[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 4th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
126/05:21:08
431 -1
0 4
4 4
4
N/A -3
7 -0
5 216
6
000/00:12:16
861 -2
2 0
1 215
0
133/21:39:30
000 0
0 0
0 0
0
N/A 0
0 0
0 218
0
000/00:00:00
000 0
0 0
0 214
1
136/01:09:28
922 -5
1 7
1 7
1
N/A -0
6 -0
4 218
4
000/00:24:57
845 -4
8 0
1 217
5
Coasting Arc #1 (Orbit 2123)
---------------------------------------
Vector Time (GMT): 2015/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2835108
11 A = 6771375
54 meter
Y = -3317924
39 meter E =
0009027
Z = -5185114
50 I = 51
31570
XDOT = 4740
649346 Wp = 87
42391
YDOT = -5905
507584 meter/sec RA = 301
53361 deg
ZDOT = 1189
009375 TA = 194
02470
MA = 194
04979
Ha = 216
327 n
mi
Hp = 212
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9301535
79 X = -2772607
67
Y = -10885578
72 feet Y = -3349278
99 meter
Z = -17011530
50 Z = -5198735
38
XDOT = 15553
311503 XDOT = 4800
557910
YDOT = -19375
024881 feet/sec YDOT = -5852
159569 meter/sec
ZDOT = 3900
949393 ZDOT = 1212
184586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14089181
87 X = -4294382
63
Y = -2131180
99 feet Y = -649583
97 meter
Z = -17069258
44 Z = -5202709
97
XDOT = -1242
260036 XDOT = -378
640859
YDOT = -23778
288475 feet/sec YDOT = -7247
622327 meter/sec
ZDOT = 4001
386989 ZDOT = 1219
622754
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 15124
51397071
00016717 00000-0 10270-3 0 9003
2 25544 51
6418 302
1562 0005592 298
4190 61
6400 15
56352367 21249
Satellite: ISS
Catalog Number: 25544
Epoch time: 15124
51397071 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 302
1562 deg
Eccentricity:
0005592
Arg of perigee: 298
4190 deg
Mean anomaly: 61
6400 deg
Mean motion: 15
56352367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2124
Checksum: 286
Coasting Arc #2 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2015/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1107905
35 A = 6775495
02 meter
Y = 5235507
09 meter E =
0007613
Z = 4155017
17 I = 51
31367
XDOT = -5342
110542 Wp = 42
42127
YDOT = 4074
830986 meter/sec RA = 296
49446 deg
ZDOT = -3700
538570 TA = 85
79622
MA = 85
70922
Ha = 216
523 n
mi
Hp = 212
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3634860
08 X = 1029094
38
Y = 17176860
52 feet Y = 5247455
70 meter
Z = 13631946
11 Z = 4160207
92
XDOT = -17526
609389 XDOT = -5369
303020
YDOT = 13368
868065 feet/sec YDOT = 4014
940021 meter/sec
ZDOT = -12140
874575 ZDOT = -3726
556055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14168433
54 X = 4318538
54
Y = 10340825
88 feet Y = 3151883
73 meter
Z = 13653186
83 Z = 4161491
35
XDOT = -3190
862570 XDOT = -972
574911
YDOT = 20591
059591 feet/sec YDOT = 6276
154963 meter/sec
ZDOT = -12253
137556 ZDOT = -3734
756327
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 15125
54132531
00016717 00000-0 10270-3 0 9016
2 25544 51
6418 297
0170 0005702 301
9822 58
0777 15
56357565 21401
Satellite: ISS
Catalog Number: 25544
Epoch time: 15125
54132531 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 297
0170 deg
Eccentricity:
0005702
Arg of perigee: 301
9822 deg
Mean anomaly: 58
0777 deg
Mean motion: 15
56357565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2140
Checksum: 291
Coasting Arc #3 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2015/126/05:27:16
861
Vector Time (MET): N/A
Weight (LBS) : 911233
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4642822
72 A = 6775210
25 meter
Y = 1058222
10 meter E =
0006202
Z = -4824962
31 I = 51
29847
XDOT = 909
085805 Wp = 42
78553
YDOT = -7205
806038 meter/sec RA = 292
88735 deg
ZDOT = -2452
551209 TA = 202
99873
MA = 203
02651
Ha = 216
