[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 8th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 ET - UTC (sec) : 67 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
254/21:27:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 213
3
257/01:13:13
329 7
0 7
2 7
2
N/A -0
8 0
0 219
3
000/00:02:26
657 -1
0 0
0 217
3
Coasting Arc #1 (Orbit 82)
---------------------------------------
Vector Time (GMT): 2015/250/08:43:40
250
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1010633
47 A = 6777922
43 meter
Y = -4929747
05 meter E =
0009382
Z = -4549972
26 I = 51
83574
XDOT = 6823
123206 Wp = 64
33991
YDOT = 1502
333655 meter/sec RA = 33
13158 deg
ZDOT = -3144
356403 TA = 174
19988
MA = 174
18900
Ha = 219
301 n
mi
Hp = 213
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3315726
60 X = -933330
85
Y = -16173710
80 feet Y = -4940616
69 meter
Z = -14927730
51 Z = -4554693
61
XDOT = 22385
574822 XDOT = 6821
090616
YDOT = 4928
916191 feet/sec YDOT = 1578
622743 meter/sec
ZDOT = -10316
129932 ZDOT = -3111
216310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13093063
85 X = -3990765
86
Y = 10028704
83 feet Y = 3056749
23 meter
Z = -14947135
54 Z = -4555886
91
XDOT = -4755
509246 XDOT = -1449
479218
YDOT = -21366
213641 feet/sec YDOT = -6512
421918 meter/sec
ZDOT = -10173
478384 ZDOT = -3100
876211
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 15250
38529787
00016717 00000-0 10270-3 0 9009
2 25544 51
6416 33
6027 0000991 305
6105 54
4956 15
55027256 837
Satellite: ISS
Catalog Number: 25544
Epoch time: 15250
38529787 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 33
6027 deg
Eccentricity:
0000991
Arg of perigee: 305
6105 deg
Mean anomaly: 54
4956 deg
Mean motion: 15
55027256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 83
Checksum: 300
Coasting Arc #2 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2015/251/08:43:40
250
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -942501
46 A = 6775126
36 meter
Y = 4178696
05 meter E =
0002591
Z = 5247238
70 I = 51
79896
XDOT = -7044
992299 Wp = 117
24348
YDOT = -2863
328323 meter/sec RA = 28
13753 deg
ZDOT = 1013
290243 TA = 323
07184
MA = 323
08968
Ha = 219
432 n
mi
Hp = 213
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3092196
39 X = -1014647
45
Y = 13709632
71 feet Y = 4167753
37 meter
Z = 17215350
07 Z = 5242484
72
XDOT = -23113
491796 XDOT = -7017
372402
YDOT = -9394
121796 feet/sec YDOT = -2941
955557 meter/sec
ZDOT = 3324
443054 ZDOT = 979
134705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13660011
81 X = 4163571
60
Y = -3413708
43 feet Y = -1040498
33 meter
Z = 17194029
71 Z = 5240740
25
XDOT = 1960
250706 XDOT = 597
484415
YDOT = 23874
698364 feet/sec YDOT = 7277
008061 meter/sec
ZDOT = 3177
682004 ZDOT = 968
557475
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 15251
41353307
00016717 00000-0 10270-3 0 9018
2 25544 51
6417 28
4689 0000980 312
9684 47
1387 15
54997750 993
Satellite: ISS
Catalog Number: 25544
Epoch time: 15251
41353307 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 28
4689 deg
Eccentricity:
0000980
Arg of perigee: 312
9684 deg
Mean anomaly: 47
1387 deg
Mean motion: 15
54997750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 99
Checksum: 325
Coasting Arc #3 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2015/252/08:43:40
250
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2929082
76 A = 6775212
49 meter
Y = -3210865
79 meter E =
0013244
Z = -5209180
46 I = 51
77078
XDOT = 6491
853236 Wp = 97
39561
YDOT = 3862
425453 meter/sec RA = 23
13651 deg
ZDOT = 1270
679566 TA = 184
78899
