[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 12th 2013
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) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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 2388)
---------------------------------------
Vector Time (GMT): 2013/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1441727
89 A = 6792961
55 meter
Y = -6209858
66 meter E =
0024093
Z = 2310457
87 I = 52
00704
XDOT = 4444
692511 Wp = 112
32742
YDOT = -3072
789188 meter/sec RA = 93
37372 deg
ZDOT = -5449
015949 TA = 42
05527
MA = 41
87058
Ha = 227
873 n
mi
Hp = 214
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4730078
38 X = -1383404
42
Y = -20373552
04 feet Y = -6225654
58 meter
Z = 7580242
35 Z = 2303596
47
XDOT = 14582
324512 XDOT = 4505
192767
YDOT = -10081
329357 feet/sec YDOT = -3022
748228 meter/sec
ZDOT = -17877
348913 ZDOT = -5427
276574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10238213
87 X = -3120607
59
Y = -18249828
84 feet Y = -5562547
83 meter
Z = 7552354
75 Z = 2301957
73
XDOT = 9989
969584 XDOT = 3044
942729
YDOT = -13014
385660 feet/sec YDOT = -3966
784749 meter/sec
ZDOT = -17786
313917 ZDOT = -5421
268482
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 13098
53684942
00016717 00000-0 10270-3 0 9009
2 25544 51
6418 94
0407 0010388 118
8170 241
4026 15
52111758 23894
Satellite: ISS
Catalog Number: 25544
Epoch time: 13098
53684942 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 94
0407 deg
Eccentricity:
0010388
Arg of perigee: 118
8170 deg
Mean anomaly: 241
4026 deg
Mean motion: 15
52111758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2389
Checksum: 307
Coasting Arc #2 (Orbit 2403)
---------------------------------------
Vector Time (GMT): 2013/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1242060
05 A = 6794333
69 meter
Y = 6541425
97 meter E =
0014265
Z = -1361193
91 I = 52
01252
XDOT = -4505
519047 Wp = 85
34620
YDOT = 2059
392204 meter/sec RA = 88
43551 deg
ZDOT = 5839
247064 TA = 259
93164
MA = 260
09262
Ha = 227
828 n
mi
Hp = 214
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4075000
15 X = 1175432
49
Y = 21461371
29 feet Y = 6554942
77 meter
Z = -4465859
29 Z = -1355322
64
XDOT = -14781
886638 XDOT = -4556
578521
YDOT = 6756
536102 feet/sec YDOT = 2008
723842 meter/sec
ZDOT = 19157
634723 ZDOT = 5817
235177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10225698
43 X = 3116792
88
Y = 19309126
11 feet Y = 5885421
64 meter
Z = -4442153
02 Z = -1353968
24
XDOT = -10849
283421 XDOT = -3306
861587
YDOT = 10090
915272 feet/sec YDOT = 3075
710975 meter/sec
ZDOT = 19065
578369 ZDOT = 5811
188287
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 13099
50263982
00016717 00000-0 10270-3 0 9015
2 25544 51
6415 89
2412 0010576 122
9044 237
3127 15
52138917 24048
Satellite: ISS
Catalog Number: 25544
Epoch time: 13099
50263982 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 89
2412 deg
Eccentricity:
0010576
Arg of perigee: 122
9044 deg
Mean anomaly: 237
3127 deg
Mean motion: 15
52138917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2404
Checksum: 297
Coasting Arc #3 (Orbit 2419)
---------------------------------------
Vector Time (GMT): 2013/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -987691
99 A = 6795081
39 meter
Y = -6706335
26 meter E =
0022899
Z = 284136
16 I = 52
01343
XDOT = 4636
131493 Wp = 129
05367
YDOT = -951
726618 meter/sec RA = 83
49763 deg
ZDOT = -6036
671484 TA = 47
90042
MA = 47
70595
Ha = 227
708 n
mi
Hp = 214
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3240459
29 X = -914007
18
Y = -22002412
26 feet Y = -6716968
23 meter
Z = 932205
25 Z = 279517
66
XDOT = 15210
405161 XDOT = 4675