584 n
mi
Hp = 215
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15232357
99 X = -4630872
62
Y = 3471857
29 feet Y = 1006369
96 meter
Z = -15829928
84 Z = -4847487
64
XDOT = 2982
564976 XDOT = 1001
509088
YDOT = -23641
095925 feet/sec YDOT = -7195
123218 meter/sec
ZDOT = -8046
427851 ZDOT = -2447
910642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11475025
74 X = -3497587
85
Y = -10456132
85 feet Y = -3187029
29 meter
Z = -15926651
88 Z = -4854443
49
XDOT = 20393
316903 XDOT = 6215
882992
YDOT = -10143
725162 feet/sec YDOT = -3091
807429 meter/sec
ZDOT = -8025
168828 ZDOT = -2446
071459
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 15126
24763168
00016717 00000-0 10270-3 0 9021
2 25544 51
6453 293
4875 0007074 278
0984 81
9367 15
55545681 21518
Satellite: ISS
Catalog Number: 25544
Epoch time: 15126
24763168 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 293
4875 deg
Eccentricity:
0007074
Arg of perigee: 278
0984 deg
Mean anomaly: 81
9367 deg
Mean motion: 15
55545681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 333
Coasting Arc #4 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2015/127/05:27:16
861
Vector Time (MET): N/A
Weight (LBS) : 911233
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4052616
83 A = 6773133
80 meter
Y = 1242837
30 meter E =
0004887
Z = 5286772
93 I = 51
28025
XDOT = -2309
685403 Wp = 286
12802
YDOT = 7311
477308 meter/sec RA = 287
84918 deg
ZDOT = 53
068935 TA = 163
37174
MA = 163
35571
Ha = 216
787 n
mi
Hp = 215
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13295986
97 X = 4012736
33
Y = 4077550
19 feet Y = 1287933
14 meter
Z = 17345055
55 Z = 5306363
26
XDOT = -7577
708014 XDOT = -2391
530214
YDOT = 23987
786444 feet/sec YDOT = 7285
191274 meter/sec
ZDOT = 174
110679 ZDOT = 41
650203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4388170
31 X = 1337514
31
Y = 13085972
32 feet Y = 3988604
36 meter
Z = 17428767
22 Z = 5312288
25
XDOT = -22944
442973 XDOT = -6993
466218
YDOT = 7535
154375 feet/sec YDOT = 2296
715053 meter/sec
ZDOT = 123
792880 ZDOT = 37
732070
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 15127
27553185
00016717 00000-0 10270-3 0 9032
2 25544 51
6452 288
3522 0007242 281
6930 78
3411 15
55577426 21676
Satellite: ISS
Catalog Number: 25544
Epoch time: 15127
27553185 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 288
3522 deg
Eccentricity:
0007242
Arg of perigee: 281
6930 deg
Mean anomaly: 78
3411 deg
Mean motion: 15
55577426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 312
Coasting Arc #5 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2015/128/05:27:16
861
Vector Time (MET): N/A
Weight (LBS) : 911233
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3206331
22 A = 6775011
58 meter
Y = -3471211
83 meter E =
0004687
Z = -4859404
64 I = 51
27817
XDOT = 3406
955007 Wp = 108
67505
YDOT = -6450
017984 meter/sec RA = 282
80994 deg
ZDOT = 2359
854842 TA = 184
55906
MA = 184
56333
Ha = 217
035 n
mi
Hp = 215
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10519459
37 X = -3143671
52
Y = -11388490
26 feet Y = -3506716
58 meter
Z = -15942928
62 Z = -4874828
52
XDOT = 11177
673907 XDOT = 3467
363990
YDOT = -21161
476324 feet/sec YDOT = -6411
581513 meter/sec
ZDOT = 7742
305912 ZDOT = 2376
551860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2902465
13 X = 884671
37
Y = -15160523
04 feet Y = -4620927
42 meter
Z = -16008371
13 Z = -4879351
52
XDOT = 22510
298270 XDOT = 6861
138913
YDOT = -3941
182278 feet/sec YDOT = -1201
272358 meter/sec
ZDOT = 7815
073099 ZDOT = 2382
034281
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 15128
23917605
00016717 00000-0 10270-3 0 9041
2 25544 51