MA = 184
80167
Ha = 219
310 n
mi
Hp = 213
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9609851
59 X = 2990073
70
Y = -10534336
57 feet Y = -3177770
29 meter
Z = -17090487
08 Z = -5194803
30
XDOT = 21298
731089 XDOT = 6442
007759
YDOT = 12671
999517 feet/sec YDOT = 3934
743038 meter/sec
ZDOT = 4168
896214 ZDOT = 1302
093943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13875492
86 X = -4229250
22
Y = -3595725
64 feet Y = -1095977
17 meter
Z = -17027850
66 Z = -5190088
88
XDOT = 870
615598 XDOT = 265
363634
YDOT = -23722
585754 feet/sec YDOT = -7230
644138 meter/sec
ZDOT = 4303
632960 ZDOT = 1311
747326
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 15252
37749027
00016717 00000-0 10270-3 0 9023
2 25544 51
6413 23
6555 0000911 313
9167 46
1911 15
55060595 1148
Satellite: ISS
Catalog Number: 25544
Epoch time: 15252
37749027 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 23
6555 deg
Eccentricity:
0000911
Arg of perigee: 313
9167 deg
Mean anomaly: 46
1911 deg
Mean motion: 15
55060595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 114
Checksum: 285
Coasting Arc #4 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2015/253/08:43:40
250
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4701245
84 A = 6778506
63 meter
Y = 2109106
89 meter E =
0009124
Z = 4399473
70 I = 51
75225
XDOT = -5200
462268 Wp = 64
83669
YDOT = -4511
683657 meter/sec RA = 18
14027 deg
ZDOT = -3385
002888 TA = 59
38998
MA = 59
30003
Ha = 219
404 n
mi
Hp = 213
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15424034
92 X = -4745851
73
Y = 6919642
01 feet Y = 2056285
51 meter
Z = 14433968
83 Z = 4376527
67
XDOT = -17061
884083 XDOT = -5133
182135
YDOT = -14802
111736 feet/sec YDOT = -4569
462815 meter/sec
ZDOT = -11105
652520 ZDOT = -3410
101543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13601626
92 X = 4145775
89
Y = 10180220
22 feet Y = 3102931
12 meter
Z = 14334595
07 Z = 4369184
58
XDOT = -3910
859173 XDOT = -1192
029876
YDOT = 21057
230419 feet/sec YDOT = 6418
243832 meter/sec
ZDOT = -11213
016859 ZDOT = -3417
727539
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 15253
40570086
00016717 00000-0 10270-3 0 9036
2 25544 51
6414 18
5222 0001003 315
2202 44
8871 15
55061576 1309
Satellite: ISS
Catalog Number: 25544
Epoch time: 15253
40570086 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 18
5222 deg
Eccentricity:
0001003
Arg of perigee: 315
2202 deg
Mean anomaly: 44
8871 deg
Mean motion: 15
55061576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 259
Coasting Arc #5 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2015/254/08:43:40
250
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6015186
52 A = 6782876
76 meter
Y = -1000120
43 meter E =
0004467
Z = -2970453
92 I = 51
73714
XDOT = 3263
807874 Wp = 54
57616
YDOT = 4810
460383 meter/sec RA = 13
15449 deg
ZDOT = 4997
416185 TA = 271
52293
MA = 271
57411
Ha = 219
356 n
mi
Hp = 213
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19734863
93 X = 6040352
26
Y = -3281235
00 feet Y = -932714
29 meter
Z = -9745583
72 Z = -2941172
37
XDOT = 10708
031084 XDOT = 3185
498239
YDOT = 15782
350338 feet/sec YDOT = 4846
521169 meter/sec
ZDOT = 16395
722393 ZDOT = 5013
080190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12776634
91 X = -3894318
32
Y = -15473786
27 feet Y = -4716410
05 meter
Z = -9619111
10 Z = -2931905
06
XDOT = 7199
628695 XDOT = 2194
446826
YDOT = -16162
179133 feet/sec YDOT = -4926
232200 meter/sec
ZDOT = 16462
334795 ZDOT = 5017
719645
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 15254
36963777
00016717 00000-0 10270-3 0 9046
