
1616 deg
Mean anomaly: 68
9124 deg
Mean motion: 15
54295498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 357
Coasting Arc #15 (Orbit 3652)
---------------------------------------
Vector Time (GMT): 2017/263/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3854077
42 A = 6783962
21 meter
Y = -4474099
26 meter E =
0009082
Z = 3329630
77 I = 51
28022
XDOT = 2459
556833 Wp = 78
82501
YDOT = 5584
440582 meter/sec RA = 283
86723 deg
ZDOT = 4647
903127 TA = 320
18889
MA = 320
25549
Ha = 219
430 n
mi
Hp = 215
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12644610
97 X = 3887647
82
Y = -14678803
35 feet Y = -4430812
17 meter
Z = 10923985
47 Z = 3348434
86
XDOT = 8069
412182 XDOT = 2374
350075
YDOT = 18321
655454 feet/sec YDOT = 5611
469254 meter/sec
ZDOT = 15249
026007 ZDOT = 4659
643167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10478590
61 X = -3193874
42
Y = -16239233
92 feet Y = -4949718
50 meter
Z = 11007875
98 Z = 3355200
60
XDOT = 18651
154510 XDOT = 5684
871895
YDOT = -1643
597612 feet/sec YDOT = -500
968552 meter/sec
ZDOT = 15300
116538 ZDOT = 4663
475521
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 17263
26564299
00016717 00000-0 10270-3 0 9144
2 25544 51
6399 284
3483 0003928 293
1872 66
8867 15
54331909 36539
Satellite: ISS
Catalog Number: 25544
Epoch time: 17263
26564299 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 284
3483 deg
Eccentricity:
0003928
Arg of perigee: 293
1872 deg
Mean anomaly: 66
8867 deg
Mean motion: 15
54331909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3653
Checksum: 357
Coasting Arc #16 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2017/264/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4118701
76 A = 6780123
30 meter
Y = 2965361
11 meter E =
0007790
Z = -4503701
06 I = 51
26055
XDOT = -1484
135363 Wp = 47
29664
YDOT = -6830
037814 meter/sec RA = 278
85341 deg
ZDOT = -3138
101664 TA = 191
01884
MA = 191
03591
Ha = 219
721 n
mi
Hp = 215
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13512801
04 X = -4129678
22
Y = 9728875
04 feet Y = 2919240
97 meter
Z = -14775922
11 Z = -4523735
62
XDOT = -4869
210507 XDOT = -1392
406318
YDOT = -22408
260544 feet/sec YDOT = -6846
121985 meter/sec
ZDOT = -10295
609135 ZDOT = -3145
087404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5761804
79 X = 1756198
10
Y = 15537294
89 feet Y = 4735767
48 meter
Z = -14865017
61 Z = -4530857
37
XDOT = -21741
875740 XDOT = -6626
923725
YDOT = -1821
388655 feet/sec YDOT = -555
159262 meter/sec
ZDOT = -10325
485334 ZDOT = -3147
207930
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 17264
23006563
00016717 00000-0 10270-3 0 9158
2 25544 51
6401 279
5397 0003894 299
0341 61
0421 15
54304763 36688
Satellite: ISS
Catalog Number: 25544
Epoch time: 17264
23006563 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 279
5397 deg
Eccentricity:
0003894
Arg of perigee: 299
0341 deg
Mean anomaly: 61
0421 deg
Mean motion: 15
54304763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 310
Coasting Arc #17 (Orbit 3683)
---------------------------------------
Vector Time (GMT): 2017/265/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4231353
51 A = 6777230
07 meter
Y = -1173148
97 meter E =
0000333
Z = 5162277
05 I = 51
24720
XDOT = 526
668472 Wp = 146
32903
YDOT = 7542
866817 meter/sec RA = 273
82849 deg
ZDOT = 1282
141865 TA = 291
29031
MA = 291
29387
Ha = 219
575 n
mi
Hp = 215
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13882393
40 X = 4219081
45
Y = -3848913
95 feet Y = -1125899
00 meter
Z = 16936604
50 Z = 5182802
19
XDOT = 1727
914935 XDOT = 436
054912
YDOT = 24746
938377 feet/sec YDOT = 7548
249906 meter/sec
ZDOT = 4206
502182 ZDOT = 1284
479167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -248631
51 X = -75782
89
Y = -14296247
93 feet Y = -4357496
37 meter
Z = 17027596
27 Z = 5190011
34
XDOT = 23333
174751 XDOT = 7111
951664
YDOT = 4616
563045 feet/sec YDOT = 1407
128416 meter/sec
ZDOT = 4215
716282 ZDOT = 1284
950323
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 17265
25877199
00016717 00000-0 10270-3 0 9163
2 25544 51
6400 274
4097 0003906 302
9332 57
1445 15
54356551 36848
Satellite: ISS
Catalog Number: 25544
Epoch time: 17265
25877199 = yrday
fracday
Element set: 916
Inclination: 51
6400 deg
RA of node: 274
4097 deg
Eccentricity:
0003906
Arg of perigee: 302
9332 deg
Mean anomaly: 57
1445 deg
Mean motion: 15
54356551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3684
Checksum: 325
Coasting Arc #18 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2017/266/05:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905019
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4232202
88 A = 6776859
84 meter
Y = -730103
75 meter E =
0011533
Z = -5252148
18 I = 51
24542
XDOT = 420
308185 Wp = 85
34269
YDOT = -7614
917935 meter/sec RA = 268
80000 deg
ZDOT = 722
162318 TA = 191
58714
MA = 191
61371
Ha = 219
832 n
mi
Hp = 215
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13885180
04 X = -4198211
45
Y = -2395353
50 feet Y = -777241
72 meter
Z = -17231457
30 Z = -5272624
50
XDOT = 1378
963860 XDOT = 501
921033
YDOT = -24983
326559 feet/sec YDOT = -7609
761348 meter/sec
ZDOT = 2369
298945 ZDOT = 724
403237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5574182
96 X = -1699010
97
Y = 12819422
59 feet Y = 3907360
00 meter
Z = -17321950
02 Z = -5279730
37
XDOT = -23023
710054 XDOT = -7017
626824
YDOT = -6804
984707 feet/sec YDOT = -2074
159339 meter/sec
ZDOT = 2380
340195 ZDOT = 725
527691
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 17266
22317826
00016717 00000-0 10270-3 0 9178
2 25544 51
6406 269
6018 0003853 307
8872 52
1932 15
54358053 36998
Satellite: ISS
Catalog Number: 25544
Epoch time: 17266
22317826 = yrday
fracday
Element set: 917
Inclination: 51
6406 deg
RA of node: 269
6018 deg
Eccentricity:
0003853
Arg of perigee: 307
8872 deg
Mean anomaly: 52
1932 deg
Mean motion: 15
54358053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 330
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