6457 283
5380 0007263 286
1732 73
8622 15
55577139 21825
Satellite: ISS
Catalog Number: 25544
Epoch time: 15128
23917605 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 283
5380 deg
Eccentricity:
0007263
Arg of perigee: 286
1732 deg
Mean anomaly: 73
8622 deg
Mean motion: 15
55577139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 320
Coasting Arc #6 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2015/129/05:27:16
861
Vector Time (MET): N/A
Weight (LBS) : 911233
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2183542
98 A = 6779518
93 meter
Y = 5314636
39 meter E =
0006141
Z = 3597046
82 I = 51
28712
XDOT = -4188
644557 Wp = 57
23037
YDOT = 4694
439802 meter/sec RA = 277
78255 deg
ZDOT = -4384
632113 TA = 79
92241
MA = 79
85313
Ha = 217
395 n
mi
Hp = 215
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7163854
93 X = 2106477
89
Y = 17436471
11 feet Y = 5338623
17 meter
Z = 11801334
72 Z = 3607467
16
XDOT = -13742
272169 XDOT = -4219
528488
YDOT = 15401
705387 feet/sec YDOT = 4647
427119 meter/sec
ZDOT = -14385
275961 ZDOT = -4405
054773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9462187
63 X = -2884074
79
Y = 16272241
68 feet Y = 4959779
26 meter
Z = 11844998
91 Z = 3610355
67
XDOT = -19346
270738 XDOT = -5896
743321
YDOT = -693
149296 feet/sec YDOT = -211
271905 meter/sec
ZDOT = -14473
674675 ZDOT = -4411
576041
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 15129
26704784
00016717 00000-0 10270-3 0 9058
2 25544 51
6455 278
4031 0007252 290
8296 69
2081 15
55600509 21987
Satellite: ISS
Catalog Number: 25544
Epoch time: 15129
26704784 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 278
4031 deg
Eccentricity:
0007252
Arg of perigee: 290
8296 deg
Mean anomaly: 69
2081 deg
Mean motion: 15
55600509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 319
Coasting Arc #7 (Orbit 2212)
---------------------------------------
Vector Time (GMT): 2015/130/05:27:16
861
Vector Time (MET): N/A
Weight (LBS) : 911233
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1067021
69 A = 6783716
06 meter
Y = -6468051
79 meter E =
0009264
Z = -1720417
73 I = 51
29817
XDOT = 4651
915856 Wp = 347
17132
YDOT = -2272
709171 meter/sec RA = 272
77044 deg
ZDOT = 5662
266933 TA = 353
84677
MA = 353
85814
Ha = 217
522 n
mi
Hp = 214
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3500727
34 X = -986257
89
Y = -21220642
36 feet Y = -6479532
30 meter
Z = -5644415
14 Z = -1725405
16
XDOT = 15262
191129 XDOT = 4649
478725
YDOT = -7456
394919 feet/sec YDOT = -2220
702183 meter/sec
ZDOT = 18576
991251 ZDOT = 5684
859219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14399452
96 X = 4388953
26
Y = -15968666
35 feet Y = -4867249
50 meter
Z = -5664594
06 Z = -1726568
27
XDOT = 14120
153132 XDOT = 4303
822675
YDOT = 6111
721678 feet/sec YDOT = 1862
852767 meter/sec
ZDOT = 18674
236131 ZDOT = 5691
907173
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 15130
23066286
00016717 00000-0 10270-3 0 9066
2 25544 51
6456 273
5882 0007404 294
4715 65
5666 15
55624661 22134
Satellite: ISS
Catalog Number: 25544
Epoch time: 15130
23066286 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 273
5882 deg
Eccentricity:
0007404
Arg of perigee: 294
4715 deg
Mean anomaly: 65
5666 deg
Mean motion: 15
55624661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2213
Checksum: 314
Coasting Arc #8 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2015/131/05:27:16
861
Vector Time (MET): N/A
Weight (LBS) : 911233
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -112066
52 A = 6784956
19 meter
Y = 6764549
10 meter E =
0004996
Z = -468408
92 I = 51
30110
XDOT = -4798
502479 Wp = 170
66033
