[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 26th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 ET - UTC (sec) : 66 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
147/00:13:08
846 -2
6 3
0 3
1
N/A -0
2 -0
5 220
3
000/00:06:17
693 -1
7 -0
1 211
2
Coasting Arc #1 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2012/146/17:31:48
695
Vector Time (MET): N/A
Weight (LBS) : 941309
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3645319
34 A = 6770640
72 meter
Y = -2168375
70 meter E =
0012688
Z = 5275972
36 I = 51
33336
XDOT = 4303
485948 Wp = 11
03456
YDOT = 6344
031306 meter/sec RA = 233
73317 deg
ZDOT = -353
681188 TA = 82
42143
MA = 82
27733
Ha = 220
125 n
mi
Hp = 209
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11959709
13 X = 3643666
06
Y = -7114093
51 feet Y = -2127621
28 meter
Z = 17309620
60 Z = 5293676
98
XDOT = 14119
048385 XDOT = 4233
943960
YDOT = 20813
751004 feet/sec YDOT = 6391
766755 meter/sec
ZDOT = -1160
371353 ZDOT = -332
943230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13803065
63 X = -4207174
40
Y = -767328
73 feet Y = -233881
80 meter
Z = 17382592
45 Z = 5298214
18
XDOT = -63
136157 XDOT = -19
243901
YDOT = -24147
969623 feet/sec YDOT = -7360
301141 meter/sec
ZDOT = -1075
659486 ZDOT = -327
861011
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 12146
77805499
00016717 00000-0 10270-3 0 9000
2 25544 51
6372 234
4588 0011797 359
6659
4485 15
56447352 14523
Satellite: ISS
Catalog Number: 25544
Epoch time: 12146
77805499 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 234
4588 deg
Eccentricity:
0011797
Arg of perigee: 359
6659 deg
Mean anomaly:
4485 deg
Mean motion: 15
56447352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 337
Coasting Arc #2 (Orbit 1455)
---------------------------------------
Vector Time (GMT): 2012/147/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 260387
22 A = 6777593
76 meter
Y = 5509909
75 meter E =
0012951
Z = -3951763
77 I = 51
35804
XDOT = -6012
479872 Wp = 22
86734
YDOT = -2578
673304 meter/sec RA = 232
35123 deg
ZDOT = -3984
291763 TA = 205
34559
MA = 205
40917
Ha = 220
293 n
mi
Hp = 211
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 854288
77 X = 217951
76
Y = 18077131
74 feet Y = 5512584
69 meter
Z = -12965104
25 Z = -3950601
35
XDOT = -19725
983831 XDOT = -5963
842912
YDOT = -8460
214252 feet/sec YDOT = -2645
636231 meter/sec
ZDOT = -13071
823368 ZDOT = -4013
382329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17030896
91 X = -5191017
38
Y = -6129661
37 feet Y = -1868320
79 meter
Z = -12960795
94 Z = -3950450
60
XDOT = 14953
113499 XDOT = 4557
708994
YDOT = -13603
676059 feet/sec YDOT = -4146
400463 meter/sec
ZDOT = -13191
201087 ZDOT = -4020
678091
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 12147
03488670
00016717 00000-0 10270-3 0 9019
2 25544 51
6390 233
1744 0010125 351
9262 8
1727 15
55892152 14561
Satellite: ISS
Catalog Number: 25544
Epoch time: 12147
03488670 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 233
1744 deg
Eccentricity:
0010125
Arg of perigee: 351
9262 deg
Mean anomaly: 8
1727 deg
Mean motion: 15
55892152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1456
Checksum: 294
Coasting Arc #3 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2012/148/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1658914
51 A = 6773155
19 meter
