[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 20th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 568 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
There are no maneuvers
Coasting Arc #1 (Orbit 2341)
---------------------------------------
Vector Time (GMT): 2015/138/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -642233
12 A = 6778006
50 meter
Y = 5001693
29 meter E =
0008274
Z = -4537228
93 I = 51
34808
XDOT = -6031
404378 Wp = 47
23928
YDOT = -3577
515579 meter/sec RA = 231
29560 deg
ZDOT = -3088
085874 TA = 191
68300
MA = 191
70221
Ha = 218
763 n
mi
Hp = 214
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2107064
05 X = -676074
94
Y = 16409754
90 feet Y = 4994322
50 meter
Z = -14885921
70 Z = -4540430
71
XDOT = -19788
072105 XDOT = -5975
950425
YDOT = -11737
255837 feet/sec YDOT = -3644
652420 meter/sec
ZDOT = -10131
515336 ZDOT = -3117
251371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11895577
12 X = 3625771
91
Y = 11479550
40 feet Y = 3498966
96 meter
Z = -14900523
72 Z = -4541679
63
XDOT = -20405
420081 XDOT = -6219
572041
YDOT = 7824
480762 feet/sec YDOT = 2384
901736 meter/sec
ZDOT = -10255
942528 ZDOT = -3126
011283
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 15138
51612055
00016717 00000-0 10270-3 0 9000
2 25544 51
6451 232
1798 0003876 305
3320 54
7470 15
55016674 23424
Satellite: ISS
Catalog Number: 25544
Epoch time: 15138
51612055 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 232
1798 deg
Eccentricity:
0003876
Arg of perigee: 305
3320 deg
Mean anomaly: 54
7470 deg
Mean motion: 15
55016674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2342
Checksum: 288
Coasting Arc #2 (Orbit 2357)
---------------------------------------
Vector Time (GMT): 2015/139/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2273998
40 A = 6774853
26 meter
Y = -3665015
38 meter E =
0000650
Z = 5224345
45 I = 51
35883
XDOT = 5785
098778 Wp = 4
86492
YDOT = 4946
001081 meter/sec RA = 226
26974 deg
ZDOT = 952
299691 TA = 75
99282
MA = 75
98559
Ha = 218
669 n
mi
Hp = 214
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7460624
66 X = 2289434
15
Y = -12024328
68 feet Y = -3639500
17 meter
Z = 17140240
97 Z = 5235429
46
XDOT = 18979
982867 XDOT = 5724
735463
YDOT = 16227
037666 feet/sec YDOT = 5010
356247 meter/sec
ZDOT = 3124
342819 ZDOT = 980
256814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5404888
86 X = -1647410
12
Y = -13014569
38 feet Y = -3966840
75 meter
Z = 17188409
50 Z = 5239027
22
XDOT = 23323
666998 XDOT = 7109
053701
YDOT = -5405
387510 feet/sec YDOT = -1647
562113 meter/sec
ZDOT = 3243
366972 ZDOT = 988
578253
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 15139
54434330
00016717 00000-0 10270-3 0 9013
2 25544 51
6450 227
0467 0003927 310
7020 49
3792 15
55095893 23587
Satellite: ISS
Catalog Number: 25544
Epoch time: 15139
54434330 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 227
0467 deg
Eccentricity:
0003927
Arg of perigee: 310
7020 deg
Mean anomaly: 49
3792 deg
Mean motion: 15
55095893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2358
Checksum: 304
Coasting Arc #3 (Orbit 2372)
---------------------------------------
Vector Time (GMT): 2015/140/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3854877
03 A = 6775061
70 meter
Y = 2108936
93 meter E =
0011078
Z = -5166430
15 I = 51
38135
XDOT = -4914
756754 Wp = 87
75456
YDOT = -5725
030129 meter/sec RA = 221
24170 deg
ZDOT = 1333
040960 TA = 195
09499
MA = 195
12808
Ha = 218
888 n
mi
Hp = 213
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12647234
36 X = -3853076
28
Y = 6919084
42 feet Y = 2065839
71 meter
Z = -16950230
16 Z = -5185152
06
XDOT = -16124