2 25544 51
6420 13
7091 0000881 323
8958 36
2136 15
55092524 1455
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
36963777 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 13
7091 deg
Eccentricity:
0000881
Arg of perigee: 323
8958 deg
Mean anomaly: 36
2136 deg
Mean motion: 15
55092524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 305
Coasting Arc #6 (Orbit 153)
---------------------------------------
Vector Time (GMT): 2015/254/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 927453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3115544
30 A = 6778153
43 meter
Y = 4109385
32 meter E =
0008446
Z = 4393013
31 I = 51
70581
XDOT = -6725
463397 Wp = 104
52333
YDOT = 1467
990637 meter/sec RA = 10
56219 deg
ZDOT = 3389
000148 TA = 311
19225
MA = 311
26505
Ha = 219
185 n
mi
Hp = 213
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10221602
04 X = 3048021
18
Y = 13482235
31 feet Y = 4143848
40 meter
Z = 14412773
32 Z = 4407983
36
XDOT = -22065
168625 XDOT = -6757
841319
YDOT = 4816
242247 feet/sec YDOT = 1392
601465 meter/sec
ZDOT = 11118
766890 ZDOT = 3356
250629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3390196
23 X = -1033331
81
Y = 16520186
52 feet Y = 5035352
85 meter
Z = 14476527
86 Z = 4412445
69
XDOT = -17067
882389 XDOT = -5202
290552
YDOT = -13143
397074 feet/sec YDOT = -4006
107428 meter/sec
ZDOT = 10977
252806 ZDOT = 3345
866655
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 15254
94799380
00016717 00000-0 10270-3 0 9058
2 25544 51
6423 10
8255 0001182 329
3238 30
7846 15
55126583 1545
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
94799380 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 10
8255 deg
Eccentricity:
0001182
Arg of perigee: 329
3238 deg
Mean anomaly: 30
7846 deg
Mean motion: 15
55126583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 154
Checksum: 307
Coasting Arc #7 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2015/255/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 927453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1018098
32 A = 6774986
99 meter
Y = -4233105
41 meter E =
0013980
Z = -5203175
02 I = 51
66380
XDOT = 7550
575868 Wp = 75
23787
YDOT = -266
255146 meter/sec RA = 5
55951 deg
ZDOT = -1260
149314 TA = 182
65121
MA = 182
65862
Ha = 219
362 n
mi
Hp = 213
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3340217
59 X = -945412
12
Y = -13888141
10 feet Y = -4244084
75 meter
Z = -17070784
19 Z = -5207943
59
XDOT = 24772
230539 XDOT = 7559
113319
YDOT = -873
540506 feet/sec YDOT = -181
772069 meter/sec
ZDOT = -4134
348143 ZDOT = -1223
449542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8063078
86 X = 2457626
44
Y = -11762228
93 feet Y = -3585127
38 meter
Z = -17090521
34 Z = -5209190
90
XDOT = 16531
689933 XDOT = 5038
859092
YDOT = 17112
848924 feet/sec YDOT = 5215
996352 meter/sec
ZDOT = -3976
046388 ZDOT = -1211
898939
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 15255
91191446
00016717 00000-0 10270-3 0 9066
2 25544 51
6426 6
0125 0001236 341
6953 18
4156 15
55109934 1696
Satellite: ISS
Catalog Number: 25544
Epoch time: 15255
91191446 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 6
0125 deg
Eccentricity:
0001236
Arg of perigee: 341
6953 deg
Mean anomaly: 18
4156 deg
Mean motion: 15
55109934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 296
Coasting Arc #8 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2015/256/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 927453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1228801
69 A = 6774830
76 meter
Y = 4127408
79 meter E =
0004425
