[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 9th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
191/02:59:28
657 3
1 3
6 3
7
N/A -1
9 -0
4 219
3
000/00:10:57
314 0
7 -0
0 213
8
Coasting Arc #1 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2015/189/10:28:15
059
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6178638
10 A = 6784842
18 meter
Y = 2776824
93 meter E =
0014885
Z = 227539
98 I = 51
52498
XDOT = -2149
309939 Wp = 131
96705
YDOT = -4270
741808 meter/sec RA = 337
32943 deg
ZDOT = -6001
051121 TA = 45
57523
MA = 45
45351
Ha = 219
294 n
mi
Hp = 211
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20271122
39 X = -6210335
31
Y = 9110318
03 feet Y = 2707554
11 meter
Z = 746522
26 Z = 197448
73
XDOT = -7051
541794 XDOT = -2072
243066
YDOT = -14011
620106 feet/sec YDOT = -4294
345522 meter/sec
ZDOT = -19688
487929 ZDOT = -6011
305064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6305904
35 X = 1922039
65
Y = 21314995
16 feet Y = 6496810
52 meter
Z = 616558
79 Z = 187927
12
XDOT = -13262
115164 XDOT = -4042
292702
YDOT = 4522
160608 feet/sec YDOT = 1378
354553 meter/sec
ZDOT = -19731
686582 ZDOT = -6014
218070
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 15189
46881197
00016717 00000-0 10270-3 0 9005
2 25544 51
6415 337
7396 0002417 130
8999 229
2373 15
55668943 31357
Satellite: ISS
Catalog Number: 25544
Epoch time: 15189
46881197 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 337
7396 deg
Eccentricity:
0002417
Arg of perigee: 130
8999 deg
Mean anomaly: 229
2373 deg
Mean motion: 15
55668943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 346
Coasting Arc #2 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2015/190/10:28:15
059
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6304405
38 A = 6783262
21 meter
Y = -1571663
79 meter E =
0015096
Z = 1928387
16 I = 51
49029
XDOT = -414
095269 Wp = 77
06227
YDOT = 5238
767587 meter/sec RA = 332
34147 deg
ZDOT = 5589
844689 TA = 304
25999
MA = 304
40287
Ha = 219
340 n
mi
Hp = 211
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20683744
70 X = 6312144
20
Y = -5156377
25 feet Y = -1501120
66 meter
Z = 6326729
52 Z = 1959031
32
XDOT = -1358
580279 XDOT = -499
798925
YDOT = 17187
557699 feet/sec YDOT = 5233
657301 meter/sec
ZDOT = 18339
385464 ZDOT = 5587
625315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2701188
62 X = -823322
29
Y = -21104984
21 feet Y = -6432799
19 meter
Z = 6458811
74 Z = 1968645
82
XDOT = 15358
949866 XDOT = 4681
407919
YDOT = 3676
490545 feet/sec YDOT = 1120
594318 meter/sec
ZDOT = 18328
753398 ZDOT = 5586
604036
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 15190
49664704
00016717 00000-0 10270-3 0 9014
2 25544 51
6412 332
6034 0002680 137
9228 222
2132 15
55651977 31515
Satellite: ISS
Catalog Number: 25544
Epoch time: 15190
49664704 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 332
6034 deg
Eccentricity:
0002680
Arg of perigee: 137
9228 deg
Mean anomaly: 222
2132 deg
Mean motion: 15
55651977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 293
Coasting Arc #3 (Orbit 3160)
---------------------------------------
Vector Time (GMT): 2015/191/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1043468
45 A = 6778035
09 meter
Y = -4895599
01 meter E =
0009370
Z = -4579535
29 I = 51
45014
XDOT = 6906
195168 Wp = 118
68167
YDOT = -1358
375432 meter/sec RA = 328