530033 XDOT = -4856
848316
YDOT = -18782
907248 feet/sec YDOT = -5779
666487 meter/sec
ZDOT = 4373
493962 ZDOT = 1309
305872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1529938
11 X = -466325
14
Y = 14238843
70 feet Y = 4339999
56 meter
Z = -17030889
23 Z = -5191015
04
XDOT = -23612
544923 XDOT = -7197
103693
YDOT = 2562
039960 feet/sec YDOT = 780
909780 meter/sec
ZDOT = 4272
692861 ZDOT = 1302
316784
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 15140
50828194
00016717 00000-0 10270-3 0 9027
2 25544 51
6441 222
2356 0003998 316
9417 43
1423 15
55108197 23739
Satellite: ISS
Catalog Number: 25544
Epoch time: 15140
50828194 = yrday
fracday
Element set: 902
Inclination: 51
6441 deg
RA of node: 222
2356 deg
Eccentricity:
0003998
Arg of perigee: 316
9417 deg
Mean anomaly: 43
1423 deg
Mean motion: 15
55108197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2373
Checksum: 300
Coasting Arc #4 (Orbit 2388)
---------------------------------------
Vector Time (GMT): 2015/141/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5189412
88 A = 6778232
36 meter
Y = -483021
72 meter E =
0009016
Z = 4331897
77 I = 51
41691
XDOT = 3437
886352 Wp = 46
07449
YDOT = 5926
683762 meter/sec RA = 216
21968 deg
ZDOT = -3446
961780 TA = 79
07035
MA = 78
96892
Ha = 218
868 n
mi
Hp = 213
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17025632
82 X = 5173385
55
Y = -1584716
93 feet Y = -425080
32 meter
Z = 14212263
02 Z = 4357068
17
XDOT = 11279
154698 XDOT = 3388
101436
YDOT = 19444
500530 feet/sec YDOT = 5964
850400 meter/sec
ZDOT = -11308
929724 ZDOT = -3430
381444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8165372
67 X = 2488805
59
Y = -14920701
48 feet Y = -4547829
81 meter
Z = 14320309
95 Z = 4364830
47
XDOT = 21377
801389 XDOT = 6515
953864
YDOT = 879
241669 feet/sec YDOT = 267
992861 meter/sec
ZDOT = -11238
833509 ZDOT = -3425
596454
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 15141
53645838
00016717 00000-0 10270-3 0 9034
2 25544 51
6439 217
1020 0004107 321
3845 38
7014 15
55163317 23893
Satellite: ISS
Catalog Number: 25544
Epoch time: 15141
53645838 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 217
1020 deg
Eccentricity:
0004107
Arg of perigee: 321
3845 deg
Mean anomaly: 38
7014 deg
Mean motion: 15
55163317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2389
Checksum: 291
Coasting Arc #5 (Orbit 2403)
---------------------------------------
Vector Time (GMT): 2015/142/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6062394
21 A = 6782725
55 meter
Y = -1004018
25 meter E =
0005639
Z = -2865773
77 I = 51
45709
XDOT = -1457
503274 Wp = 19
18182
YDOT = -5585
611617 meter/sec RA = 211
21369 deg
ZDOT = 5048
226873 TA = 308
10832
MA = 308
15915
Ha = 218
970 n
mi
Hp = 213
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19889744
78 X = -6036795
53
Y = -3294023
13 feet Y = -1071668
54 meter
Z = -9402144
90 Z = -2895161
77
XDOT = -4781
834888 XDOT = -1419
457837
YDOT = -18325
497432 feet/sec YDOT = -5601
698056 meter/sec
ZDOT = 16562
424124 ZDOT = 5041
238522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13575127
72 X = -4137698
93
Y = 14825152
95 feet Y = 4518706
62 meter
Z = -9528043
45 Z = -2904147
64
XDOT = -16943
655305 XDOT = -5164
426137
YDOT = -4905
820058 feet/sec YDOT = -1495
293954 meter/sec
ZDOT = 16533
402319 ZDOT = 5039
381027
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 15142
50035327
00016717 00000-0 10270-3 0 9049
2 25544 51
6429 212
2899 0004118 325
3324 34
7560 15
55167717 24048
Satellite: ISS
Catalog Number: 25544
Epoch time: 15142
50035327 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 212
2899 deg
Eccentricity:
0004118
Arg of perigee: 325
3324 deg