Y = -4173590
26 meter E =
0007909
Z = 5065023
44 I = 51
36252
XDOT = 5996
784486 Wp = 27
19641
YDOT = 4469
707990 meter/sec RA = 227
32177 deg
ZDOT = 1724
805178 TA = 46
11691
MA = 46
05162
Ha = 220
297 n
mi
Hp = 211
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5442632
92 X = 1680856
36
Y = -13692881
44 feet Y = -4154917
00 meter
Z = 16617530
97 Z = 5073135
33
XDOT = 19674
489782 XDOT = 5937
978870
YDOT = 14664
396292 feet/sec YDOT = 4536
438798 meter/sec
ZDOT = 5658
809639 ZDOT = 1753
794900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10735332
67 X = 3272129
40
Y = 10037360
01 feet Y = 3059387
33 meter
Z = 16651235
00 Z = 5075296
43
XDOT = -20169
660243 XDOT = -6147
712442
YDOT = 12019
295264 feet/sec YDOT = 3663
481197 meter/sec
ZDOT = 5777
628458 ZDOT = 1761
021154
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 12148
06255014
00016717 00000-0 10270-3 0 9028
2 25544 51
6386 228
0366 0010117 355
7711 4
3355 15
55919289 14725
Satellite: ISS
Catalog Number: 25544
Epoch time: 12148
06255014 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 228
0366 deg
Eccentricity:
0010117
Arg of perigee: 355
7711 deg
Mean anomaly: 4
3355 deg
Mean motion: 15
55919289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 297
Coasting Arc #4 (Orbit 1486)
---------------------------------------
Vector Time (GMT): 2012/149/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3533682
83 A = 6772263
02 meter
Y = 2448604
25 meter E =
0016670
Z = -5244019
65 I = 51
38159
XDOT = -5147
616064 Wp = 59
17422
YDOT = -5609
679050 meter/sec RA = 222
28389 deg
ZDOT = 859
791538 TA = 219
02311
MA = 219
14350
Ha = 220
419 n
mi
Hp = 210
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11593447
61 X = -3535326
64
Y = 8033478
51 feet Y = 2409079
60 meter
Z = -17204788
88 Z = -5261190
00
XDOT = -16888
504148 XDOT = -5088
681593
YDOT = -18404
458827 feet/sec YDOT = -5666
913420 meter/sec
ZDOT = 2820
838379 ZDOT = 834
927315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3434311
65 X = -1046778
19
Y = -13590763
60 feet Y = -4142464
75 meter
Z = -17275595
88 Z = -5265601
63
XDOT = 22213
522803 XDOT = 6770
681750
YDOT = -9026
263540 feet/sec YDOT = -2751
205127 meter/sec
ZDOT = 2719
062162 ZDOT = 828
770147
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 12149
02596593
00016717 00000-0 10270-3 0 9036
2 25544 51
6389 223
2202 0010238 359
0227 1
0904 15
55956077 14873
Satellite: ISS
Catalog Number: 25544
Epoch time: 12149
02596593 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 223
2202 deg
Eccentricity:
0010238
Arg of perigee: 359
0227 deg
Mean anomaly: 1
0904 deg
Mean motion: 15
55956077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1487
Checksum: 303
Coasting Arc #5 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2012/150/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5119383
94 A = 6775504
64 meter
Y = -524272
08 meter E =
0016349
Z = 4407206
72 I = 51
41621
XDOT = 3483
963421 Wp = 33
98530
YDOT = 5974
152955 meter/sec RA = 217
25202 deg
ZDOT = -3316
999781 TA = 89
69711
MA = 89
50977
Ha = 220
461 n
mi
Hp = 210
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16795879
08 X = 5103456
63
Y = -1720052
77 feet Y = -467113
29 meter
Z = 14459339
64 Z = 4432037
89
XDOT = 11430
326186 XDOT = 3433
013623
YDOT = 19600
239354 feet/sec YDOT = 6012
828117 meter/sec
ZDOT = -10882