83783 deg
ZDOT = 3026
041146 TA = 181
65042
MA = 181
65352
Ha = 219
296 n
mi
Hp = 213
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3423452
92 X = 1120380
27
Y = -16061676
53 feet Y = -4883499
84 meter
Z = -15024722
09 Z = -4574279
93
XDOT = 22658
120631 XDOT = 6906
172227
YDOT = -4456
612311 feet/sec YDOT = -1281
146213 meter/sec
ZDOT = 9927
956517 ZDOT = 3059
589856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10399446
15 X = 3169751
19
Y = -12738051
88 feet Y = -3882558
21 meter
Z = -15001110
32 Z = -4572338
43
XDOT = 21239
797461 XDOT = 6473
890266
YDOT = 5479
557270 feet/sec YDOT = 1670
169056 meter/sec
ZDOT = 10072
478295 ZDOT = 3070
091384
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 15191
13903544
00016717 00000-0 10270-3 0 9025
2 25544 51
6447 329
3968 0001630 227
3811 132
7205 15
54966725 31614
Satellite: ISS
Catalog Number: 25544
Epoch time: 15191
13903544 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 329
3968 deg
Eccentricity:
0001630
Arg of perigee: 227
3811 deg
Mean anomaly: 132
7205 deg
Mean motion: 15
54966725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3161
Checksum: 303
Coasting Arc #4 (Orbit 3176)
---------------------------------------
Vector Time (GMT): 2015/192/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2783473
06 A = 6782416
99 meter
Y = 5250871
92 meter E =
0011619
Z = 3256550
78 I = 51
43783
XDOT = -6035
776889 Wp = 97
89136
YDOT = -258
181785 meter/sec RA = 323
83045 deg
ZDOT = -4729
749377 TA = 44
18845
MA = 44
09571
Ha = 219
288 n
mi
Hp = 213
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9132129
47 X = -2857801
76
Y = 17227270
07 feet Y = 5219329
38 meter
Z = 10684221
73 Z = 3242849
23
XDOT = -19802
417616 XDOT = -6009
465958
YDOT = -847
053099 feet/sec YDOT = -325
530210 meter/sec
ZDOT = -15517
550448 ZDOT = -4759
006056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15798421
25 X = -4815358
80
Y = 11483157
85 feet Y = 3500066
51 meter
Z = 10624226
49 Z = 3238264
23
XDOT = -16518
470004 XDOT = -5034
829657
YDOT = -8213
343020 feet/sec YDOT = -2503
426953 meter/sec
ZDOT = -15643
280369 ZDOT = -4768
071856
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 15192
16730715
00016717 00000-0 10270-3 0 9038
2 25544 51
6444 324
2643 0001605 230
8488 129
2523 15
54975050 31778
Satellite: ISS
Catalog Number: 25544
Epoch time: 15192
16730715 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 324
2643 deg
Eccentricity:
0001605
Arg of perigee: 230
8488 deg
Mean anomaly: 129
2523 deg
Mean motion: 15
54975050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3177
Checksum: 300
Coasting Arc #5 (Orbit 3191)
---------------------------------------
Vector Time (GMT): 2015/193/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4118230
81 A = 6785823
83 meter
Y = -5179357
42 meter E =
0006916
Z = -1489823
26 I = 51
42532
XDOT = 4639
719853 Wp = 32
13078
YDOT = 2039
224930 meter/sec RA = 318
83382 deg
ZDOT = 5754
016892 TA = 311
55196
MA = 311
61125
Ha = 219
125 n
mi
Hp = 213
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13511255
93 X = 4183078
52
Y = -16992642
46 feet Y = -5132941
91 meter
Z = -4887871
58 Z = -1469660
86
XDOT = 15222
177994 XDOT = 4588
621192
YDOT = 6690
370504 feet/sec YDOT = 2090
822955 meter/sec
ZDOT = 18878
008175 ZDOT = 5776
431766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19438030
