[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 15th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 29062 56 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
136/01:21:30
934 -3
1 5
0 5
0
N/A -3
8 -0
5 219
1
000/00:15:01
868 -0
5 0
2 215
7
Coasting Arc #1 (Orbit 2280)
---------------------------------------
Vector Time (GMT): 2015/134/13:02:26
123
Vector Time (MET): N/A
Weight (LBS) : 911227
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1860159
27 A = 6776385
60 meter
Y = -4974204
44 meter E =
0004741
Z = 4204114
07 I = 51
29426
XDOT = 4725
308349 Wp = 68
29195
YDOT = 4835
293353 meter/sec RA = 251
13182 deg
ZDOT = 3628
657209 TA = 344
39934
MA = 344
41394
Ha = 217
587 n
mi
Hp = 213
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6102884
75 X = 1895221
42
Y = -16319568
37 feet Y = -4953206
85 meter
Z = 13793025
16 Z = 4213235
70
XDOT = 15502
980146 XDOT = 4653
260811
YDOT = 15863
823338 feet/sec YDOT = 4887
732023 meter/sec
ZDOT = 11905
043338 ZDOT = 3651
437175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12614003
34 X = -3844748
22
Y = -11973132
97 feet Y = -3649410
93 meter
Z = 13833006
32 Z = 4216300
33
XDOT = 19796
270191 XDOT = 6033
903154
YDOT = -6983
763499 feet/sec YDOT = -2128
651114 meter/sec
ZDOT = 12001
830924 ZDOT = 3658
158066
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
59821958
00016717 00000-0 10270-3 0 9008
2 25544 51
6458 251
7598 0006994 310
3766 49
6777 15
55981301 22813
Satellite: ISS
Catalog Number: 25544
Epoch time: 15134
59821958 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 251
7598 deg
Eccentricity:
0006994
Arg of perigee: 310
3766 deg
Mean anomaly: 49
6777 deg
Mean motion: 15
55981301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2281
Checksum: 345
Coasting Arc #2 (Orbit 2295)
---------------------------------------
Vector Time (GMT): 2015/135/13:02:26
123
Vector Time (MET): N/A
Weight (LBS) : 911227
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3216005
56 A = 6772440
76 meter
Y = 2975277
06 meter E =
0011451
Z = -5173361
72 I = 51
29249
XDOT = -3950
760081 Wp = 49
83533
YDOT = -6447
822471 meter/sec RA = 246
09584 deg
ZDOT = -1246
837061 TA = 208
10048
MA = 208
16233
Ha = 217
829 n
mi
Hp = 213
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10551199
35 X = -3223906
06
Y = 9761407
68 feet Y = 2939269
45 meter
Z = -16972971
52 Z = -5189003
92
XDOT = -12961
811289 XDOT = -3872
308578
YDOT = -21154
273200 feet/sec YDOT = -6491
563797 meter/sec
ZDOT = -4090
672771 ZDOT = -1265
838945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5070274
65 X = 1545419
71
Y = 13364380
73 feet Y = 4073463
25 meter
Z = -17040548
48 Z = -5193959
18
XDOT = -23505
513275 XDOT = -7164
480446
YDOT = 3576
783260 feet/sec YDOT = 1090
203538 meter/sec
ZDOT = -4170
989997 ZDOT = -1271
317751
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
56159951
00016717 00000-0 10270-3 0 9014
2 25544 51
6459 246
9449 0007184 314
5827 45
4740 15
56002132 22968
Satellite: ISS
Catalog Number: 25544
Epoch time: 15135
56159951 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 246
9449 deg
Eccentricity:
0007184
Arg of perigee: 314
5827 deg
Mean anomaly: 45
4740 deg
Mean motion: 15
56002132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2296
Checksum: 316
Coasting Arc #3 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2015/136/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4418007
44 A = 6775383
29 meter
Y = 349469
81 meter E =
0005231
Z = -5128652
96 I = 51
29958
XDOT = -2267
781128 Wp = 66
84530
YDOT = -7175
265568 meter/sec RA = 243
46990 deg
ZDOT = 1467
837352 TA = 217
33699
MA = 217
37336
Ha = 219
094 n
mi
Hp = 215
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14494775
07 X = -4396673
35
Y = 1146554
49 feet Y = 300184
13 meter
Z = -16826289
22 Z = -5150063
39
XDOT = -7440
226798 XDOT = -2194
507399
YDOT = -23540
897533 feet/sec YDOT = -7200