754241
YDOT = -3122
462657 feet/sec YDOT = -899
661564 meter/sec
ZDOT = -19805
352638 ZDOT = -6014
052937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9910108
10 X = -3020600
95
Y = -19910563
31 feet Y = -6068739
70 meter
Z = 913758
43 Z = 278513
57
XDOT = 12155
482233 XDOT = 3704
990985
YDOT = -7002
488915 feet/sec YDOT = -2134
358621 meter/sec
ZDOT = -19710
896371 ZDOT = -6007
881214
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 13100
53280091
00016717 00000-0 10270-3 0 9022
2 25544 51
6418 84
1195 0010332 125
9294 234
2818 15
52142616 24205
Satellite: ISS
Catalog Number: 25544
Epoch time: 13100
53280091 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 84
1195 deg
Eccentricity:
0010332
Arg of perigee: 125
9294 deg
Mean anomaly: 234
2818 deg
Mean motion: 15
52142616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2420
Checksum: 271
Coasting Arc #4 (Orbit 2435)
---------------------------------------
Vector Time (GMT): 2013/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 766814
40 A = 6794699
74 meter
Y = 6707916
01 meter E =
0018565
Z = 740945
60 I = 52
00827
XDOT = -4790
106223 Wp = 86
34456
YDOT = -126
935590 meter/sec RA = 78
56137 deg
ZDOT = 5978
836277 TA = 281
61187
MA = 281
82020
Ha = 227
591 n
mi
Hp = 214
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2515795
28 X = 688148
69
Y = 22007598
46 feet Y = 6716051
23 meter
Z = 2430923
89 Z = 744479
10
XDOT = -15715
571599 XDOT = -4817
374799
YDOT = -416
455348 feet/sec YDOT = -180
653514 meter/sec
ZDOT = 19615
604584 ZDOT = 5955
499799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9548337
71 X = 2910333
33
Y = 19985621
37 feet Y = 6091617
39 meter
Z = 2444829
74 Z = 745184
10
XDOT = -13646
797480 XDOT = -4159
543872
YDOT = 4081
286461 feet/sec YDOT = 1243
976113 meter/sec
ZDOT = 19518
285172 ZDOT = 5949
173320
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 13101
56294465
00016717 00000-0 10270-3 0 9037
2 25544 51
6417 78
9999 0010465 130
9365 229
2694 15
52202075 24368
Satellite: ISS
Catalog Number: 25544
Epoch time: 13101
56294465 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 78
9999 deg
Eccentricity:
0010465
Arg of perigee: 130
9365 deg
Mean anomaly: 229
2694 deg
Mean motion: 15
52202075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2436
Checksum: 319
Coasting Arc #5 (Orbit 2450)
---------------------------------------
Vector Time (GMT): 2013/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -440256
39 A = 6793588
59 meter
Y = -6526380
84 meter E =
0017495
Z = -1814617
03 I = 51
99833
XDOT = 4992
203524 Wp = 136
44416
YDOT = 1231
626317 meter/sec RA = 73
62247 deg
ZDOT = -5685
629889 TA = 63
38632
MA = 63
20719
Ha = 227
507 n
mi
Hp = 214
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1444410
72 X = -358429
22
Y = -21412010
63 feet Y = -6530846
67 meter
Z = -5953467
93 Z = -1816556
57
XDOT = 16378
620484 XDOT = 5005
679865
YDOT = 4040
768758 feet/sec YDOT = 1287
527235 meter/sec
ZDOT = -18653
641369 ZDOT = -5661
345189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8659780
46 X = -2639501
09
Y = -19633699
77 feet Y = -5984351
69 meter
Z = -5960732
98 Z = -1816831
41
XDOT = 15447
323455 XDOT = 4708
344189
YDOT = -1225
409009 feet/sec YDOT = -373
504666 meter/sec
ZDOT = -18552
505992 ZDOT = -5654
803826
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 13102
52869350
00016717 00000-0 10270-3 0 9046
2 25544 51
6426 74
1986 0010232 133
2889 226
9118 15
52183366 24514
Satellite: ISS
Catalog Number: 25544
Epoch time: 13102
52869350 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 74
1986 deg
Eccentricity:
0010232
Arg of perigee: 133
2889 deg
Mean anomaly: 226
9118 deg
Mean motion: 15