545214 ZDOT = -3300
198131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4039997
58 X = -1231391
26
Y = 16302573
33 feet Y = 4969024
35 meter
Z = 14561495
82 Z = 4438343
93
XDOT = -21145
816293 XDOT = -6445
244806
YDOT = 4474
914507 feet/sec YDOT = 1363
953942 meter/sec
ZDOT = -10813
940911 ZDOT = -3296
089190
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 12150
05358922
00016717 00000-0 10270-3 0 9044
2 25544 51
6389 218
0823 0010376 2
4832 357
6371 15
56007164 15030
Satellite: ISS
Catalog Number: 25544
Epoch time: 12150
05358922 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 218
0823 deg
Eccentricity:
0010376
Arg of perigee: 2
4832 deg
Mean anomaly: 357
6371 deg
Mean motion: 15
56007164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 288
Coasting Arc #6 (Orbit 1517)
---------------------------------------
Vector Time (GMT): 2012/151/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6065851
79 A = 6780579
27 meter
Y = -1230329
08 meter E =
0013711
Z = -2755568
96 I = 51
45808
XDOT = -1188
895755 Wp = 22
30705
YDOT = -5581
359065 meter/sec RA = 212
23880 deg
ZDOT = 5129
949517 TA = 306
36043
MA = 306
48688
Ha = 220
555 n
mi
Hp = 210
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19901088
55 X = -6038257
10
Y = -4036512
73 feet Y = -1298006
74 meter
Z = -9040580
59 Z = -2784969
94
XDOT = -3900
576623 XDOT = -1151
315883
YDOT = -18311
545489 feet/sec YDOT = -5594
444210 meter/sec
ZDOT = 16830
543036 ZDOT = 5124
264816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10219570
16 X = 3114924
98
Y = -17484509
70 feet Y = -5329278
56 meter
Z = -9161395
33 Z = -2792393
30
XDOT = 17348
385770 XDOT = 5287
787983
YDOT = 1368
593707 feet/sec YDOT = 417
147362 meter/sec
ZDOT = 16807
617561 ZDOT = 5122
961833
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 12151
01696899
00016717 00000-0 10270-3 0 9050
2 25544 51
6390 213
2654 0010397 5
7081 354
4190 15
55997871 15188
Satellite: ISS
Catalog Number: 25544
Epoch time: 12151
01696899 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 213
2654 deg
Eccentricity:
0010397
Arg of perigee: 5
7081 deg
Mean anomaly: 354
4190 deg
Mean motion: 15
55997871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1518
Checksum: 322
Coasting Arc #7 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2012/152/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6192699
12 A = 6783764
33 meter
Y = 2720593
54 meter E =
0012065
Z = 523102
35 I = 51
49484
XDOT = -1494
080648 Wp = 81
52555
YDOT = 4571
462471 meter/sec RA = 207
24449 deg
ZDOT = -5968
306450 TA = 92
81980
MA = 92
68171
Ha = 220
725 n
mi
Hp = 210
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20317254
32 X = 6159275
48
Y = 8925831
84 feet Y = 2789657
22 meter
Z = 1716215
07 Z = 553105
62
XDOT = -4901
839395 XDOT = -1516
095535
YDOT = 14998
236454 feet/sec YDOT = 4554
632034 meter/sec
ZDOT = -19581
057908 ZDOT = -5975
617906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14712582
08 X = -4484395
02
Y = 16600097
69 feet Y = 5059709
78 meter
Z = 1839395
72 Z = 560647
81
XDOT = -11603
119434 XDOT = -3536
630803
YDOT = -8070
074532 feet/sec YDOT = -2459
758717 meter/sec
ZDOT = -19611
500046 ZDOT = -5977
585214
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 12152
04455536
00016717 00000-0 10270-3 0 9066
2 25544 51
6389 208
1276 0010230 10
1015 350
0343 15
55996950 15349