05 X = 5924711
56
Y = -9711697
97 feet Y = -2960125
54 meter
Z = -4800118
05 Z = -1463075
98
XDOT = 10171
971348 XDOT = 3100
416867
YDOT = 11010
996607 feet/sec YDOT = 3356
151766 meter/sec
ZDOT = 18973
954699 ZDOT = 5783
261392
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 15193
13129567
00016717 00000-0 10270-3 0 9044
2 25544 51
6451 319
4518 0001633 239
8100 120
2892 15
55020834 31923
Satellite: ISS
Catalog Number: 25544
Epoch time: 15193
13129567 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 319
4518 deg
Eccentricity:
0001633
Arg of perigee: 239
8100 deg
Mean anomaly: 120
2892 deg
Mean motion: 15
55020834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3192
Checksum: 291
Coasting Arc #6 (Orbit 3207)
---------------------------------------
Vector Time (GMT): 2015/194/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4975459
53 A = 6786647
16 meter
Y = 4577383
91 meter E =
0010634
Z = -523396
61 I = 51
40505
XDOT = -2913
030091 Wp = 147
47086
YDOT = -3841
062475 meter/sec RA = 313
84362 deg
ZDOT = -5965
892446 TA = 38
19674
MA = 38
12143
Ha = 219
063 n
mi
Hp = 213
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16323686
13 X = -5023732
71
Y = 15017663
76 feet Y = 4521475
22 meter
Z = -1717180
49 Z = -547682
94
XDOT = -9557
185338 XDOT = -2840
882071
YDOT = -12601
911006 feet/sec YDOT = -3873
233762 meter/sec
ZDOT = -19573
137946 ZDOT = -5979
868494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20999715
39 X = -6400713
25
Y = 7115615
12 feet Y = 2168839
49 meter
Z = -1822535
99 Z = -555508
97
XDOT = -2994
436693 XDOT = -912
704304
YDOT = -13814
026619 feet/sec YDOT = -4210
515314 meter/sec
ZDOT = -19632
435598 ZDOT = -5983
966370
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 15194
15953561
00016717 00000-0 10270-3 0 9057
2 25544 51
6455 314
3189 0001698 242
5692 117
5289 15
55006356 32083
Satellite: ISS
Catalog Number: 25544
Epoch time: 15194
15953561 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 314
3189 deg
Eccentricity:
0001698
Arg of perigee: 242
5692 deg
Mean anomaly: 117
5289 deg
Mean motion: 15
55006356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3208
Checksum: 324
Coasting Arc #7 (Orbit 3223)
---------------------------------------
Vector Time (GMT): 2015/195/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5291806
73 A = 6784066
00 meter
Y = -3463269
02 meter E =
0012170
Z = 2439238
61 I = 51
37563
XDOT = 1088
457217 Wp = 74
58404
YDOT = 5421
621745 meter/sec RA = 308
84848 deg
ZDOT = 5317
341290 TA = 312
84229
MA = 312
94449
Ha = 218
956 n
mi
Hp = 213
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17361570
64 X = 5318291
77
Y = -11362431
18 feet Y = -3403944
78 meter
Z = 8002751
33 Z = 2465008
79
XDOT = 3571
053861 XDOT = 1001
921098
YDOT = 17787
472917 feet/sec YDOT = 5433
309090 meter/sec
ZDOT = 17445
345438 ZDOT = 5322
419214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20368920
76 X = 6208447
05
Y = -3720073
11 feet Y = -1133878
28 meter
Z = 8114254
70 Z = 2473224
83
XDOT = -4015
249113 XDOT = -1223
847930
YDOT = 16246
164708 feet/sec YDOT = 4951
831003 meter/sec
ZDOT = 17466
069924 ZDOT = 5323
658113
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 15195
18775875
00016717 00000-0 10270-3 0 9062
2 25544 51
6456 309
1856 0001560 256
0157 104
0823 15
55047243 32244
Satellite: ISS
Catalog Number: 25544