215706 meter/sec
ZDOT = 4815
739343 ZDOT = 1456
998548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2649198
31 X = 807475
64
Y = -14187869
94 feet Y = -4324462
76 meter
Z = -16918132
14 Z = -5156646
68
XDOT = 23639
719161 XDOT = 7205
386400
YDOT = -1261
976859 feet/sec YDOT = -384
650547 meter/sec
ZDOT = 4770
538362 ZDOT = 1454
060093
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
07539185
00016717 00000-0 10270-3 0 9023
2 25544 51
6456 244
3771 0009929 298
3989 61
6163 15
55043067 23042
Satellite: ISS
Catalog Number: 25544
Epoch time: 15136
07539185 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 244
3771 deg
Eccentricity:
0009929
Arg of perigee: 298
3989 deg
Mean anomaly: 61
6163 deg
Mean motion: 15
55043067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 329
Coasting Arc #4 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2015/137/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5010976
24 A = 6778663
63 meter
Y = 1631247
77 meter E =
0008395
Z = 4268183
12 I = 51
32594
XDOT = 823
077561 Wp = 6
76949
YDOT = 6750
127797 meter/sec RA = 238
44361 deg
ZDOT = -3537
233069 TA = 119
50686
MA = 119
42311
Ha = 219
324 n
mi
Hp = 215
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16440210
76 X = 4971629
13
Y = 5351862
76 feet Y = 1687063
62 meter
Z = 14003225
45 Z = 4292430
47
XDOT = 2700
385698 XDOT = 764
717767
YDOT = 22146
088574 feet/sec YDOT = 6759
005810 meter/sec
ZDOT = -11605
095370 ZDOT = -3533
376138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9185667
49 X = -2799791
45
Y = 14547593
16 feet Y = 4434106
40 meter
Z = 14106889
58 Z = 4299779
94
XDOT = -21090
862265 XDOT = -6428
494818
YDOT = -2050
472237 feet/sec YDOT = -624
983938 meter/sec
ZDOT = -11589
744224 ZDOT = -3532
554040
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
10360500
00016717 00000-0 10270-3 0 9032
2 25544 51
6454 239
2445 0009997 302
8504 57
1686 15
55101092 23201
Satellite: ISS
Catalog Number: 25544
Epoch time: 15137
10360500 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 239
2445 deg
Eccentricity:
0009997
Arg of perigee: 302
8504 deg
Mean anomaly: 57
1686 deg
Mean motion: 15
55101092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 287
Coasting Arc #5 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2015/138/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5220130
57 A = 6782987
56 meter
Y = -3311849
33 meter E =
0009236
Z = -2776035
06 I = 51
35897
XDOT = 879
438436 Wp = 334
61878
YDOT = -5662
017302 meter/sec RA = 233
43109 deg
ZDOT = 5103
029362 TA = 353
74944
MA = 353
76096
Ha = 219
381 n
mi
Hp = 215
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17126412
63 X = -5169223
50
Y = -10865647
40 feet Y = -3369939
44 meter
Z = -9107726
58 Z = -2801270
50
XDOT = 2885
296705 XDOT = 917
897997
YDOT = -18576
172250 feet/sec YDOT = -5651
968101 meter/sec
ZDOT = 16742
222316 ZDOT = 5107
394679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14465964
86 X = 4409226
09
Y = -14147094
72 feet Y = -4312034
47 meter
Z = -9215343
63 Z = -2808836
74
XDOT = 16423
065124 XDOT = 5005
750250
YDOT = 5878
576334 feet/sec YDOT = 1791
790067 meter/sec
ZDOT = 16761
928825 ZDOT = 5109
035906
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
06752023
00016717 00000-0 10270-3 0 9044
2 25544 51
6460 234
4318 0010086 306
6272 53
3953 15
55156941 23353
Satellite: ISS
Catalog Number: 25544
Epoch time: 15138
06752023 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 234
4318 deg
Eccentricity:
0010086
Arg of perigee: 306
6272 deg
Mean anomaly: 53
3953 deg
Mean motion: 15
55156941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 291
Coasting Arc #6 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2015/139/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4949861
78 A = 6785967
28 meter
Y = 4562177
79 meter E =
0003534
Z = 847057
75 I = 51
38829
XDOT = -2718
764427 Wp = 112