Satellite: ISS
Catalog Number: 25544
Epoch time: 12152
04455536 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 208
1276 deg
Eccentricity:
0010230
Arg of perigee: 10
1015 deg
Mean anomaly: 350
0343 deg
Mean motion: 15
55996950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 279
Coasting Arc #8 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2012/153/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5364744
85 A = 6782405
51 meter
Y = -3723980
72 meter E =
0021950
Z = 1779801
38 I = 51
51782
XDOT = 4098
527904 Wp = 43
32018
YDOT = -3185
989463 meter/sec RA = 202
25474 deg
ZDOT = 5661
993349 TA = 336
30711
MA = 336
40803
Ha = 220
765 n
mi
Hp = 209
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17600868
95 X = -5331349
84
Y = -12217784
52 feet Y = -3783786
05 meter
Z = 5839243
38 Z = 1753820
04
XDOT = 13446
613857 XDOT = 4106
344510
YDOT = -10452
721335 feet/sec YDOT = -3140
113958 meter/sec
ZDOT = 18576
093665 ZDOT = 5681
922881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16801829
27 X = 5121197
56
Y = -13341534
75 feet Y = -4066499
79 meter
Z = 5732677
68 Z = 1747320
16
XDOT = 5168
869478 XDOT = 1575
471417
YDOT = 14563
639859 feet/sec YDOT = 4438
997429 meter/sec
ZDOT = 18658
328859 ZDOT = 5687
058636
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 12153
07211930
00016717 00000-0 10270-3 0 9079
2 25544 51
6384 202
9890 0010423 12
9232 347
2186 15
56068613 15501
Satellite: ISS
Catalog Number: 25544
Epoch time: 12153
07211930 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 202
9890 deg
Eccentricity:
0010423
Arg of perigee: 12
9232 deg
Mean anomaly: 347
2186 deg
Mean motion: 15
56068613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 284
Coasting Arc #9 (Orbit 1564)
---------------------------------------
Vector Time (GMT): 2012/154/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3667038
22 A = 6777691
77 meter
Y = 4282835
92 meter E =
0014165
Z = -3778410
81 I = 51
52960
XDOT = -6194
567211 Wp = 37
89507
YDOT = 1583
014963 meter/sec RA = 197
25561 deg
ZDOT = -4215
103864 TA = 187
42466
MA = 187
44566
Ha = 220
810 n
mi
Hp = 209
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12030965
27 X = 3637229
13
Y = 14051298
95 feet Y = 4323676
76 meter
Z = -12396360
93 Z = -3760668
10
XDOT = -20323
383239 XDOT = -6191
332003
YDOT = 5193
618646 feet/sec YDOT = 1513
762038 meter/sec
ZDOT = -13829
080920 ZDOT = -4245
189326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16822870
88 X = -5127611
04
Y = 7808312
54 feet Y = 2379973
66 meter
Z = -12323723
57 Z = -3756270
95
XDOT = 1101
937742 XDOT = 335
870624
YDOT = -19660
764271 feet/sec YDOT = -5992
600950 meter/sec
ZDOT = -13952
974211 ZDOT = -4252
866539
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 12154
03544418
00016717 00000-0 10270-3 0 9087
2 25544 51
6373 198
1721 0010376 16
1275 344
0207 15
56076904 15655
Satellite: ISS
Catalog Number: 25544
Epoch time: 12154
03544418 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 198
1721 deg
Eccentricity:
0010376
Arg of perigee: 16
1275 deg
Mean anomaly: 344
0207 deg
Mean motion: 15
56076904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1565
Checksum: 296
Coasting Arc #10 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2012/155/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1300618
03 A = 6772948
83 meter
Y = -4355212
80 meter E =