52183366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2451
Checksum: 304
Coasting Arc #6 (Orbit 2466)
---------------------------------------
Vector Time (GMT): 2013/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 109957
23 A = 6791624
50 meter
Y = 6202920
18 meter E =
0020720
Z = 2753542
51 I = 51
98306
XDOT = -5205
473480 Wp = 104
11041
YDOT = -2219
714794 meter/sec RA = 68
68186 deg
ZDOT = 5170
790857 TA = 286
88246
MA = 287
10957
Ha = 227
354 n
mi
Hp = 214
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 360752
08 X = 27210
52
Y = 20350787
98 feet Y = 6203687
27 meter
Z = 9033932
13 Z = 2753875
36
XDOT = -17078
325066 XDOT = -5205
383945
YDOT = -7282
528852 feet/sec YDOT = -2277
924904 meter/sec
ZDOT = 16964
536933 ZDOT = 5145
503097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7586323
99 X = 2312311
55
Y = 18887078
35 feet Y = 5756781
48 meter
Z = 9034522
84 Z = 2753722
56
XDOT = -17273
823962 XDOT = -5265
061544
YDOT = -1184
994797 feet/sec YDOT = -361
186414 meter/sec
ZDOT = 16859
346187 ZDOT = 5138
728718
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 13103
55880691
00016717 00000-0 10270-3 0 9052
2 25544 51
6430 69
0792 0010272 138
2524 221
9413 15
52239528 24674
Satellite: ISS
Catalog Number: 25544
Epoch time: 13103
55880691 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 69
0792 deg
Eccentricity:
0010272
Arg of perigee: 138
2524 deg
Mean anomaly: 221
9413 deg
Mean motion: 15
52239528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2467
Checksum: 300
Coasting Arc #7 (Orbit 2481)
---------------------------------------
Vector Time (GMT): 2013/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 363400
16 A = 6789213
73 meter
Y = -5715683
13 meter E =
0013748
Z = -3649688
25 I = 51
96366
XDOT = 5407
586755 Wp = 120
23538
YDOT = 3151
445665 meter/sec RA = 63
73532 deg
ZDOT = -4416
078668 TA = 102
78982
MA = 102
63616
Ha = 227
278 n
mi
Hp = 214
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1192257
73 X = 445016
57
Y = -18752241
24 feet Y = -5711163
17 meter
Z = -11974042
82 Z = -3647724
39
XDOT = 17741
426362 XDOT = 5393
397104
YDOT = 10339
388664 feet/sec YDOT = 3211
837189 meter/sec
ZDOT = -14488
447072 ZDOT = -4389
843350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5854447
12 X = -1784435
48
Y = -17860779
61 feet Y = -5443965
62 meter
Z = -11965104
78 Z = -3646963
94
XDOT = 19103
083431 XDOT = 5822
619830
YDOT = 3329
219108 feet/sec YDOT = 1014
745984 meter/sec
ZDOT = -14379
428480 ZDOT = -4382
849801
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 13104
52452625
00016717 00000-0 10270-3 0 9063
2 25544 51
6437 64
2781 0010130 140
7123 219
4766 15
52234211 24826
Satellite: ISS
Catalog Number: 25544
Epoch time: 13104
52452625 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 64
2781 deg
Eccentricity:
0010130
Arg of perigee: 140
7123 deg
Mean anomaly: 219
4766 deg
Mean motion: 15
52234211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2482
Checksum: 273
Coasting Arc #8 (Orbit 2497)
---------------------------------------
Vector Time (GMT): 2013/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -861439
44 A = 6786728
07 meter
Y = 5138848
93 meter E =
0018753
Z = 4342597
36 I = 51
94191
XDOT = -5582
772384 Wp = 127
09040
YDOT = -3916
611409 meter/sec RA = 58
78552 deg
ZDOT = 3505
871394 TA = 287
30974
MA = 287
51481
Ha = 227
114 n
mi
Hp = 214
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2826244
89 X = -939934
52
Y = 16859740
59 feet Y = 5128777
03 meter
Z = 14247366
66 Z = 4338221
68
XDOT = -18316
182363 XDOT = -5555
591829
YDOT = -12849
774963 feet/sec YDOT = -3978
889392 meter/sec
ZDOT = 11502
202737 ZDOT = 3478