Mean anomaly: 34
7560 deg
Mean motion: 15
55167717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2404
Checksum: 291
Coasting Arc #6 (Orbit 2419)
---------------------------------------
Vector Time (GMT): 2015/143/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6317363
31 A = 6785760
58 meter
Y = 2283345
12 meter E =
0010008
Z = 933922
20 I = 51
49508
XDOT = -860
143356 Wp = 113
86639
YDOT = 4814
519936 meter/sec RA = 206
22235 deg
ZDOT = -5906
535995 TA = 55
99844
MA = 55
90340
Ha = 219
160 n
mi
Hp = 213
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20726257
59 X = 6286824
22
Y = 7491289
76 feet Y = 2353819
19 meter
Z = 3064049
20 Z = 964536
83
XDOT = -2821
992639 XDOT = -885
224686
YDOT = 15795
669083 feet/sec YDOT = 4804
761411 meter/sec
ZDOT = -19378
398933 ZDOT = -5910
775018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17340157
51 X = 5285280
01
Y = -13571898
42 feet Y = -4136714
64 meter
Z = 3195009
27 Z = 973838
83
XDOT = 10962
971643 XDOT = 3341
513757
YDOT = 9406
240683 feet/sec YDOT = 2867
022160 meter/sec
ZDOT = -19397
406041 ZDOT = -5912
329361
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 15143
52848474
00016717 00000-0 10270-3 0 9058
2 25544 51
6428 207
1561 0004176 331
8832 28
2095 15
55218163 24207
Satellite: ISS
Catalog Number: 25544
Epoch time: 15143
52848474 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 207
1561 deg
Eccentricity:
0004176
Arg of perigee: 331
8832 deg
Mean anomaly: 28
2095 deg
Mean motion: 15
55218163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2420
Checksum: 299
Coasting Arc #7 (Orbit 2435)
---------------------------------------
Vector Time (GMT): 2015/144/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5848920
65 A = 6785704
21 meter
Y = -3232456
68 meter E =
0015016
Z = 1125121
90 I = 51
52323
XDOT = 3212
135103 Wp = 40
96920
YDOT = -3757
245976 meter/sec RA = 201
23777 deg
ZDOT = 5870
390968 TA = 331
27487
MA = 331
35749
Ha = 219
343 n
mi
Hp = 213
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19189372
20 X = -5817805
28
Y = -10605172
83 feet Y = -3297689
22 meter
Z = 3691344
80 Z = 1096784
27
XDOT = 10538
500994 XDOT = 3225
394521
YDOT = -12326
922494 feet/sec YDOT = -3721
251959 meter/sec
ZDOT = 19259
812887 ZDOT = 5886
026962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18999544
01 X = -5791061
02
Y = 10981712
99 feet Y = 3347226
12 meter
Z = 3570298
27 Z = 1088226
91
XDOT = -4379
476855 XDOT = -1334
864545
YDOT = -13897
341545 feet/sec YDOT = -4235
909703 meter/sec
ZDOT = 19327
541683 ZDOT = 5891
034705
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 15144
55659421
00016717 00000-0 10270-3 0 9065
2 25544 51
6425 202
0220 0004286 337
4579 22
6385 15
55205156 24367
Satellite: ISS
Catalog Number: 25544
Epoch time: 15144
55659421 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 202
0220 deg
Eccentricity:
0004286
Arg of perigee: 337
4579 deg
Mean anomaly: 22
6385 deg
Mean motion: 15
55205156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2436
Checksum: 296
Coasting Arc #8 (Orbit 2450)
---------------------------------------
Vector Time (GMT): 2015/145/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4658205
68 A = 6782128
84 meter
Y = 3878808
01 meter E =
0003821
Z = -3047491
14 I = 51
54201
XDOT = -5312
180930 Wp = 49
99225
YDOT = 2518
599778 meter/sec RA = 196
24908 deg
ZDOT = -4915
914887 TA = 165
01028
MA = 164
99895
Ha = 219
326 n
mi
Hp = 213
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15282827
04 X = 4629289
36
Y = 12725748
08 feet Y = 3930737
57 meter
Z = -9998330
51 Z = -3024932
43
XDOT = -17428
415125 XDOT = -5316
069909
YDOT = 8263
122630 feet/sec YDOT = 2459
173967 meter/sec