Z = 5228109
93 I = 51
63189
XDOT = -7545
089914 Wp = 39
17213
YDOT = -906
689143 meter/sec RA =
54996 deg
ZDOT = -1053
736029 TA = 60
93908
MA = 60
89477
Ha = 219
398 n
mi
Hp = 213
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4031501
62 X = -1300260
19
Y = 13541367
41 feet Y = 4113268
71 meter
Z = 17152591
63 Z = 5221966
52
XDOT = -24754
232002 XDOT = -7529
271686
YDOT = -2974
701912 feet/sec YDOT = -990
975013 meter/sec
ZDOT = -3457
139202 ZDOT = -1090
349959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12678620
90 X = -3864443
65
Y = 6309494
37 feet Y = 1923133
89 meter
Z = 17125299
68 Z = 5219791
34
XDOT = -14391
691896 XDOT = -4386
587690
YDOT = -19073
712440 feet/sec YDOT = -5813
667552 meter/sec
ZDOT = -3614
828796 ZDOT = -1101
799817
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 15256
94008365
00016717 00000-0 10270-3 0 9078
2 25544 51
6429
8797 0001361 344
4567 15
6545 15
55131044 1853
Satellite: ISS
Catalog Number: 25544
Epoch time: 15256
94008365 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node:
8797 deg
Eccentricity:
0001361
Arg of perigee: 344
4567 deg
Mean anomaly: 15
6545 deg
Mean motion: 15
55131044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 185
Checksum: 305
Coasting Arc #9 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2015/257/01:14:26
657
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -616797
42 A = 6778292
44 meter
Y = -4192469
32 meter E =
0008903
Z = -5298075
64 I = 51
62891
XDOT = 7629
951165 Wp = 80
45420
YDOT = -450
433365 meter/sec RA = 359
77563 deg
ZDOT = -531
154612 TA = 184
46879
MA = 184
47674
Ha = 219
324 n
mi
Hp = 217
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2023613
59 X = -544134
35
Y = -13754820
61 feet Y = -4198961
23 meter
Z = -17382137
92 Z = -5300894
83
XDOT = 25032
648180 XDOT = 7637
001090
YDOT = -1477
799755 feet/sec YDOT = -365
070882 meter/sec
ZDOT = -1742
633243 ZDOT = -494
072686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4381870
05 X = -1335593
99
Y = -13179339
97 feet Y = -4017062
82 meter
Z = -17393476
75 Z = -5301531
71
XDOT = 23396
084794 XDOT = 7131
126645
YDOT = -5687
062782 feet/sec YDOT = -1733
416736 meter/sec
ZDOT = -1582
663699 ZDOT = -482
395896
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 15257
06860732
00016717 00000-0 10270-3 0 9087
2 25544 51
6459
2392 0005952 274
3130 85
7342 15
53831784 1879
Satellite: ISS
Catalog Number: 25544
Epoch time: 15257
06860732 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node:
2392 deg
Eccentricity:
0005952
Arg of perigee: 274
3130 deg
Mean anomaly: 85
7342 deg
Mean motion: 15
53831784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 310
Coasting Arc #10 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2015/258/01:14:26
657
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1078627
66 A = 6778700
14 meter
Y = 4229126
05 meter E =
0004211
Z = 5189523
47 I = 51
59852
XDOT = -7548
742485 Wp = 323
15245
YDOT = -337
620361 meter/sec RA = 354
77728 deg
ZDOT = -1291
093240 TA = 139
27373
MA = 139
24224
Ha = 219
407 n
mi
Hp = 217
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3538804
66 X = -1151047
41
Y = 13875085
47 feet Y = 4216659
94 meter
Z = 17025995
65 Z = 5184107
20
XDOT = -24766
215502 XDOT = -7538
134434
YDOT = -1107
678351 feet/sec YDOT = -421
976244 meter/sec
ZDOT = -4235
870209 ZDOT = -1327
737803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -817347
17 X = -249127
42
Y = 14324652
16 feet Y = 4366153
98 meter
Z = 17001821
87 Z = 5182155
31
XDOT = -23420
975382 XDOT = -7138
713297
YDOT = 3889
314294 feet/sec YDOT = 1185