816651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3904503
22 X = 1190092
58
Y = 16659305
88 feet Y = 5077756
43 meter
Z = 14228434
63 Z = 4336826
87
XDOT = -20730
531610 XDOT = -6318
666035
YDOT = -4929
339167 feet/sec YDOT = -1502
462578 meter/sec
ZDOT = 11389
871384 ZDOT = 3471
632798
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 13105
55460853
00016717 00000-0 10270-3 0 9070
2 25544 51
6442 59
1587 0010134 145
7177 214
4631 15
52286512 24981
Satellite: ISS
Catalog Number: 25544
Epoch time: 13105
55460853 = yrday
fracday
Element set: 907
Inclination: 51
6442 deg
RA of node: 59
1587 deg
Eccentricity:
0010134
Arg of perigee: 145
7177 deg
Mean anomaly: 214
4631 deg
Mean motion: 15
52286512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2498
Checksum: 305
Coasting Arc #9 (Orbit 2512)
---------------------------------------
Vector Time (GMT): 2013/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1507707
24 A = 6784596
03 meter
Y = -4451151
27 meter E =
0017449
Z = -4905900
83 I = 51
91817
XDOT = 5663
259172 Wp = 106
53603
YDOT = 4554
503471 meter/sec RA = 53
82818 deg
ZDOT = -2403
764810 TA = 140
01576
MA = 139
88715
Ha = 227
043 n
mi
Hp = 215
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4946546
07 X = 1581200
65
Y = -14603514
66 feet Y = -4433880
38 meter
Z = -16095475
15 Z = -4898397
80
XDOT = 18580
246626 XDOT = 5623
585768
YDOT = 14942
596690 feet/sec YDOT = 4617
611696 meter/sec
ZDOT = -7886
367487 ZDOT = -2376
349492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1325849
71 X = -404118
99
Y = -15394762
75 feet Y = -4692323
69 meter
Z = -16063582
45 Z = -4896179
93
XDOT = 21970
998434 XDOT = 6696
760323
YDOT = 6177
260875 feet/sec YDOT = 1882
829115 meter/sec
ZDOT = -7772
622068 ZDOT = -2369
095206
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 13106
52029837
00016717 00000-0 10270-3 0 9082
2 25544 51
6444 54
3573 0010052 148
4368 211
7389 15
52278117 25136
Satellite: ISS
Catalog Number: 25544
Epoch time: 13106
52029837 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 54
3573 deg
Eccentricity:
0010052
Arg of perigee: 148
4368 deg
Mean anomaly: 211
7389 deg
Mean motion: 15
52278117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2513
Checksum: 302
Coasting Arc #10 (Orbit 2528)
---------------------------------------
Vector Time (GMT): 2013/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2171019
75 A = 6783053
16 meter
Y = 3739280
27 meter E =
0013653
Z = 5221457
34 I = 51
89507
XDOT = -5665
328372 Wp = 144
47187
YDOT = -5022
294961 meter/sec RA = 48
86866 deg
ZDOT = 1228
634918 TA = 293
71063
MA = 293
85382
Ha = 226
877 n
mi
Hp = 215
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7122768
21 X = -2238036
42
Y = 12267979
90 feet Y = 3714628
05 meter
Z = 17130765
56 Z = 5210747
73
XDOT = -18587
035342 XDOT = -5614
715347
YDOT = -16477
345672 feet/sec YDOT = -5085
365193 meter/sec
ZDOT = 4030
954456 ZDOT = 1201
236209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1373952
96 X = -418780
86
Y = 14173751
02 feet Y = 4320159
31 meter
Z = 17085588
13 Z = 5207687
26
XDOT = -22793
740153 XDOT = -6947
531999
YDOT = -6981
000509 feet/sec YDOT = -2127
808955 meter/sec
ZDOT = 3917
346620 ZDOT = 1194
007250
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 13107
55034912
00016717 00000-0 10270-3 0 9097
2 25544 51
6448 49
2377 0009994 153
1560 207
0111 15
52333357 25291
Satellite: ISS
Catalog Number: 25544
Epoch time: 13107
55034912 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 49
2377 deg
Eccentricity:
0009994
Arg of perigee: 153
1560 deg
Mean anomaly: 207
0111 deg
Mean motion: 15
52333357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2529
Checksum: 302