79270
YDOT = 4051
002744 meter/sec RA = 228
43365 deg
ZDOT = -5912
584877 TA = 58
01337
MA = 57
97903
Ha = 219
638 n
mi
Hp = 214
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16239703
99 X = 4894363
77
Y = 14967774
90 feet Y = 4617220
01 meter
Z = 2779060
86 Z = 870969
18
XDOT = -8919
830796 XDOT = -2735
140019
YDOT = 13290
691417 feet/sec YDOT = 4020
508630 meter/sec
ZDOT = -19398
244348 ZDOT = -5925
831806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18051394
13 X = -5502064
93
Y = 12701717
68 feet Y = 3871483
55 meter
Z = 2880796
49 Z = 878066
77
XDOT = -10209
631621 XDOT = -3111
895718
YDOT = -10083
853104 feet/sec YDOT = -3073
558426 meter/sec
ZDOT = -19455
753043 ZDOT = -5930
113527
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
09566158
00016717 00000-0 10270-3 0 9051
2 25544 51
6457 229
2989 0010025 310
2584 49
7692 15
55171719 23512
Satellite: ISS
Catalog Number: 25544
Epoch time: 15139
09566158 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 229
2989 deg
Eccentricity:
0010025
Arg of perigee: 310
2584 deg
Mean anomaly: 49
7692 deg
Mean motion: 15
55171719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 327
Coasting Arc #7 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2015/140/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4115244
01 A = 6785452
37 meter
Y = -5241409
65 meter E =
0015136
Z = 1223014
29 I = 51
40872
XDOT = 4490
885766 Wp = 17
01812
YDOT = -2162
947421 meter/sec RA = 223
44110 deg
ZDOT = 5837
358435 TA = 356
33483
MA = 356
34591
Ha = 219
791 n
mi
Hp = 214
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13501456
73 X = -4062268
49
Y = -17196225
87 feet Y = -5287132
90 meter
Z = 4012514
08 Z = 1203151
17
XDOT = 14733
877184 XDOT = 4486
382499
YDOT = -7096
284188 feet/sec YDOT = -2112
753094 meter/sec
ZDOT = 19151
438435 ZDOT = 5859
163459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19493000
17 X = 5941466
45
Y = -9934367
06 feet Y = -3027995
08 meter
Z = 3928241
69 Z = 1197328
07
XDOT = 3401
124084 XDOT = 1036
662621
YDOT = 14289
031446 feet/sec YDOT = 4355
296785 meter/sec
ZDOT = 19245
324896 ZDOT = 5865
975028
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
12376410
00016717 00000-0 10270-3 0 9068
2 25544 51
6454 224
1647 0010294 315
0089 45
0230 15
55255411 23671
Satellite: ISS
Catalog Number: 25544
Epoch time: 15140
12376410 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 224
1647 deg
Eccentricity:
0010294
Arg of perigee: 315
0089 deg
Mean anomaly: 45
0230 deg
Mean motion: 15
55255411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2367
Checksum: 273
Coasting Arc #8 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2015/141/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2745938
36 A = 6781864
32 meter
Y = 5360539
71 meter E =
0006994
Z = -3122896
39 I = 51
42015
XDOT = -5937
738082 Wp = 338
38537
YDOT = 216
134650 meter/sec RA = 218
44398 deg
ZDOT = -4840
161180 TA = 237
68810
MA = 237
75585
Ha = 219
913 n
mi
Hp = 214
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9008984
13 X = 2700961
45
Y = 17587072
52 feet Y = 5390995
39 meter
Z = -10245723
05 Z = -3109665
77
XDOT = -19480
767984 XDOT = -5916
201723
YDOT = 709
103181 feet/sec YDOT = 149
855841 meter/sec
ZDOT = -15879
793898 ZDOT = -4868
953518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18914910
17 X = -5765264
62
Y = 5816683
77 feet Y = 1772925
21 meter
Z = -10189902
80 Z = -3105882
37
XDOT = 3159
105681 XDOT = 962
895412
YDOT = -17819
263180 feet/sec YDOT = -5431
311417 meter/sec
ZDOT = -16003
323307 ZDOT = -4877
812944
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
08757782
00016717 00000-0 10270-3 0 9070
2 25544 51
6449 219
3521 0010364 317
7963 42
2392 15
55289760 23829
Satellite: ISS
Catalog Number: 25544
Epoch time: 15141
08757782 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 219
3521 deg
Eccentricity:
0010364
Arg of perigee: 317