ZDOT = -16128
329681 ZDOT = -4941
729896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18703773
80 X = 5700910
25
Y = -6898682
78 feet Y = -2102718
51 meter
Z = -9902176
58 Z = -3018183
42
XDOT = -2040
725119 XDOT = -622
013016
YDOT = 17768
922416 feet/sec YDOT = 5415
967552 meter/sec
ZDOT = -16239
536080 ZDOT = -4949
810597
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 15145
52042394
00016717 00000-0 10270-3 0 9079
2 25544 51
6427 197
2088 0004220 341
4374 18
6625 15
55276181 24517
Satellite: ISS
Catalog Number: 25544
Epoch time: 15145
52042394 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 197
2088 deg
Eccentricity:
0004220
Arg of perigee: 341
4374 deg
Mean anomaly: 18
6625 deg
Mean motion: 15
55276181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2451
Checksum: 300
Coasting Arc #9 (Orbit 2466)
---------------------------------------
Vector Time (GMT): 2015/146/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2852309
66 A = 6777394
96 meter
Y = -4197458
91 meter E =
0007422
Z = 4485273
56 I = 51
55701
XDOT = 6861
985270 Wp = 84
10519
YDOT = -1231
366297 meter/sec RA = 191
24812 deg
ZDOT = 3207
557112 TA = 333
62322
MA = 333
66098
Ha = 219
423 n
mi
Hp = 213
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9357971
32 X = -2826948
61
Y = -13771190
66 feet Y = -4229213
68 meter
Z = 14715464
45 Z = 4471478
94
XDOT = 22513
075032 XDOT = 6859
663483
YDOT = -4039
915672 feet/sec YDOT = -1154
644193 meter/sec
ZDOT = 10523
481338 ZDOT = 3240
885852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16628291
26 X = -5068303
18
Y = 1560607
16 feet Y = 475673
06 meter
Z = 14656965
86 Z = 4467443
19
XDOT = 7502
057077 XDOT = 2286
626997
YDOT = -20363
768253 feet/sec YDOT = -6206
876564 meter/sec
ZDOT = 10666
729273 ZDOT = 3251
219082
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 15146
54848722
00016717 00000-0 10270-3 0 9082
2 25544 51
6424 192
0746 0004264 345
4571 14
6459 15
55314286 24676
Satellite: ISS
Catalog Number: 25544
Epoch time: 15146
54848722 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 192
0746 deg
Eccentricity:
0004264
Arg of perigee: 345
4571 deg
Mean anomaly: 14
6459 deg
Mean motion: 15
55314286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2467
Checksum: 322
Coasting Arc #10 (Orbit 2481)
---------------------------------------
Vector Time (GMT): 2015/147/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 650111
19 A = 6774230
39 meter
Y = 4254911
14 meter E =
0014760
Z = -5243489
41 I = 51
57854
XDOT = -7596
965651 Wp = 65
54202
YDOT = -49
441373 meter/sec RA = 186
23495 deg
ZDOT = -978
220938 TA = 195
05465
MA = 195
09863
Ha = 219
465 n
mi
Hp = 212
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2132910
73 X = 627954
59
Y = 13959682
23 feet Y = 4262057
42 meter
Z = -17203049
25 Z = -5240384
93
XDOT = -24924
427990 XDOT = -7591
096285
YDOT = -162
209228 feet/sec YDOT = -134
362758 meter/sec
ZDOT = -3209
386281 ZDOT = -1015
111622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13367501
38 X = 4074414
42
Y = 4600617
10 feet Y = 1402268
09 meter
Z = -17190438
30 Z = -5239645
59
XDOT = -11544
456193 XDOT = -3518
750248
YDOT = 20913
101845 feet/sec YDOT = 6374
313442 meter/sec
ZDOT = -3367
722240 ZDOT = -1026
481739
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 15147
51227744
00016717 00000-0 10270-3 0 9096
2 25544 51
6431 187
2612 0004322 349
1942 10
9117 15
55323387 24829
Satellite: ISS
Catalog Number: 25544
Epoch time: 15147
51227744 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 187
2612 deg
Eccentricity:
0004322
Arg of perigee: 349
1942 deg
Mean anomaly: 10
9117 deg
Mean motion: 15
55323387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2482