YDOT = -491
330628 meter/sec RA = 267
76954 deg
ZDOT = -5961
338679 TA = 14
41704
MA = 14
40279
Ha = 217
754 n
mi
Hp = 214
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -367672
32 X = -185425
63
Y = 22193402
57 feet Y = 6762885
73 meter
Z = -1536774
69 Z = -469131
43
XDOT = -15743
118368 XDOT = -4763
693531
YDOT = -1611
977125 feet/sec YDOT = -544
795922 meter/sec
ZDOT = -19558
197767 ZDOT = -5984
564481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17311211
16 X = -5276457
16
Y = 13892117
54 feet Y = 4234317
43 meter
Z = -1541108
49 Z = -469729
87
XDOT = -7715
299362 XDOT = -2351
623246
YDOT = -11789
862529 feet/sec YDOT = -3593
550099 meter/sec
ZDOT = -19657
652059 ZDOT = -5991
652348
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 15131
25850544
00016717 00000-0 10270-3 0 9078
2 25544 51
6452 268
4532 0007392 297
1861 62
8538 15
55600895 22291
Satellite: ISS
Catalog Number: 25544
Epoch time: 15131
25850544 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 268
4532 deg
Eccentricity:
0007392
Arg of perigee: 297
1861 deg
Mean anomaly: 62
8538 deg
Mean motion: 15
55600895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 323
Coasting Arc #9 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2015/132/05:27:16
861
Vector Time (MET): N/A
Weight (LBS) : 911233
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1301950
79 A = 6782062
23 meter
Y = -6130222
25 meter E =
0010022
Z = 2575344
61 I = 51
29345
XDOT = 4627
995716 Wp = 43
52644
YDOT = 3181
834887 meter/sec RA = 262
76400 deg
ZDOT = 5229
205526 TA = 345
62245
MA = 345
65094
Ha = 217
919 n
mi
Hp = 214
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4271492
08 X = 1357893
47
Y = -20112277
71 feet Y = -6115350
18 meter
Z = 8449293
36 Z = 2581805
18
XDOT = 15183
712980 XDOT = 4566
669996
YDOT = 10439
090837 feet/sec YDOT = 3233
245282 meter/sec
ZDOT = 17156
186110 ZDOT = 5251
538644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18005157
84 X = 5487972
11
Y = -9903340
19 feet Y = -3018538
09 meter
Z = 8478093
05 Z = 2584122
76
XDOT = 1178
513090 XDOT = 359
210790
YDOT = 16925
284418 feet/sec YDOT = 5158
826691 meter/sec
ZDOT = 17251
332280 ZDOT = 5258
206079
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 15132
28633122
00016717 00000-0 10270-3 0 9084
2 25544 51
6446 263
3165 0007592 303
0943 56
9481 15
55653830 22456
Satellite: ISS
Catalog Number: 25544
Epoch time: 15132
28633122 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 263
3165 deg
Eccentricity:
0007592
Arg of perigee: 303
0943 deg
Mean anomaly: 56
9481 deg
Mean motion: 15
55653830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 304
Coasting Arc #10 (Orbit 2259)
---------------------------------------
Vector Time (GMT): 2015/133/05:27:16
861
Vector Time (MET): N/A
Weight (LBS) : 911233
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2463173
22 A = 6777143
58 meter
Y = 4681730
56 meter E =
0007499
Z = -4242076
42 I = 51
28136
XDOT = -4102
866296 Wp = 11
52455
YDOT = -5400
147472 meter/sec RA = 257
74487 deg
ZDOT = -3571
360299 TA = 221
77816
MA = 221
83543
Ha = 218
103 n
mi
Hp = 214
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8081276
95 X = -2494735
73
Y = 15360008
41 feet Y = 4654009
23 meter
Z = -13917573
55 Z = -4254118
88
XDOT = -13460
847427 XDOT = -4024
827106
YDOT = -17717
019265 feet/sec YDOT = -5445
592100 meter/sec
ZDOT = -11717
061347 ZDOT = -3591
101835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16788707
04 X = -5117197
91
Y = 4232416
81 feet Y = 1290040
64 meter
Z = -13970029
09 Z = -4258064
87
XDOT = 4654
846843 XDOT = 1418
797318
YDOT = -20552
578874 feet/sec YDOT = -6264
426041 meter/sec
ZDOT = -11800