7963 deg
Mean anomaly: 42
2392 deg
Mean motion: 15
55289760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 323
Coasting Arc #9 (Orbit 2397)
---------------------------------------
Vector Time (GMT): 2015/142/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -903257
10 A = 6777035
44 meter
Y = -4940396
40 meter E =
0005196
Z = 4546139
38 I = 51
42958
XDOT = 6847
693912 Wp = 20
78416
YDOT = 1578
265903 meter/sec RA = 213
43231 deg
ZDOT = 3079
368071 TA = 38
34686
MA = 38
30993
Ha = 220
063 n
mi
Hp = 213
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2963441
94 X = -870028
87
Y = -16208649
62 feet Y = -4950311
81 meter
Z = 14915155
45 Z = 4541831
79
XDOT = 22466
187374 XDOT = 6814
577914
YDOT = 5178
037740 feet/sec YDOT = 1654
655866 meter/sec
ZDOT = 10102
913619 ZDOT = 3112
552763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16487821
53 X = 5025488
00
Y = -423811
44 feet Y = -129177
73 meter
Z = 14897526
57 Z = 4540766
10
XDOT = -8729
727145 XDOT = -2660
820834
YDOT = 20081
042590 feet/sec YDOT = 6120
701781 meter/sec
ZDOT = 10244
992269 ZDOT = 3122
673644
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
11561198
00016717 00000-0 10270-3 0 9080
2 25544 51
6445 214
2172 0010376 323
2302 36
8138 15
55342038 23985
Satellite: ISS
Catalog Number: 25544
Epoch time: 15142
11561198 = yrday
fracday
Element set: 908
Inclination: 51
6445 deg
RA of node: 214
2172 deg
Eccentricity:
0010376
Arg of perigee: 323
2302 deg
Mean anomaly: 36
8138 deg
Mean motion: 15
55342038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2398
Checksum: 289
Coasting Arc #10 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2015/143/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1173585
16 A = 6773805
04 meter
Y = 4124427
53 meter E =
0013493
Z = -5252406
98 I = 51
44565
XDOT = -6987
274443 Wp = 39
81417
YDOT = -3039
484846 meter/sec RA = 208
40848 deg
ZDOT = -816
528044 TA = 222
30286
MA = 222
40700
Ha = 220
106 n
mi
Hp = 213
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3850345
03 X = -1194103
93
Y = 13531586
37 feet Y = 4111189
39 meter
Z = -17232306
35 Z = -5258157
59
XDOT = -22924
128750 XDOT = -6948
800483
YDOT = -9972
063144 feet/sec YDOT = -3117
405937 meter/sec
ZDOT = -2678
897781 ZDOT = -850
377797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12855413
35 X = -3918329
99
Y = -5638451
14 feet Y = -1718599
91 meter
Z = -17257681
92 Z = -5260141
45
XDOT = 12736
556015 XDOT = 3882
102273
YDOT = -20306
367572 feet/sec YDOT = -6189
380836 meter/sec
ZDOT = -2823
599924 ZDOT = -860
633257
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
07935958
00016717 00000-0 10270-3 0 9096
2 25544 51
6434 209
4031 0010511 326
3301 33
7183 15
55433460 24131
Satellite: ISS
Catalog Number: 25544
Epoch time: 15143
07935958 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 209
4031 deg
Eccentricity:
0010511
Arg of perigee: 326
3301 deg
Mean anomaly: 33
7183 deg
Mean motion: 15
55433460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 281
Coasting Arc #11 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2015/144/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3291554
74 A = 6774241
20 meter
Y = -3005027
57 meter E =
0011964
Z = 5105485
63 I = 51
47632
XDOT = 6269
481222 Wp = 354
14151
YDOT = 4108
978048 meter/sec RA = 203
38185 deg
ZDOT = -1612
164498 TA = 111
51258
MA = 111
38499
Ha = 220
129 n
mi
Hp = 213
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10799064
09 X = 3300112
41
Y = -9859014
33 feet Y = -2968171
70 meter
Z = 16750280
94 Z = 5121496
03
XDOT = 20569
164115 XDOT = 6230
899007
YDOT = 13480
899108 feet/sec YDOT = 4178
871856 meter/sec
ZDOT = -5289
253601 ZDOT = -1581
801926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8430953
03 X = 2569754
48
Y = 11849715
41 feet Y = 3611793
26 meter
Z = 16819486
80 Z = 5126579
58
XDOT = -15105
893726 XDOT = -4604
276408
YDOT = 18123