Coasting Arc #11 (Orbit 2543)
---------------------------------------
Vector Time (GMT): 2013/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2945174
99 A = 6782636
92 meter
Y = -2988451
16 meter E =
0021041
Z = -5345490
56 I = 51
87263
XDOT = 5491
851284 Wp = 115
79972
YDOT = 5327
565952 meter/sec RA = 43
90323 deg
ZDOT = 38
594954 TA = 154
61945
MA = 154
51595
Ha = 226
783 n
mi
Hp = 215
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9662647
62 X = 3004340
69
Y = -9804629
79 feet Y = -2955185
78 meter
Z = -17537698
70 Z = -5331039
25
XDOT = 18017
884791 XDOT = 5431
681646
YDOT = 17478
890919 feet/sec YDOT = 5388
642868 meter/sec
ZDOT = 126
623866 ZDOT = 65
127621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4493938
67 X = 1369752
51
Y = -13093011
22 feet Y = -3990749
82 meter
Z = -17477012
69 Z = -5326993
47
XDOT = 22894
457205 XDOT = 6978
230556
YDOT = 7503
696917 feet/sec YDOT = 2287
126820 meter/sec
ZDOT = 236
572058 ZDOT = 72
107163
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 13108
51600914
00016717 00000-0 10270-3 0 9107
2 25544 51
6449 44
4359 0009965 156
1755 203
9859 15
52318583 25441
Satellite: ISS
Catalog Number: 25544
Epoch time: 13108
51600914 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 44
4359 deg
Eccentricity:
0009965
Arg of perigee: 156
1755 deg
Mean anomaly: 203
9859 deg
Mean motion: 15
52318583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2544
Checksum: 322
Coasting Arc #12 (Orbit 2559)
---------------------------------------
Vector Time (GMT): 2013/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3696400
72 A = 6783067
52 meter
Y = 2271280
45 meter E =
0009764
Z = 5206902
85 I = 51
85198
XDOT = -5191
444535 Wp = 134
47178
YDOT = -5499
223903 meter/sec RA = 38
93849 deg
ZDOT = -1291
816988 TA = 327
86168
MA = 327
92117
Ha = 226
703 n
mi
Hp = 215
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12127298
96 X = -3746817
79
Y = 7451707
50 feet Y = 2229663
36 meter
Z = 17083014
61 Z = 5188823
40
XDOT = -17032
298344 XDOT = -5123
289865
YDOT = -18042
073174 feet/sec YDOT = -5556
896905 meter/sec
ZDOT = -4238
244711 ZDOT = -1316
870827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7528710
36 X = -2294750
92
Y = 12186026
66 feet Y = 3714300
93 meter
Z = 17007292
18 Z = 5183822
66
XDOT = -22445
804620 XDOT = -6841
481248
YDOT = -7831
335575 feet/sec YDOT = -2386
991083 meter/sec
ZDOT = -4341
994663 ZDOT = -1323
439973
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 13109
54602915
00016717 00000-0 10270-3 0 9115
2 25544 51
6451 39
3159 0009925 160
1165 200
0376 15
52360623 25603
Satellite: ISS
Catalog Number: 25544
Epoch time: 13109
54602915 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 39
3159 deg
Eccentricity:
0009925
Arg of perigee: 160
1165 deg
Mean anomaly: 200
0376 deg
Mean motion: 15
52360623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2560
Checksum: 282
Coasting Arc #13 (Orbit 2574)
---------------------------------------
Vector Time (GMT): 2013/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4482605
17 A = 6784613
84 meter
Y = -1583431
75 meter E =
0018977
Z = -4857546
04 I = 51
83312
XDOT = 4669
820206 Wp = 133
14850
YDOT = 5519
401888 meter/sec RA = 33
97171 deg
ZDOT = 2503
726146 TA = 161
48214
MA = 161
41298
Ha = 226
494 n
mi
Hp = 215
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14706709
87 X = 4523575
06
Y = -5194986
07 feet Y = -1533075
69 meter
Z = -15936830
83 Z = -4835670
20
XDOT = 15320
932435 XDOT = 4595
591503
YDOT = 18108
273911 feet/sec YDOT = 5571
207896 meter/sec
ZDOT = 8214
324625 ZDOT = 2526
231164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10647644
85 X = 3245402
15
Y = -11524309
10 feet Y = -3512609