Epoch time: 15195
18775875 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 309
1856 deg
Eccentricity:
0001560
Arg of perigee: 256
0157 deg
Mean anomaly: 104
0823 deg
Mean motion: 15
55047243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3224
Checksum: 310
Coasting Arc #8 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2015/196/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5128747
33 A = 6779555
06 meter
Y = 1858366
65 meter E =
0005509
Z = -4031481
56 I = 51
34191
XDOT = 668
165642 Wp = 67
99719
YDOT = -6573
655147 meter/sec RA = 303
84065 deg
ZDOT = -3882
487086 TA = 161
56507
MA = 161
54509
Ha = 218
838 n
mi
Hp = 213
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16826598
84 X = -5129563
72
Y = 6097003
43 feet Y = 1801009
53 meter
Z = -13226645
54 Z = -4056397
41
XDOT = 2192
144495 XDOT = 760
483554
YDOT = -21567
110063 feet/sec YDOT = -6565
666653 meter/sec
ZDOT = -12737
818523 ZDOT = -3879
017847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17807019
16 X = -5427579
44
Y = -602177
88 feet Y = -183543
82 meter
Z = -13334147
22 Z = -4064248
07
XDOT = 10124
508536 XDOT = 3085
950202
YDOT = -17857
760118 feet/sec YDOT = -5443
045284 meter/sec
ZDOT = -12721
570944 ZDOT = -3877
534824
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 15196
15170242
00016717 00000-0 10270-3 0 9078
2 25544 51
6458 304
3738 0001767 261
7386 98
3567 15
55081342 32392
Satellite: ISS
Catalog Number: 25544
Epoch time: 15196
15170242 = yrday
fracday
Element set: 907
Inclination: 51
6458 deg
RA of node: 304
3738 deg
Eccentricity:
0001767
Arg of perigee: 261
7386 deg
Mean anomaly: 98
3567 deg
Mean motion: 15
55081342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 324
Coasting Arc #9 (Orbit 3254)
---------------------------------------
Vector Time (GMT): 2015/197/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4551768
57 A = 6775679
60 meter
Y = 61285
94 meter E =
0004430
Z = 5017022
59 I = 51
31222
XDOT = -2182
992024 Wp = 136
95377
YDOT = 7107
319587 meter/sec RA = 298
81696 deg
ZDOT = 1889
561068 TA = 294
62863
MA = 294
67477
Ha = 218
733 n
mi
Hp = 213
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14933623
92 X = 4526374
58
Y = 201069
35 feet Y = 112044
29 meter
Z = 16460047
85 Z = 5039072
13
XDOT = -7162
047324 XDOT = -2271
484151
YDOT = 23317
977649 feet/sec YDOT = 7082
412955 meter/sec
ZDOT = 6199
347337 ZDOT = 1878
742509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13774993
07 X = 4198617
89
Y = 5493049
36 feet Y = 1674281
45 meter
Z = 16554839
23 Z = 5045915
00
XDOT = -14664
996187 XDOT = -4469
890838
YDOT = 18195
619434 feet/sec YDOT = 5546
024804 meter/sec
ZDOT = 6151
406671 ZDOT = 1874
948753
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 15197
17989542
00016717 00000-0 10270-3 0 9083
2 25544 51
6458 299
2407 0001613 266
9855 93
1114 15
55101556 32554
Satellite: ISS
Catalog Number: 25544
Epoch time: 15197
17989542 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 299
2407 deg
Eccentricity:
0001613
Arg of perigee: 266
9855 deg
Mean anomaly: 93
1114 deg
Mean motion: 15
55101556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3255
Checksum: 331
Coasting Arc #10 (Orbit 3269)
---------------------------------------
Vector Time (GMT): 2015/198/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3692245
10 A = 6774440
57 meter
Y = -2117281
22 meter E =
0013041