897152 feet/sec YDOT = 5524
163852 meter/sec
ZDOT = -5159
674810 ZDOT = -1572
668882
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
10732427
00016717 00000-0 10270-3 0 9109
2 25544 51
6437 204
2683 0010519 329
8803 30
1745 15
55481292 24291
Satellite: ISS
Catalog Number: 25544
Epoch time: 15144
10732427 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 204
2683 deg
Eccentricity:
0010519
Arg of perigee: 329
8803 deg
Mean anomaly: 30
1745 deg
Mean motion: 15
55481292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 294
Coasting Arc #12 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2015/145/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5075498
15 A = 6777920
05 meter
Y = 1770928
55 meter E =
0007317
Z = -4125861
43 I = 51
51746
XDOT = -4713
018989 Wp = 21
13677
YDOT = -4728
218895 meter/sec RA = 198
36419 deg
ZDOT = 3777
098254 TA = 287
80396
MA = 287
88378
Ha = 220
192 n
mi
Hp = 212
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16651896
80 X = -5074881
89
Y = 5810133
05 feet Y = 1714174
66 meter
Z = -13536290
77 Z = -4150515
74
XDOT = -15462
660724 XDOT = -4678
144442
YDOT = -15512
529182 feet/sec YDOT = -4780
728140 meter/sec
ZDOT = 12392
054639 ZDOT = 3754
287703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3969032
58 X = -1209761
13
Y = -17099899
70 feet Y = -5212049
43 meter
Z = -13642385
84 Z = -4158199
20
XDOT = 15865
670319 XDOT = 4835
856313
YDOT = -13468
756922 feet/sec YDOT = -4105
277110 meter/sec
ZDOT = 12294
969122 ZDOT = 3747
506588
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
07101017
00016717 00000-0 10270-3 0 9112
2 25544 51
6425 199
4532 0010535 333
5336 26
5278 15
55525057 24442
Satellite: ISS
Catalog Number: 25544
Epoch time: 15145
07101017 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 199
4532 deg
Eccentricity:
0010535
Arg of perigee: 333
5336 deg
Mean anomaly: 26
5278 deg
Mean motion: 15
55525057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2444
Checksum: 288
Coasting Arc #13 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2015/146/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6316675
97 A = 6782445
00 meter
Y = -477990
17 meter E =
0011113
Z = 2425913
38 I = 51
56420
XDOT = 2432
707436 Wp = 55
82525
YDOT = 4932
855084 meter/sec RA = 193
36554 deg
ZDOT = -5338
777232 TA = 97
00928
MA = 96
88287
Ha = 220
368 n
mi
Hp = 212
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20724002
54 X = 6309767
25
Y = -1568209
23 feet Y = -407391
70 meter
Z = 7959033
39 Z = 2456581
95
XDOT = 7981
323608 XDOT = 2403
300203
YDOT = 16183
907757 feet/sec YDOT = 4959
894998 meter/sec
ZDOT = -17515
673333 ZDOT = -5327
030770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -338204
78 X = -103084
82
Y = 20729579
03 feet Y = 6318375
69 meter
Z = 8090732
03 Z = 2466055
12
XDOT = -15345
626584 XDOT = -4677
346983
YDOT = 6596
414323 feet/sec YDOT = 2010
587086 meter/sec
ZDOT = -17466
091748 ZDOT = -5323
664765
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
09890699
00016717 00000-0 10270-3 0 9127
2 25544 51
6430 194
3182 0010728 337
5528 22
5155 15
55610328 24608
Satellite: ISS
Catalog Number: 25544
Epoch time: 15146
09890699 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 194
3182 deg
Eccentricity:
0010728
Arg of perigee: 337
5528 deg
Mean anomaly: 22
5155 deg
Mean motion: 15
55610328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 309
Coasting Arc #14 (Orbit 2474)
---------------------------------------
Vector Time (GMT): 2015/147/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6725264
88 A = 6784996
07 meter
Y = -733037
11 meter E =
0018872
Z = -321764
49 I = 51
60220
XDOT = 237
532860 Wp = 13
45664
YDOT = -4777
053222 meter/sec RA = 188
38079 deg
ZDOT = 6006
933798 TA = 343
06798
MA = 343
13088
Ha = 220
453 n
mi
Hp = 212
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22064517
34 X = -6715005
03
Y = -2404977