0010787
Z = 5011917
26 I = 51
54291
XDOT = 7427
061996 Wp = 52
99080
YDOT = 24
521103 meter/sec RA = 192
23833 deg
ZDOT = 1952
136422 TA = 18
08551
MA = 18
04717
Ha = 220
952 n
mi
Hp = 209
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4267119
52 X = -1276167
66
Y = -14288755
90 feet Y = -4369621
11 meter
Z = 16443298
09 Z = 5005657
58
XDOT = 24367
001299 XDOT = 7416
752594
YDOT = 80
449814 feet/sec YDOT = 107
517188 meter/sec
ZDOT = 6404
647053 ZDOT = 1988
192343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14929921
59 X = 4550640
10
Y = -555648
58 feet Y = -169361
69 meter
Z = 16417904
92 Z = 5004177
42
XDOT = -6359
749723 XDOT = -1938
451715
YDOT = 22403
895722 feet/sec YDOT = 6828
707416 meter/sec
ZDOT = 6552
988589 ZDOT = 1997
350922
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 12155
06297231
00016717 00000-0 10270-3 0 9090
2 25544 51
6369 193
0332 0010495 20
6737 339
4840 15
56090826 15815
Satellite: ISS
Catalog Number: 25544
Epoch time: 12155
06297231 = yrday
fracday
Element set: 909
Inclination: 51
6369 deg
RA of node: 193
0332 deg
Eccentricity:
0010495
Arg of perigee: 20
6737 deg
Mean anomaly: 339
4840 deg
Mean motion: 15
56090826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 309
Coasting Arc #11 (Orbit 1595)
---------------------------------------
Vector Time (GMT): 2012/156/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1311887
38 A = 6771603
02 meter
Y = 4055205
93 meter E =
0020541
Z = -5277513
75 I = 51
56739
XDOT = -7474
692802 Wp = 66
76779
YDOT = -1511
162156 meter/sec RA = 187
21052 deg
ZDOT = 707
007283 TA = 209
94129
MA = 210
05893
Ha = 220
881 n
mi
Hp = 209
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4304092
45 X = -1331498
72
Y = 13304481
40 feet Y = 4040426
81 meter
Z = -17314677
67 Z = -5283933
89
XDOT = -24523
270347 XDOT = -7460
673663
YDOT = -4957
881089 feet/sec YDOT = -1594
670526 meter/sec
ZDOT = 2319
577699 ZDOT = 670
728894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11907808
74 X = -3629500
10
Y = -7267133
84 feet Y = -2215022
39 meter
Z = -17341434
68 Z = -5285669
29
XDOT = 10168
982960 XDOT = 3099
506006
YDOT = -21762
939042 feet/sec YDOT = -6633
343820 meter/sec
ZDOT = 2170
422542 ZDOT = 661
544791
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 12156
02625968
00016717 00000-0 10270-3 0 9101
2 25544 51
6352 188
2149 0010434 23
8168 336
3466 15
56156895 15960
Satellite: ISS
Catalog Number: 25544
Epoch time: 12156
02625968 = yrday
fracday
Element set: 910
Inclination: 51
6352 deg
RA of node: 188
2149 deg
Eccentricity:
0010434
Arg of perigee: 23
8168 deg
Mean anomaly: 336
3466 deg
Mean motion: 15
56156895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1596
Checksum: 325
Coasting Arc #12 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2012/157/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3812834
25 A = 6774796
83 meter
Y = -3386886
55 meter E =
0018151
Z = 4455303
28 I = 51
60907
XDOT = 6345
263876 Wp = 46
51727
YDOT = 2827
611897 meter/sec RA = 182
18949 deg
ZDOT = -3260
158531 TA = 76
40632
MA = 76
20421
Ha = 220
810 n
mi
Hp = 208
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12509298
71 X = 3828780
72
Y = -11111832
53 feet Y = -3344160
71 meter
Z = 14617136
76 Z = 4473864
13
XDOT = 20817
794868 XDOT = 6329
010562
YDOT = 9276
941920 feet/sec YDOT = 2898
478260 meter/sec
ZDOT = -10696