41 meter
Z = -15845369
40 Z = -4829668
59
XDOT = 21132
131802 XDOT = 6441
073773
YDOT = 8072
944422 feet/sec YDOT = 2460
633460 meter/sec
ZDOT = 8307
433448 ZDOT = 2532
105715
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 13110
51165865
00016717 00000-0 10270-3 0 9123
2 25544 51
6455 34
5140 0009912 163
5807 196
5667 15
52370998 25754
Satellite: ISS
Catalog Number: 25544
Epoch time: 13110
51165865 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 34
5140 deg
Eccentricity:
0009912
Arg of perigee: 163
5807 deg
Mean anomaly: 196
5667 deg
Mean motion: 15
52370998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2575
Checksum: 321
Coasting Arc #14 (Orbit 2590)
---------------------------------------
Vector Time (GMT): 2013/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5179922
15 A = 6786793
25 meter
Y = 962073
90 meter E =
0013739
Z = 4263548
53 I = 51
81473
XDOT = -3992
939014 Wp = 119
83791
YDOT = -5465
805512 meter/sec RA = 29
00821 deg
ZDOT = -3615
745621 TA = 7
00067
MA = 6
98151
Ha = 226
501 n
mi
Hp = 215
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16994495
24 X = -5211006
61
Y = 3156410
42 feet Y = 903975
28 meter
Z = 13988020
12 Z = 4238309
16
XDOT = -13100
193615 XDOT = -3913
957982
YDOT = -17932
432782 feet/sec YDOT = -5510
015754 meter/sec
ZDOT = -11862
682482 ZDOT = -3634
950834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13425538
57 X = -4092104
16
Y = 11021265
73 feet Y = 3359281
79 meter
Z = 13882619
28 Z = 4231422
36
XDOT = -19269
235014 XDOT = -5873
262832
YDOT = -8421
865121 feet/sec YDOT = -2566
984489 meter/sec
ZDOT = -11942
027798 ZDOT = -3639
930073
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 13111
54164796
00016717 00000-0 10270-3 0 9130
2 25544 51
6456 29
3935 0009935 167
3356 192
8047 15
52388378 25915
Satellite: ISS
Catalog Number: 25544
Epoch time: 13111
54164796 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 29
3935 deg
Eccentricity:
0009935
Arg of perigee: 167
3356 deg
Mean anomaly: 192
8047 deg
Mean motion: 15
52388378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2591
Checksum: 339
Coasting Arc #15 (Orbit 2605)
---------------------------------------
Vector Time (GMT): 2013/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5817564
08 A = 6789231
35 meter
Y = -412872
31 meter E =
0011852
Z = -3491072
65 I = 51
79680
XDOT = 3109
308211 Wp = 146
48046
YDOT = 5309
573456 meter/sec RA = 24
04593 deg
ZDOT = 4551
205095 TA = 172
70692
MA = 172
68966
Ha = 226
190 n
mi
Hp = 215
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19086496
32 X = 5838707
41
Y = -1354567
95 feet Y = -347698
72 meter
Z = -11453650
42 Z = -3462759
73
XDOT = 10201
142426 XDOT = 3027
595548
YDOT = 17419
860420 feet/sec YDOT = 5343
887210 meter/sec
ZDOT = 14931
775246 ZDOT = 4566
111075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15932172
24 X = 4856126
10
Y = -10723214
87 feet Y = -3268435
89 meter
Z = -11335512
99 Z = -3455064
36
XDOT = 16664
674381 XDOT = 5079
392751
YDOT = 8902
597228 feet/sec YDOT = 2713
511635 meter/sec
ZDOT = 14993
203288 ZDOT = 4569
928362
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 13112
50724749
00016717 00000-0 10270-3 0 9148
2 25544 51
6465 24
5919 0009906 171
1474 188
9854 15
52429950 26067
Satellite: ISS
Catalog Number: 25544
Epoch time: 13112
50724749 = yrday
fracday
Element set: 914
Inclination: 51
6465 deg
RA of node: 24
5919 deg
Eccentricity:
0009906
Arg of perigee: 171
1474 deg
Mean anomaly: 188
9854 deg
Mean motion: 15
52429950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2606
Checksum: 329
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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