462997 meter/sec
ZDOT = -4393
786952 ZDOT = -1339
226263
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 15258
09764117
00016717 00000-0 10270-3 0 9092
2 25544 51
6457 355
1120 0006128 278
7677 81
2781 15
53868716 2030
Satellite: ISS
Catalog Number: 25544
Epoch time: 15258
09764117 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 355
1120 deg
Eccentricity:
0006128
Arg of perigee: 278
7677 deg
Mean anomaly: 81
2781 deg
Mean motion: 15
53868716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 203
Checksum: 326
Coasting Arc #11 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2015/259/01:14:26
657
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2682717
75 A = 6781208
77 meter
Y = -4196463
81 meter E =
0004124
Z = -4606022
51 I = 51
57551
XDOT = 6957
919922 Wp = 120
27475
YDOT = 1160
175913 meter/sec RA = 349
78005 deg
ZDOT = 2995
506337 TA = 179
65426
MA = 179
65398
Ha = 219
620 n
mi
Hp = 217
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8801567
42 X = 2751818
68
Y = -13767925
89 feet Y = -4166078
16 meter
Z = -15111622
40 Z = -4592821
91
XDOT = 22827
821265 XDOT = 6929
878304
YDOT = 3806
351420 feet/sec YDOT = 1237
827580 meter/sec
ZDOT = 9827
776697 ZDOT = 3029
238447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5720987
98 X = 1743757
14
Y = -15363427
19 feet Y = -4682772
61 meter
Z = -15053900
00 Z = -4588428
72
XDOT = 21929
837262 XDOT = 6684
214397
YDOT = -1605
961902 feet/sec YDOT = -489
497188 meter/sec
ZDOT = 9972
965213 ZDOT = 3039
759797
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 15259
06235183
00016717 00000-0 10270-3 0 9108
2 25544 51
6461 350
3049 0006090 282
9360 77
1112 15
53853577 2183
Satellite: ISS
Catalog Number: 25544
Epoch time: 15259
06235183 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 350
3049 deg
Eccentricity:
0006090
Arg of perigee: 282
9360 deg
Mean anomaly: 77
1112 deg
Mean motion: 15
53853577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 218
Checksum: 295
Coasting Arc #12 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2015/260/01:14:26
657
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4087707
87 A = 6784719
63 meter
Y = 4058246
29 meter E =
0006753
Z = 3582017
31 I = 51
55592
XDOT = -5914
750370 Wp = 69
13828
YDOT = -2037
781600 meter/sec RA = 344
78901 deg
ZDOT = -4431
942160 TA = 68
46561
MA = 68
39364
Ha = 219
818 n
mi
Hp = 217
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13411115
05 X = -4150184
58
Y = 13314456
34 feet Y = 4012185
98 meter
Z = 11752025
31 Z = 3562007
61
XDOT = -19405
348984 XDOT = -5869
994929
YDOT = -6685
635169 feet/sec YDOT = -2103
674564 meter/sec
ZDOT = -14540
492650 ZDOT = -4460
566103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10023780
67 X = -3055248
35
Y = 16083993
23 feet Y = 4902401
14 meter
Z = 11664983
34 Z = 3555486
92
XDOT = -19164
340994 XDOT = -5841
291135
YDOT = -1286
891858 feet/sec YDOT = -392
244638 meter/sec
ZDOT = -14663
480707 ZDOT = -4469
428919
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 15260
09136475
00016717 00000-0 10270-3 0 9118
2 25544 51
6457 345
1776 0006038 287
6060 72
4433 15
53871355 2344
Satellite: ISS
Catalog Number: 25544
Epoch time: 15260
09136475 = yrday
fracday
Element set: 911
Inclination: 51
6457 deg
RA of node: 345
1776 deg
Eccentricity:
0006038
Arg of perigee: 287
6060 deg
Mean anomaly: 72
4433 deg
Mean motion: 15
53871355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 234
Checksum: 306
Coasting Arc #13 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2015/261/01:14:26
657
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5167930