40 feet Y = -808186
05 meter
Z = -1055657
78 Z = -354409
91
XDOT = 779
307284 XDOT = 261
753678
YDOT = -15672
746791 feet/sec YDOT = -4774
261769 meter/sec
ZDOT = 19707
788051 ZDOT = 6008
146351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4046459
54 X = 1233360
87
Y = -21815999
60 feet Y = -6649516
68 meter
Z = -1195651
10 Z = -364434
45
XDOT = 13987
399436 XDOT = 4263
359348
YDOT = 1528
041055 feet/sec YDOT = 465
746913 meter/sec
ZDOT = 19713
794444 ZDOT = 6008
764547
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
06253091
00016717 00000-0 10270-3 0 9135
2 25544 51
6416 189
5027 0010586 341
1065 18
9694 15
55603063 24756
Satellite: ISS
Catalog Number: 25544
Epoch time: 15147
06253091 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 189
5027 deg
Eccentricity:
0010586
Arg of perigee: 341
1065 deg
Mean anomaly: 18
9694 deg
Mean motion: 15
55603063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2475
Checksum: 305
Coasting Arc #15 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2015/148/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6251361
52 A = 6783407
79 meter
Y = 1859894
05 meter E =
0004888
Z = -1876398
68 I = 51
62861
XDOT = -2961
178737 Wp = 22
35736
YDOT = 4282
438880 meter/sec RA = 183
40167 deg
ZDOT = -5621
019771 TA = 178
29228
MA = 178
29061
Ha = 220
527 n
mi
Hp = 211
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20509716
26 X = 6239214
06
Y = 6102014
59 feet Y = 1929733
01 meter
Z = -6156163
65 Z = -1846059
88
XDOT = -9715
153336 XDOT = -2981
540799
YDOT = 14049
996326 feet/sec YDOT = 4249
211405 meter/sec
ZDOT = -18441
665914 ZDOT = -5635
454058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7273992
01 X = -2217112
76
Y = 20163203
78 feet Y = 6145744
51 meter
Z = -6026246
57 Z = -1836799
95
XDOT = -12002
279842 XDOT = -3658
294896
YDOT = -9859
944495 feet/sec YDOT = -3005
311082 meter/sec
ZDOT = -18504
344073 ZDOT = -5640
124073
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
09036212
00016717 00000-0 10270-3 0 9144
2 25544 51
6412 184
3673 0010548 345
2146 14
8697 15
55672192 24910
Satellite: ISS
Catalog Number: 25544
Epoch time: 15148
09036212 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 184
3673 deg
Eccentricity:
0010548
Arg of perigee: 345
2146 deg
Mean anomaly: 14
8697 deg
Mean motion: 15
55672192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 308
Coasting Arc #16 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2015/149/01:29:01
868
Vector Time (MET): N/A
Weight (LBS) : 910673
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4877890
27 A = 6778793
99 meter
Y = -2829843
35 meter E =
0013141
Z = 3745610
40 I = 51
64478
XDOT = 5321
943392 Wp = 46
80847
YDOT = -3525
250221 meter/sec RA = 178
41156 deg
ZDOT = 4266
767007 TA = 358
06527
MA = 358
07035
Ha = 220
603 n
mi
Hp = 211
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16003577
01 X = -4864078
77
Y = -9284262
94 feet Y = -2884314
05 meter
Z = 12288748
04 Z = 3721947
65
XDOT = 17460
444201 XDOT = 5340
241401
YDOT = -11565
781566 feet/sec YDOT = -3465
634649 meter/sec
ZDOT = 13998
579419 ZDOT = 4292
664620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9924815
16 X = 3025083
66
Y = -15693463
15 feet Y = -4783367
57 meter
Z = 12187641
38 Z = 3714793
09
XDOT = 9709
335483 XDOT = 2959
405455
YDOT = 17100
115286 feet/sec YDOT = 5212
115139 meter/sec
ZDOT = 14110
349404 ZDOT = 4300
834498
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
11815815
00016717 00000-0 10270-3 0 9153
2 25544 51
6405 179
2300 0010446 348
4237 11
6675 15
55732563 25073
Satellite: ISS
Catalog Number: 25544
Epoch time: 15149
11815815 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 179
2300 deg
Eccentricity:
0010446
Arg of perigee: 348
4237 deg
Mean anomaly: 11
6675 deg
Mean motion: 15
55732563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 300
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