710912 ZDOT = -3596
856686
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 15133
24990406
00016717 00000-0 10270-3 0 9093
2 25544 51
6438 258
5017 0007701 305
9197 54
1241 15
55675326 22608
Satellite: ISS
Catalog Number: 25544
Epoch time: 15133
24990406 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 258
5017 deg
Eccentricity:
0007701
Arg of perigee: 305
9197 deg
Mean anomaly: 54
1241 deg
Mean motion: 15
55675326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2260
Checksum: 305
Coasting Arc #11 (Orbit 2270)
---------------------------------------
Vector Time (GMT): 2015/133/21:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 893564
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2431361
87 A = 6776286
18 meter
Y = -4505454
42 meter E =
0003020
Z = 4436195
93 I = 51
28117
XDOT = 4248
771982 Wp = 63
00165
YDOT = 5497
104577 meter/sec RA = 254
35249 deg
ZDOT = 3253
920808 TA = 354
06716
MA = 354
07074
Ha = 218
020 n
mi
Hp = 214
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7976909
01 X = 2460012
56
Y = -14781674
62 feet Y = -4478105
11 meter
Z = 14554448
60 Z = 4448076
81
XDOT = 13939
540624 XDOT = 4171
179729
YDOT = 18035
120004 feet/sec YDOT = 5544
183314 meter/sec
ZDOT = 10675
593201 ZDOT = 3274
372270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3687013
03 X = -1123801
57
Y = 16340945
46 feet Y = 4980720
18 meter
Z = 14606176
51 Z = 4451962
60
XDOT = -16962
325584 XDOT = -5170
116838
YDOT = -13448
026855 feet/sec YDOT = -4098
958585 meter/sec
ZDOT = 10762
275933 ZDOT = 3280
341704
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 15133
95651668
00016717 00000-0 10270-3 0 9107
2 25544 51
6412 254
9699 0007487 308
6190 51
4292 15
55717237 22716
Satellite: ISS
Catalog Number: 25544
Epoch time: 15133
95651668 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 254
9699 deg
Eccentricity:
0007487
Arg of perigee: 308
6190 deg
Mean anomaly: 51
4292 deg
Mean motion: 15
55717237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2271
Checksum: 327
Coasting Arc #12 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2015/134/21:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 893564
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3559931
79 A = 6773041
16 meter
Y = 2439383
28 meter E =
0011302
Z = -5228874
31 I = 51
28000
XDOT = -3351
646531 Wp = 52
34341
YDOT = -6833
043279 meter/sec RA = 249
31467 deg
ZDOT = -900
444553 TA = 208
96407
MA = 209
02684
Ha = 218
300 n
mi
Hp = 213
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11679566
26 X = -3561544
63
Y = 8003225
98 feet Y = 2399564
76 meter
Z = -17155099
45 Z = -5246171
99
XDOT = -10996
215652 XDOT = -3270
614611
YDOT = -22418
120995 feet/sec YDOT = -6870
070509 meter/sec
ZDOT = -2954
214413 ZDOT = -916
529643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8850389
80 X = 2697598
81
Y = -10934813
44 feet Y = -3332931
14 meter
Z = -17229677
49 Z = -5251605
70
XDOT = 16046
067430 XDOT = 4890
841353
YDOT = 17776
953332 feet/sec YDOT = 5418
415376 meter/sec
ZDOT = -3021
954399 ZDOT = -921
091701
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 15134
92006847
00016717 00000-0 10270-3 0 9119
2 25544 51
6415 250
1542 0007460 313
6062 46
4472 15
55708148 22860
Satellite: ISS
Catalog Number: 25544
Epoch time: 15134
92006847 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 250
1542 deg
Eccentricity:
0007460
Arg of perigee: 313
6062 deg
Mean anomaly: 46
4472 deg
Mean motion: 15
55708148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2286
Checksum: 293
Coasting Arc #13 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2015/135/21:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 893564