Checksum: 299
Coasting Arc #11 (Orbit 2497)
---------------------------------------
Vector Time (GMT): 2015/148/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1692567
75 A = 6774305
04 meter
Y = -4051214
96 meter E =
0007589
Z = 5157540
02 I = 51
61034
XDOT = 7428
815480 Wp = 25
15317
YDOT = 1284
526780 meter/sec RA = 181
21883 deg
ZDOT = -1421
459328 TA = 78
56285
MA = 78
47762
Ha = 219
427 n
mi
Hp = 212
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5553043
82 X = 1712689
91
Y = -13291387
66 feet Y = -4032175
26 meter
Z = 16921063
06 Z = 5165811
00
XDOT = 24372
754201 XDOT = 7420
804468
YDOT = 4214
326706 feet/sec YDOT = 1367
555919 meter/sec
ZDOT = -4663
580473 ZDOT = -1385
390546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9344063
65 X = -2848070
60
Y = -10906871
91 feet Y = -3324414
56 meter
Z = 16957248
49 Z = 5168569
34
XDOT = 14083
144432 XDOT = 4292
542423
YDOT = -19113
583456 feet/sec YDOT = -5825
820237 meter/sec
ZDOT = -4508
964173 ZDOT = -1374
332280
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 15148
54029677
00016717 00000-0 10270-3 0 9107
2 25544 51
6422 182
1270 0004389 354
2399 5
8703 15
55389960 24989
Satellite: ISS
Catalog Number: 25544
Epoch time: 15148
54029677 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 182
1270 deg
Eccentricity:
0004389
Arg of perigee: 354
2399 deg
Mean anomaly: 5
8703 deg
Mean motion: 15
55389960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2498
Checksum: 330
Coasting Arc #12 (Orbit 2512)
---------------------------------------
Vector Time (GMT): 2015/149/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3818491
24 A = 6777816
28 meter
Y = 3634594
54 meter E =
0007929
Z = -4265761
49 I = 51
65487
XDOT = -6319
087280 Wp = 79
05166
YDOT = -2430
080716 meter/sec RA = 176
21155 deg
ZDOT = 3593
140538 TA = 227
62240
MA = 227
68954
Ha = 219
552 n
mi
Hp = 212
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12527858
41 X = -3838128
57
Y = 11924522
78 feet Y = 3591784
09 meter
Z = -13995280
48 Z = -4284358
78
XDOT = -20731
913648 XDOT = -6308
898274
YDOT = -7972
705761 feet/sec YDOT = -2500
688090 meter/sec
ZDOT = 11788
518825 ZDOT = 3562
467811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5221843
83 X = 1591618
00
Y = 16419970
33 feet Y = 5004806
96 meter
Z = -14075733
62 Z = -4290283
61
XDOT = -15127
210584 XDOT = -4610
773786
YDOT = 14783
727154 feet/sec YDOT = 4506
080037 meter/sec
ZDOT = 11657
246040 ZDOT = 3553
128593
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 15149
50404578
00016717 00000-0 10270-3 0 9112
2 25544 51
6431 177
3134 0004491 358
6036 1
5104 15
55402431 25139
Satellite: ISS
Catalog Number: 25544
Epoch time: 15149
50404578 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 177
3134 deg
Eccentricity:
0004491
Arg of perigee: 358
6036 deg
Mean anomaly: 1
5104 deg
Mean motion: 15
55402431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2513
Checksum: 275
Coasting Arc #13 (Orbit 2528)
---------------------------------------
Vector Time (GMT): 2015/150/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5489769
41 A = 6782415
63 meter
Y = -2965261
22 meter E =
0013611
Z = 2649842
88 I = 51
70083
XDOT = 4412
686508 Wp = 83
17127
YDOT = 3486
483924 meter/sec RA = 171
22104 deg
ZDOT = -5215
859409 TA = 66
95432
MA = 66
81086
Ha = 219
584 n
mi
Hp = 212
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18011054
49 X = 5509647
50
Y = -9728547
31 feet Y = -2903760
05 meter
Z = 8693710
25 Z = 2676559
66
XDOT = 14477
317940 XDOT = 4398
708960
YDOT = 11438
595552 feet/sec YDOT = 3535
751652 meter/sec
ZDOT = -17112
399635 ZDOT = -5194
456804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1170828