Z = -5281785
51 I = 51
29319
XDOT = 3372
474801 Wp = 92
93892
YDOT = -6867
002815 meter/sec RA = 293
78265 deg
ZDOT = 395
393173 TA = 180
85233
MA = 180
85456
Ha = 218
751 n
mi
Hp = 213
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12113665
03 X = -3642638
31
Y = -6946460
69 feet Y = -2158292
49 meter
Z = -17328692
61 Z = -5299601
07
XDOT = 11064
549871 XDOT = 3447
091993
YDOT = -22529
536796 feet/sec YDOT = -6828
872418 meter/sec
ZDOT = 1297
221697 ZDOT = 411
956313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8907922
49 X = -2715134
77
Y = -10630008
49 feet Y = -3240026
59 meter
Z = -17404873
48 Z = -5305005
44
XDOT = 17311
200927 XDOT = 5276
454043
YDOT = -16748
543104 feet/sec YDOT = -5104
955938 meter/sec
ZDOT = 1369
799355 ZDOT = 417
514843
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 15198
14381077
00016717 00000-0 10270-3 0 9091
2 25544 51
6451 294
4279 0001758 274
0690 86
0262 15
55149592 32702
Satellite: ISS
Catalog Number: 25544
Epoch time: 15198
14381077 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 294
4279 deg
Eccentricity:
0001758
Arg of perigee: 274
0690 deg
Mean anomaly: 86
0262 deg
Mean motion: 15
55149592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3270
Checksum: 327
Coasting Arc #11 (Orbit 3285)
---------------------------------------
Vector Time (GMT): 2015/199/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2644482
71 A = 6776597
52 meter
Y = 4045986
30 meter E =
0006199
Z = 4747125
12 I = 51
28885
XDOT = -4211
772384 Wp = 50
76955
YDOT = 5847
129139 meter/sec RA = 288
75003 deg
ZDOT = -2631
102850 TA = 65
33709
MA = 65
27254
Ha = 218
574 n
mi
Hp = 213
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8676124
38 X = 2575983
68
Y = 13274233
28 feet Y = 4075175
31 meter
Z = 15574557
47 Z = 4759805
16
XDOT = -13818
150867 XDOT = -4264
062703
YDOT = 19183
494552 feet/sec YDOT = 5799
738152 meter/sec
ZDOT = -8632
227199 ZDOT = -2651
689015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3790903
78 X = 1155467
47
Y = 15343825
97 feet Y = 4676798
15 meter
Z = 15628285
16 Z = 4763501
32
XDOT = -18136
217078 XDOT = -5527
918965
YDOT = 13384
919063 feet/sec YDOT = 4079
723330 meter/sec
ZDOT = -8721
887640 ZDOT = -2658
431353
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 15199
17197215
00016717 00000-0 10270-3 0 9106
2 25544 51
6451 289
2950 0001881 280
1320 79
9621 15
55191247 32866
Satellite: ISS
Catalog Number: 25544
Epoch time: 15199
17197215 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 289
2950 deg
Eccentricity:
0001881
Arg of perigee: 280
1320 deg
Mean anomaly: 79
9621 deg
Mean motion: 15
55191247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3286
Checksum: 316
Coasting Arc #12 (Orbit 3300)
---------------------------------------
Vector Time (GMT): 2015/200/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1535192
83 A = 6780999
95 meter
Y = -5592461
19 meter E =
0003292
Z = -3517033
69 I = 51
29273
XDOT = 4688
847402 Wp = 89
73129
YDOT = -4096
564932 meter/sec RA = 283
72695 deg
ZDOT = 4470
937925 TA = 228
62434
MA = 228
65265
Ha = 218
670 n
mi
Hp = 213
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5036721
87 X = -1455458
37
Y = -18347969
80 feet Y = -5609182
72 meter
Z = -11538824
44 Z = -3524297
85
XDOT = 15383
357619 XDOT = 4712
589961
YDOT = -13440
173662 feet/sec YDOT = -4043
998653 meter/sec