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4474609
06 A = 6773552
41 meter
Y = -104241
01 meter E =
0008513
Z = 5087061
08 I = 51
29451
XDOT = 2028
035342 Wp = 353
07054
YDOT = 7214
191300 meter/sec RA = 244
27310 deg
ZDOT = -1628
021919 TA = 112
76047
MA = 112
67049
Ha = 218
418 n
mi
Hp = 213
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14680475
93 X = 4450730
61
Y = -341998
07 feet Y = -54336
59 meter
Z = 16689832
93 Z = 5108740
29
XDOT = 6653
659260 XDOT = 1955
122286
YDOT = 23668
606627 feet/sec YDOT = 7236
462458 meter/sec
ZDOT = -5341
279261 ZDOT = -1618
346925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13810879
37 X = -4209556
03
Y = 4667079
47 feet Y = 1422525
82 meter
Z = 16782784
02 Z = 5115392
57
XDOT = -13094
880435 XDOT = -3991
319557
YDOT = -19593
796177 feet/sec YDOT = -5972
189075 meter/sec
ZDOT = -5301
075295 ZDOT = -1615
767750
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 15135
94784159
00016717 00000-0 10270-3 0 9122
2 25544 51
6419 245
0183 0007585 317
5743 42
4824 15
55732879 23029
Satellite: ISS
Catalog Number: 25544
Epoch time: 15135
94784159 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 245
0183 deg
Eccentricity:
0007585
Arg of perigee: 317
5743 deg
Mean anomaly: 42
4824 deg
Mean motion: 15
55732879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 325
Coasting Arc #14 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2015/136/01:21:57
845
Vector Time (MET): N/A
Weight (LBS) : 892643
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2642075
28 A = 6778834
78 meter
Y = 3717381
18 meter E =
0005750
Z = -5020439
81 I = 51
29992
XDOT = -4599
365584 Wp = 59
47685
YDOT = -5830
014130 meter/sec RA = 243
52744 deg
ZDOT = -1895
107684 TA = 192
04377
MA = 192
05752
Ha = 218
380 n
mi
Hp = 217
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8668225
99 X = -2659059
65
Y = 12196132
49 feet Y = 3687740
89 meter
Z = -16471259
22 Z = -5033315
95
XDOT = -15089
782099 XDOT = -4524
625228
YDOT = -19127
342947 feet/sec YDOT = -5881
029315 meter/sec
ZDOT = -6217
544894 ZDOT = -1917
269519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9178900
50 X = -2797728
87
Y = -11738338
18 feet Y = -3577845
48 meter
Z = -16527110
22 Z = -5037463
19
XDOT = 21820
696136 XDOT = 6650
948182
YDOT = -8170
799914 feet/sec YDOT = -2490
459814 meter/sec
ZDOT = -6311
521559 ZDOT = -1923
751771
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 15136
07633771
00016717 00000-0 10270-3 0 9131
2 25544 51
6441 244
3775 0007614 268
0547 91
9734 15
54039702 23043
Satellite: ISS
Catalog Number: 25544
Epoch time: 15136
07633771 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 244
3775 deg
Eccentricity:
0007614
Arg of perigee: 268
0547 deg
Mean anomaly: 91
9734 deg
Mean motion: 15
54039702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 308
Coasting Arc #15 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2015/137/01:21:57
845
Vector Time (MET): N/A
Weight (LBS) : 892643
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3600645
64 A = 6777519
56 meter
Y = -2236936
57 meter E =
0005374
Z = 5292975
36 I = 51
31071
XDOT = 4020
142325 Wp = 271
75582
YDOT = 6525
867324 meter/sec RA = 238
50564 deg
ZDOT = 23
391051 TA = 178
02123
MA = 178
01911
Ha = 218
208 n
mi
Hp = 217
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11813141
87 X = 3599680
15
Y = -7339030
75 feet Y = -2196677
39 meter
Z = 17365404
72 Z = 5310464
54
XDOT = 13189
443323 XDOT = 3946
756105
YDOT = 21410
325867 feet/sec YDOT = 6570
412857 meter/sec
ZDOT = 76
742294 ZDOT = 42
742526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3847716
57 X = 1172784
01
Y = 13265874
93 feet Y = 4043438