058171 ZDOT = -3229
372294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8059266
75 X = 2456464
51
Y = 14586166
15 feet Y = 4445863
44 meter
Z = 14693809
57 Z = 4478673
16
XDOT = -12638
576780 XDOT = -3852
238202
YDOT = 17698
392535 feet/sec YDOT = 5394
470045 meter/sec
ZDOT = -10569
593084 ZDOT = -3221
611972
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 12157
05374745
00016717 00000-0 10270-3 0 9110
2 25544 51
6354 183
0760 0010384 26
9129 333
2561 15
56194860 16124
Satellite: ISS
Catalog Number: 25544
Epoch time: 12157
05374745 = yrday
fracday
Element set: 911
Inclination: 51
6354 deg
RA of node: 183
0760 deg
Eccentricity:
0010384
Arg of perigee: 26
9129 deg
Mean anomaly: 333
2561 deg
Mean motion: 15
56194860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 298
Coasting Arc #13 (Orbit 1626)
---------------------------------------
Vector Time (GMT): 2012/158/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5668178
56 A = 6779945
41 meter
Y = 2473332
61 meter E =
0014638
Z = -2771381
73 I = 51
65552
XDOT = -4185
322661 Wp = 40
69521
YDOT = -3863
577719 meter/sec RA = 177
18722 deg
ZDOT = 5138
098679 TA = 287
87732
MA = 288
03690
Ha = 220
874 n
mi
Hp = 208
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18596386
35 X = -5681951
84
Y = 8114608
30 feet Y = 2409871
00 meter
Z = -9092459
74 Z = -2798950
53
XDOT = -13731
373561 XDOT = -4166
768019
YDOT = -12675
779917 feet/sec YDOT = -3910
277732 meter/sec
ZDOT = 16857
279132 ZDOT = 5117
810952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4113636
95 X = -1253836
54
Y = -19815905
58 feet Y = -6039888
02 meter
Z = -9206147
63 Z = -2806033
80
XDOT = 13811
478752 XDOT = 4209
738724
YDOT = -10620
812209 feet/sec YDOT = -3237
223561 meter/sec
ZDOT = 16774
095036 ZDOT = 5112
744167
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 12158
01700074
00016717 00000-0 10270-3 0 9126
2 25544 51
6340 178
2572 0010345 31
2326 328
9440 15
56204928 16271
Satellite: ISS
Catalog Number: 25544
Epoch time: 12158
01700074 = yrday
fracday
Element set: 912
Inclination: 51
6340 deg
RA of node: 178
2572 deg
Eccentricity:
0010345
Arg of perigee: 31
2326 deg
Mean anomaly: 328
9440 deg
Mean motion: 15
56204928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1627
Checksum: 281
Coasting Arc #14 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2012/159/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6645227
65 A = 6782993
25 meter
Y = -1276085
02 meter E =
0015926
Z = 459694
61 I = 51
69698
XDOT = 1310
034721 Wp = 88
95915
YDOT = 4598
359983 meter/sec RA = 172
20565 deg
ZDOT = -5993
052667 TA = 86
08598
MA = 85
90392
Ha = 220
960 n
mi
Hp = 208
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21801927
99 X = 6656770
12
Y = -4186630
63 feet Y = -1201709
50 meter
Z = 1508184
43 Z = 492004
55
XDOT = 4298
014177 XDOT = 1287
630342
YDOT = 15086
482885 feet/sec YDOT = 4612
885286 meter/sec
ZDOT = -19662
246283 ZDOT = -5986
742287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18595
44 X = -5667
89
Y = 22190816
21 feet Y = 6763760
78 meter
Z = 1641307
59 Z = 500270
55
XDOT = -14030
851619 XDOT = -4276
603573
YDOT = 1480
704849 feet/sec YDOT = 451
318838 meter/sec
ZDOT = -19636
653510 ZDOT = -5985
251990
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 12159
04444962
00016717 00000-0 10270-3 0 9132
2 25544 51
6344 173
1180 0010515 34
4265 325