28 A = 6787977
73 meter
Y = -3787008
74 meter E =
0006965
Z = -2228174
01 I = 51
53678
XDOT = 4513
075648 Wp = 346
38680
YDOT = 2953
539475 meter/sec RA = 339
80401 deg
ZDOT = 5450
744200 TA = 348
80971
MA = 348
82519
Ha = 220
019 n
mi
Hp = 217
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16955151
83 X = 5220717
17
Y = -12424569
35 feet Y = -3728922
65 meter
Z = -7310282
17 Z = -2202940
33
XDOT = 14806
678635 XDOT = 4453
235123
YDOT = 9690
090142 feet/sec YDOT = 3003
673710 meter/sec
ZDOT = 17883
019029 ZDOT = 5472
522339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13372192
87 X = 4075844
39
Y = -16267160
68 feet Y = -4958230
58 meter
Z = -7200782
17 Z = -2194798
41
XDOT = 15456
441850 XDOT = 4711
123476
YDOT = 4753
049922 feet/sec YDOT = 1448
729616 meter/sec
ZDOT = 17976
314165 ZDOT = 5479
180557
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 15261
05605290
00016717 00000-0 10270-3 0 9122
2 25544 51
6459 340
3698 0006182 291
4267 68
6226 15
53890192 2491
Satellite: ISS
Catalog Number: 25544
Epoch time: 15261
05605290 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 340
3698 deg
Eccentricity:
0006182
Arg of perigee: 291
4267 deg
Mean anomaly: 68
6226 deg
Mean motion: 15
53890192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 317
Coasting Arc #14 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2015/262/01:14:26
657
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5876701
87 A = 6789939
42 meter
Y = 3330508
17 meter E =
0007370
Z = 646867
55 I = 51
51336
XDOT = -2862
141491 Wp = 139
91719
YDOT = -3887
160112 meter/sec RA = 334
82501 deg
ZDOT = -5956
113225 TA = 33
08769
MA = 33
04161
Ha = 220
124 n
mi
Hp = 217
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19280517
93 X = -5916649
91
Y = 10926864
09 feet Y = 3264567
73 meter
Z = 2122268
88 Z = 618222
05
XDOT = -9390
227989 XDOT = -2789
528777
YDOT = -12753
149973 feet/sec YDOT = -3918
761078 meter/sec
ZDOT = -19541
053889 ZDOT = -5969
840301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15698197
67 X = -4784810
65
Y = 15659269
04 feet Y = 4772945
20 meter
Z = 1998158
83 Z = 609038
81
XDOT = -11178
497511 XDOT = -3407
206041
YDOT = -8690
972153 feet/sec YDOT = -2649
008312 meter/sec
ZDOT = -19599
463192 ZDOT = -5973
916381
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 15262
08504429
00016717 00000-0 10270-3 0 9139
2 25544 51
6456 335
2422 0006082 294
1616 65
8901 15
53864121 2653
Satellite: ISS
Catalog Number: 25544
Epoch time: 15262
08504429 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 335
2422 deg
Eccentricity:
0006082
Arg of perigee: 294
1616 deg
Mean anomaly: 65
8901 deg
Mean motion: 15
53864121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 296
Coasting Arc #15 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2015/263/01:14:26
657
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6156344
04 A = 6789452
29 meter
Y = -2667080
75 meter E =
0012092
Z = 988144
70 I = 51
48374
XDOT = 1120
002143 Wp = 28
10840
YDOT = 4776
991134 meter/sec RA = 329
84480 deg
ZDOT = 5896
645487 TA = 342
62423
MA = 342
66558
Ha = 220
218 n
mi
Hp = 217
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20197979
13 X = 6180910
35
Y = -8750264
91 feet Y = -2598099
00 meter
Z = 3241944
54 Z = 1018111
16
XDOT = 3674
547714 XDOT = 1037
857512
YDOT = 15672
543092 feet/sec YDOT = 4789
056976 meter/sec
ZDOT = 19345
949759 ZDOT = 5901
886322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16888112
65 X = 5147496
74
Y = -14087568
19 feet Y = -4293890
78 meter
Z = 3371613
09 Z = 1027667
67
XDOT = 6802
077005 XDOT = 2073
273071