68 meter
Z = 17440774
47 Z = 5315948
06
XDOT = -23238
528819 XDOT = -7083
103584
YDOT = 6532
570941 feet/sec YDOT = 1991
127623 meter/sec
ZDOT = 158
558877 ZDOT = 48
328746
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 15137
10523512
00016717 00000-0 10270-3 0 9148
2 25544 51
6440 239
2490 0007784 271
9486 88
0775 15
54070593 23205
Satellite: ISS
Catalog Number: 25544
Epoch time: 15137
10523512 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 239
2490 deg
Eccentricity:
0007784
Arg of perigee: 271
9486 deg
Mean anomaly: 88
0775 deg
Mean motion: 15
54070593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 307
Coasting Arc #16 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2015/138/01:21:57
845
Vector Time (MET): N/A
Weight (LBS) : 892643
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4490783
75 A = 6778642
38 meter
Y = 703916
13 meter E =
0005542
Z = -5033684
76 I = 51
33229
XDOT = -3139
936094 Wp = 114
46795
YDOT = -6739
868474 meter/sec RA = 233
48458 deg
ZDOT = 1858
136275 TA = 173
62612
MA = 173
61907
Ha = 218
699 n
mi
Hp = 217
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14733542
49 X = -4473869
10
Y = 2309436
11 feet Y = 653792
11 meter
Z = -16514713
77 Z = -5055459
43
XDOT = -10301
627604 XDOT = -3073
362221
YDOT = -22112
429375 feet/sec YDOT = -6774
609162 meter/sec
ZDOT = 6096
247621 ZDOT = 1843
044083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1538102
81 X = 468813
74
Y = -14729176
14 feet Y = -4489452
89 meter
Z = -16608195
28 Z = -5062177
92
XDOT = 22955
146822 XDOT = 6996
728751
YDOT = -4407
554276 feet/sec YDOT = -1343
422543 meter/sec
ZDOT = 6032
719200 ZDOT = 1838
772812
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
06981580
00016717 00000-0 10270-3 0 9158
2 25544 51
6445 234
4409 0007739 276
3360 83
6911 15
54069030 23350
Satellite: ISS
Catalog Number: 25544
Epoch time: 15138
06981580 = yrday
fracday
Element set: 915
Inclination: 51
6445 deg
RA of node: 234
4409 deg
Eccentricity:
0007739
Arg of perigee: 276
3360 deg
Mean anomaly: 83
6911 deg
Mean motion: 15
54069030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 312
Coasting Arc #17 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2015/139/01:21:57
845
Vector Time (MET): N/A
Weight (LBS) : 892643
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5224007
06 A = 6781602
07 meter
Y = 765632
28 meter E =
0004734
Z = 4257269
07 I = 51
36176
XDOT = 1954
238222 Wp = 22
33448
YDOT = 6500
753828 meter/sec RA = 228
47106 deg
ZDOT = -3561
502885 TA = 104
19029
MA = 104
13769
Ha = 219
286 n
mi
Hp = 217
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17139130
77 X = 5194376
74
Y = 2511916
94 feet Y = 823884
55 meter
Z = 13967418
22 Z = 4282574
82
XDOT = 6411
542724 XDOT = 1898
700746
YDOT = 21327
932507 feet/sec YDOT = 6522
297139 meter/sec
ZDOT = -11684
720751 ZDOT = -3552
143813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6547084
90 X = -1995551
48
Y = 15942270
44 feet Y = 4859204
03 meter
Z = 14075794
63 Z = 4290302
20
XDOT = -21098
680621 XDOT = -6430
877853
YDOT = 1633
696881 feet/sec YDOT = 497
950809 meter/sec
ZDOT = -11645
723205 ZDOT = -3549
616433
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
09868751
00016717 00000-0 10270-3 0 9167
2 25544 51
6441 229
3127 0007777 281
0826 78
9451 15
54102852 23512
Satellite: ISS
Catalog Number: 25544
Epoch time: 15139
09868751 = yrday
fracday
Element set: 916
Inclination: 51
6441 deg
RA of node: 229
3127 deg
Eccentricity:
0007777
Arg of perigee: 281
0826 deg
Mean anomaly: 78
9451 deg
Mean motion: 15
54102852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 323
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