7568 15
56272647 16437
Satellite: ISS
Catalog Number: 25544
Epoch time: 12159
04444962 = yrday
fracday
Element set: 913
Inclination: 51
6344 deg
RA of node: 173
1180 deg
Eccentricity:
0010515
Arg of perigee: 34
4265 deg
Mean anomaly: 325
7568 deg
Mean motion: 15
56272647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 303
Coasting Arc #15 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2012/160/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6496107
91 A = 6781666
23 meter
Y = -64513
85 meter E =
0023620
Z = 1899518
19 I = 51
72153
XDOT = 1705
606967 Wp = 55
35037
YDOT = -4941
134195 meter/sec RA = 167
22831 deg
ZDOT = 5628
681631 TA = 325
59659
MA = 325
74929
Ha = 221
031 n
mi
Hp = 208
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21312689
99 X = -6504131
07
Y = -211659
62 feet Y = -137202
47 meter
Z = 6232015
06 Z = 1867941
07
XDOT = 5595
823381 XDOT = 1733
390266
YDOT = -16211
070195 feet/sec YDOT = -4921
906477 meter/sec
ZDOT = 18466
803252 ZDOT = 5637
034148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3892416
89 X = 1186408
67
Y = -20993527
79 feet Y = -6398827
27 meter
Z = 6102003
62 Z = 1859890
70
XDOT = 13489
629674 XDOT = 4111
639125
YDOT = 7914
323334 feet/sec YDOT = 2412
285752 meter/sec
ZDOT = 18501
608233 ZDOT = 5639
290189
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 12160
07188023
00016717 00000-0 10270-3 0 9141
2 25544 51
6336 167
9777 0010314 39
4211 320
7691 15
56263970 16592
Satellite: ISS
Catalog Number: 25544
Epoch time: 12160
07188023 = yrday
fracday
Element set: 914
Inclination: 51
6336 deg
RA of node: 167
9777 deg
Eccentricity:
0010314
Arg of perigee: 39
4211 deg
Mean anomaly: 320
7691 deg
Mean motion: 15
56263970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1659
Checksum: 307
Coasting Arc #16 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2012/161/00:16:17
693
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5315376
46 A = 6776574
02 meter
Y = 1549537
86 meter E =
0016325
Z = -3926350
33 I = 51
73470
XDOT = -4393
177591 Wp = 55
51400
YDOT = 4774
705025 meter/sec RA = 162
24072 deg
ZDOT = -4066
045451 TA = 171
94184
MA = 171
91559
Ha = 221
038 n
mi
Hp = 208
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17438899
14 X = 5316727
37
Y = 5083785
63 feet Y = 1608985
70 meter
Z = -12881726
80 Z = -3900525
15
XDOT = -14413
312306 XDOT = -4426
490985
YDOT = 15665
042734 feet/sec YDOT = 4725
392004 meter/sec
ZDOT = -13340
044130 ZDOT = -4087
467553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7746660
27 X = -2361182
05
Y = 16512860
28 feet Y = 5033119
81 meter
Z = -12775510
36 Z = -3893975
56
XDOT = -12039
300947 XDOT = -3669
578929
YDOT = -16029
573825 feet/sec YDOT = -4885
814102 meter/sec
ZDOT = -13428
658217 ZDOT = -4093
055024
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 12161
03507709
00016717 00000-0 10270-3 0 9155
2 25544 51
6339 163
1595 0010454 43
4735 316
7242 15
56308219 16742
Satellite: ISS
Catalog Number: 25544
Epoch time: 12161
03507709 = yrday
fracday
Element set: 915
Inclination: 51
6339 deg
RA of node: 163
1595 deg
Eccentricity:
0010454
Arg of perigee: 43
4735 deg
Mean anomaly: 316
7242 deg
Mean motion: 15
56308219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1674
Checksum: 301
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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