ZDOT = 14668
431514 ZDOT = 4493
772456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 950288
94 X = 289648
07
Y = -18984645
88 feet Y = -5786520
06 meter
Z = -11568975
92 Z = -3526223
86
XDOT = 17309
817365 XDOT = 5276
032333
YDOT = -8125
313765 feet/sec YDOT = -2476
595635 meter/sec
ZDOT = 14767
407505 ZDOT = 4501
105808
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 15200
13586144
00016717 00000-0 10270-3 0 9119
2 25544 51
6437 284
4817 0001891 283
6481 76
4461 15
55178671 33014
Satellite: ISS
Catalog Number: 25544
Epoch time: 15200
13586144 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 284
4817 deg
Eccentricity:
0001891
Arg of perigee: 283
6481 deg
Mean anomaly: 76
4461 deg
Mean motion: 15
55178671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3301
Checksum: 307
Coasting Arc #13 (Orbit 3316)
---------------------------------------
Vector Time (GMT): 2015/201/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 398699
78 A = 6784909
08 meter
Y = 6542560
82 meter E =
0012111
Z = 1729807
54 I = 51
29935
XDOT = -4860
304820 Wp = 115
78071
YDOT = 1798
440595 meter/sec RA = 278
71900 deg
ZDOT = -5656
122449 TA = 45
13490
MA = 45
03660
Ha = 218
675 n
mi
Hp = 213
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1308070
15 X = 317107
05
Y = 21465094
57 feet Y = 6546563
06 meter
Z = 5675221
58 Z = 1731546
40
XDOT = -15945
881954 XDOT = -4852
579328
YDOT = 5900
395652 feet/sec YDOT = 1744
132904 meter/sec
ZDOT = -18556
832181 ZDOT = -5679
713632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5065219
18 X = -1543878
81
Y = 20898186
29 feet Y = 6369767
18 meter
Z = 5681446
71 Z = 1731704
96
XDOT = -15336
685007 XDOT = -4674
621590
YDOT = 1378
317257 feet/sec YDOT = 420
111100 meter/sec
ZDOT = -18658
613414 ZDOT = -5687
145369
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 15201
16399455
00016717 00000-0 10270-3 0 9121
2 25544 51
6436 279
3484 0001849 291
4180 68
6776 15
55212487 33175
Satellite: ISS
Catalog Number: 25544
Epoch time: 15201
16399455 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 279
3484 deg
Eccentricity:
0001849
Arg of perigee: 291
4180 deg
Mean anomaly: 68
6776 deg
Mean motion: 15
55212487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3317
Checksum: 330
Coasting Arc #14 (Orbit 3332)
---------------------------------------
Vector Time (GMT): 2015/202/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 679300
81 A = 6786118
49 meter
Y = -6738800
95 meter E =
0011964
Z = 300654
63 I = 51
29810
XDOT = 4750
026853 Wp = 40
15522
YDOT = 751
024251 meter/sec RA = 273
71802 deg
ZDOT = 5976
906934 TA = 323
10237
MA = 323
18462
Ha = 218
651 n
mi
Hp = 213
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2228677
18 X = 753144
76
Y = -22108927
00 feet Y = -6730791
69 meter
Z = 986399
71 Z = 304133
64
XDOT = 15584
077603 XDOT = 4712
242529
YDOT = 2463
990324 feet/sec YDOT = 803
930708 meter/sec
ZDOT = 19609
274718 ZDOT = 5999
889565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8240973
08 X = 2511848
60
Y = -20635545
25 feet Y = -6289714
19 meter
Z = 1002633
57 Z = 305602
71
XDOT = 12672
078653 XDOT = 3862
449574
YDOT = 6037
729319 feet/sec YDOT = 1840
299896 meter/sec
ZDOT = 19707
954181 ZDOT = 6006
984435
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 15202
19211275
00016717 00000-0 10270-3 0 9139
2 25544 51
6421 274
2134 0001902 292
9680 67