YDOT = 12803
934818 feet/sec YDOT = 3902
639333 meter/sec
ZDOT = 19367
611478 ZDOT = 5903
247978
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 15263
11402120
00016717 00000-0 10270-3 0 9140
2 25544 51
6453 330
1133 0006295 299
3478 60
7046 15
53933502 2814
Satellite: ISS
Catalog Number: 25544
Epoch time: 15263
11402120 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 330
1133 deg
Eccentricity:
0006295
Arg of perigee: 299
3478 deg
Mean anomaly: 60
7046 deg
Mean motion: 15
53933502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 278
Coasting Arc #16 (Orbit 295)
---------------------------------------
Vector Time (GMT): 2015/264/01:14:26
657
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6037799
39 A = 6787129
13 meter
Y = 1771078
54 meter E =
0001361
Z = -2543445
64 I = 51
44834
XDOT = 591
242294 Wp = 278
75776
YDOT = -5542
199319 meter/sec RA = 324
86022 deg
ZDOT = -5260
114016 TA = 289
87591
MA = 289
89058
Ha = 220
464 n
mi
Hp = 216
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19809053
13 X = -6044800
11
Y = 5810625
12 feet Y = 1703520
53 meter
Z = -8344637
92 Z = -2572793
40
XDOT = 1939
771306 XDOT = 678
724370
YDOT = -18183
068632 feet/sec YDOT = -5535
098953 meter/sec
ZDOT = -17257
591915 ZDOT = -5257
028915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17119003
00 X = -5217872
12
Y = 11444169
00 feet Y = 3488182
71 meter
Z = -8471461
76 Z = -2582101
55
XDOT = -2639
433875 XDOT = -804
499445
YDOT = -16718
686925 feet/sec YDOT = -5095
855775 meter/sec
ZDOT = -17243
226018 ZDOT = -5255
735290
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 15264
07867929
00016717 00000-0 10270-3 0 9159
2 25544 51
6447 325
3061 0006351 302
3118 57
7419 15
53913023 2964
Satellite: ISS
Catalog Number: 25544
Epoch time: 15264
07867929 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 325
3061 deg
Eccentricity:
0006351
Arg of perigee: 302
3118 deg
Mean anomaly: 57
7419 deg
Mean motion: 15
53913023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 296
Checksum: 307
Coasting Arc #17 (Orbit 311)
---------------------------------------
Vector Time (GMT): 2015/265/01:14:26
657
Vector Time (MET): N/A
Weight (LBS) : 926721
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5543337
15 A = 6783517
79 meter
Y = -658495
80 meter E =
0006479
Z = 3846950
17 I = 51
41063
XDOT = -2137
744666 Wp = 69
53710
YDOT = 6104
874244 meter/sec RA = 319
86419 deg
ZDOT = 4121
998659 TA = 337
01214
MA = 337
04112
Ha = 220
559 n
mi
Hp = 216
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18186801
67 X = 5531601
52
Y = -2160419
28 feet Y = -596571
86 meter
Z = 12621227
58 Z = 3873850
24
XDOT = -7013
597987 XDOT = -2225
875146
YDOT = 20029
114973 feet/sec YDOT = 6080
476142 meter/sec
ZDOT = 13523
617648 ZDOT = 4111
399331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16503976
89 X = 5030412
16
Y = -7752604
12 feet Y = -2362993
73 meter
Z = 12737284
97 Z = 3882324
46
XDOT = -994
256042 XDOT = -303
049242
YDOT = 20043
558735 feet/sec YDOT = 6109
276702 meter/sec
ZDOT = 13476
765995 ZDOT = 4107
718275
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 15265
10763693
00016717 00000-0 10270-3 0 9168
2 25544 51
6444 320
1769 0006384 308
3596 51
6983 15
53927780 3124
Satellite: ISS
Catalog Number: 25544
Epoch time: 15265
10763693 = yrday
fracday
Element set: 916
Inclination: 51
6444 deg
RA of node: 320
1769 deg
Eccentricity:
0006384
Arg of perigee: 308
3596 deg
Mean anomaly: 51
6983 deg
Mean motion: 15
53927780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 312
Checksum: 326
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