91 X = -356868
65
Y = -20387627
06 feet Y = -6214148
73 meter
Z = 8808923
72 Z = 2684959
95
XDOT = 15066
449805 XDOT = 4592
253900
YDOT = -8253
945685 feet/sec YDOT = -2515
802645 meter/sec
ZDOT = -17021
095418 ZDOT = -5188
029883
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 15150
53202174
00016717 00000-0 10270-3 0 9126
2 25544 51
6416 172
1783 0004516 3
2442 356
8740 15
55455660 25298
Satellite: ISS
Catalog Number: 25544
Epoch time: 15150
53202174 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 172
1783 deg
Eccentricity:
0004516
Arg of perigee: 3
2442 deg
Mean anomaly: 356
8740 deg
Mean motion: 15
55455660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2529
Checksum: 288
Coasting Arc #14 (Orbit 2543)
---------------------------------------
Vector Time (GMT): 2015/151/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6420180
07 A = 6785155
76 meter
Y = 2079138
25 meter E =
0014522
Z = -625426
09 I = 51
74197
XDOT = -1991
243808 Wp = 31
06023
YDOT = -4370
886912 meter/sec RA = 166
24677 deg
ZDOT = 5984
256514 TA = 322
19068
MA = 322
29260
Ha = 219
558 n
mi
Hp = 212
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21063582
90 X = -6439914
19
Y = 6821319
72 feet Y = 2007233
31 meter
Z = -2051922
88 Z = -656662
38
XDOT = -6532
952125 XDOT = -1971
289286
YDOT = -14340
180158 feet/sec YDOT = -4393
043227 meter/sec
ZDOT = 19633
387512 ZDOT = 5974
631376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2397703
01 X = -730819
88
Y = 21997407
77 feet Y = 6704809
89 meter
Z = -2186409
55 Z = -666417
63
XDOT = -14203
250529 XDOT = -4329
150761
YDOT = 376
632459 feet/sec YDOT = 114
797573 meter/sec
ZDOT = 19592
800595 ZDOT = 5971
885621
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 15151
49572891
00016717 00000-0 10270-3 0 9139
2 25544 51
6420 167
3648 0004428 6
5157 353
6054 15
55500480 25441
Satellite: ISS
Catalog Number: 25544
Epoch time: 15151
49572891 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 167
3648 deg
Eccentricity:
0004428
Arg of perigee: 6
5157 deg
Mean anomaly: 353
6054 deg
Mean motion: 15
55500480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2544
Checksum: 304
Coasting Arc #15 (Orbit 2559)
---------------------------------------
Vector Time (GMT): 2015/152/11:51:59
727
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6539209
78 A = 6784380
85 meter
Y = -926302
61 meter E =
0006227
Z = -1550776
80 I = 51
76860
XDOT = -651
277567 Wp = 110
49705
YDOT = 5013
517011 meter/sec RA = 161
27735 deg
ZDOT = -5761
752342 TA = 86
42107
MA = 86
34986
Ha = 219
705 n
mi
Hp = 212
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21454100
32 X = 6556615
12
Y = -3039050
54 feet Y = -853079
41 meter
Z = -5087850
40 Z = -1518967
89
XDOT = -2136
737424 XDOT = -679
302618
YDOT = 16448
546623 feet/sec YDOT = 5006
077890 meter/sec
ZDOT = -18903
386950 ZDOT = -5764
983734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5666684
87 X = 1727205
55
Y = -20946979
16 feet Y = -6384639
25 meter
Z = -4951082
41 Z = -1509089
92
XDOT = 12796
466754 XDOT = 3900
363066
YDOT = 7916
696608 feet/sec YDOT = 2413
009126 meter/sec
ZDOT = -18918
124955 ZDOT = -5766
244486
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 15152
52366083
00016717 00000-0 10270-3 0 9149
2 25544 51
6407 162
2288 0004483 10
4706 349
6543 15
55497289 25603
Satellite: ISS
Catalog Number: 25544
Epoch time: 15152
52366083 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 162
2288 deg
Eccentricity:
0004483
Arg of perigee: 10
4706 deg
Mean anomaly: 349
6543 deg
Mean motion: 15
55497289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2560
Checksum: 316
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