1273 15
55220969 33334
Satellite: ISS
Catalog Number: 25544
Epoch time: 15202
19211275 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 274
2134 deg
Eccentricity:
0001902
Arg of perigee: 292
9680 deg
Mean anomaly: 67
1273 deg
Mean motion: 15
55220969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3333
Checksum: 287
Coasting Arc #15 (Orbit 3347)
---------------------------------------
Vector Time (GMT): 2015/203/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1720904
39 A = 6783816
10 meter
Y = 6137413
28 meter E =
0003982
Z = -2318171
11 I = 51
28864
XDOT = -4385
182675 Wp = 143
39886
YDOT = -3258
277674 meter/sec RA = 268
71638 deg
ZDOT = -5378
936093 TA = 62
57824
MA = 62
53774
Ha = 218
665 n
mi
Hp = 213
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5646011
79 X = -1778145
85
Y = 20135870
33 feet Y = 6117849
01 meter
Z = -7605548
27 Z = -2326669
69
XDOT = -14387
082267 XDOT = -4322
293358
YDOT = -10689
887382 feet/sec YDOT = -3306
963873 meter/sec
ZDOT = -17647
428126 ZDOT = -5400
085560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10631913
04 X = -3240607
09
Y = 17992175
82 feet Y = 5484015
19 meter
Z = -7643240
26 Z = -2329659
63
XDOT = -9697
973201 XDOT = -2955
942232
YDOT = -13254
880674 feet/sec YDOT = -4040
087629 meter/sec
ZDOT = -17737
758795 ZDOT = -5406
468881
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 15203
15596076
00016717 00000-0 10270-3 0 9142
2 25544 51
6414 269
4004 0001920 297
1266 62
9692 15
55232143 33486
Satellite: ISS
Catalog Number: 25544
Epoch time: 15203
15596076 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 269
4004 deg
Eccentricity:
0001920
Arg of perigee: 297
1266 deg
Mean anomaly: 62
9692 deg
Mean motion: 15
55232143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3348
Checksum: 302
Coasting Arc #16 (Orbit 3363)
---------------------------------------
Vector Time (GMT): 2015/204/03:04:57
314
Vector Time (MET): N/A
Weight (LBS) : 891754
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2663935
97 A = 6779323
65 meter
Y = -4808790
36 meter E =
0009108
Z = 3960068
03 I = 51
27509
XDOT = 3788
554465 Wp = 96
49940
YDOT = 5368
488955 meter/sec RA = 263
70124 deg
ZDOT = 3961
628417 TA = 312
02184
MA = 312
09934
Ha = 218
569 n
mi
Hp = 213
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8739947
40 X = 2698274
67
Y = -15776871
26 feet Y = -4778808
60 meter
Z = 12992349
18 Z = 3973092
06
XDOT = 12429
640633 XDOT = 3708
997220
YDOT = 17613
152738 feet/sec YDOT = 5410
410105 meter/sec
ZDOT = 12997
468559 ZDOT = 3979
839245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12229781
44 X = 3727637
38
Y = -13200270
93 feet Y = -4023442
58 meter
Z = 13049244
34 Z = 3977409
67
XDOT = 6735
442014 XDOT = 2052
962726
YDOT = 19194
103548 feet/sec YDOT = 5850
362761 meter/sec
ZDOT = 13074
779728 ZDOT = 3985
192861
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 15204
18405115
00016717 00000-0 10270-3 0 9150
2 25544 51
6410 264
2651 0001984 300
9611 59
1347 15
55258574 33649
Satellite: ISS
Catalog Number: 25544
Epoch time: 15204
18405115 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 264
2651 deg
Eccentricity:
0001984
Arg of perigee: 300
9611 deg
Mean anomaly: 59
1347 deg
Mean motion: 15
55258574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3364
Checksum: 293
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list