[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 11th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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
145/00:25:23
357 -2
4 3
4 3
4
N/A -0
4 -0
1 220
3
000/00:06:46
715 -2
3 -0
1 212
2
Coasting Arc #1 (Orbit 1198)
---------------------------------------
Vector Time (GMT): 2012/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5061185
31 A = 6783773
80 meter
Y = 4489105
24 meter E =
0004223
Z = -468523
31 I = 51
41319
XDOT = -2870
460767 Wp = 218
56500
YDOT = -3862
074772 meter/sec RA = 315
26028 deg
ZDOT = -5970
275247 TA = 326
50587
MA = 326
53256
Ha = 217
780 n
mi
Hp = 213
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16604938
69 X = -5108731
24
Y = 14728035
58 feet Y = 4432242
14 meter
Z = -1537149
96 Z = -493225
60
XDOT = -9417
522203 XDOT = -2798
058449
YDOT = -12670
848988 feet/sec YDOT = -3893
768687 meter/sec
ZDOT = -19587
517214 ZDOT = -5984
044402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -584343
32 X = -178107
84
Y = 22180482
16 feet Y = 6760610
96 meter
Z = -1639086
55 Z = -499593
58
XDOT = -13988
478695 XDOT = -4263
688306
YDOT = -1826
027960 feet/sec YDOT = -556
573322 meter/sec
ZDOT = -19643
698403 ZDOT = -5987
399273
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 12130
53114689
00016717 00000-0 10270-3 0 9001
2 25544 51
6370 315
7001 0011143 296
6926 63
3086 15
56003876 11998
Satellite: ISS
Catalog Number: 25544
Epoch time: 12130
53114689 = yrday
fracday
Element set: 900
Inclination: 51
6370 deg
RA of node: 315
7001 deg
Eccentricity:
0011143
Arg of perigee: 296
6926 deg
Mean anomaly: 63
3086 deg
Mean motion: 15
56003876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1199
Checksum: 293
Coasting Arc #2 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2012/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5409254
84 A = 6780766
41 meter
Y = -3075559
07 meter E =
0008800
Z = 2679428
01 I = 51
38158
XDOT = 642
436205 Wp = 23
85633
YDOT = 5633
279773 meter/sec RA = 310
25938 deg
ZDOT = 5171
103973 TA = 6
55410
MA = 6
54260
Ha = 217
818 n
mi
Hp = 213
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17746899
09 X = 5430228
23
Y = -10090416
91 feet Y = -3014952
38 meter
Z = 8790774
31 Z = 2705756
74
XDOT = 2107
730330 XDOT = 554
275819
YDOT = 18481
889020 feet/sec YDOT = 5639
970564 meter/sec
ZDOT = 16965
564216 ZDOT = 5174
011203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4379565
14 X = 1334891
45
Y = -19891440
12 feet Y = -6062910
95 meter
Z = 8899251
25 Z = 2712491
78
XDOT = 13604
946746 XDOT = 4146
787768
YDOT = 10587
957701 feet/sec YDOT = 3227
209507 meter/sec
ZDOT = 16976
948950 ZDOT = 5174
574040
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 12131
55875393
00016717 00000-0 10270-3 0 9011
2 25544 51
6363 310
5609 0011035 299
2497 60
7553 15
55999852 12155
Satellite: ISS
Catalog Number: 25544
Epoch time: 12131
55875393 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 310
5609 deg
Eccentricity:
0011035
Arg of perigee: 299
2497 deg
Mean anomaly: 60
7553 deg
Mean motion: 15
55999852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1215
Checksum: 320
Coasting Arc #3 (Orbit 1229)
---------------------------------------
Vector Time (GMT): 2012/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5061908
34 A = 6775598
82 meter
Y = 1105701
98 meter E =
0009265
Z = -4371053
48 I = 51
34598
XDOT = 1451
146627 Wp = 355
95242
YDOT = -6729
692896 meter/sec RA = 305
24243 deg
ZDOT = -3373
331255 TA = 239
70717
MA = 239
79888
Ha = 218
118 n
mi
Hp = 213
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16607310
82 X = -5052662
67
Y = 3627631
17 feet Y = 1049148
54 meter
Z = -14340726
66 Z = -4395621
55
XDOT = 4760
979748 XDOT = 1542
678489
YDOT = -22079
044935 feet/sec YDOT = -6712
953295 meter/sec
ZDOT = -11067
359762 ZDOT = -3366
059700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8133448
59 X = -2479075
13
Y = 14829061
93 feet Y = 4519898
07 meter
Z = -14441774
76 Z = -4401852
95
XDOT = -12374
829050 XDOT = -3771
847894
YDOT = -17566
120367 feet/sec YDOT = -5354
153488 meter/sec
ZDOT = -11036
824252 ZDOT = -3364
024032
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 12132
52212513
00016717 00000-0 10270-3 0 9029
2 25544 51
6366 305
7448 0010916 303
8816 56
1299 15
56023852 12301
Satellite: ISS
Catalog Number: 25544
Epoch time: 12132
52212513 = yrday
fracday
Element set: 902
Inclination: 51
6366 deg
RA of node: 305
7448 deg
Eccentricity:
0010916
Arg of perigee: 303
8816 deg
Mean anomaly: 56
1299 deg
Mean motion: 15
56023852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1230
Checksum: 284
Coasting Arc #4 (Orbit 1245)
---------------------------------------
Vector Time (GMT): 2012/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4137158
14 A = 6772213
35 meter
Y = 1211983
08 meter E =
0007567
Z = 5227162
69 I = 51
31697
XDOT = -3177
854597 Wp = 310
41691
YDOT = 6918
149284 meter/sec RA = 300
20484 deg
ZDOT = 916
822188 TA = 130
80555
MA = 130
73990
Ha = 218
347 n
mi
Hp = 213
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13573353
48 X = 4097905
57
Y = 3976322
46 feet Y = 1258027
66 meter
Z = 17149483
89 Z = 5247165
57
XDOT = -10426
032142 XDOT = -3259
432289
YDOT = 22697
340169 feet/sec YDOT = 6882
156384 meter/sec
ZDOT = 3007
946810 ZDOT = 901
186404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11723372
83 X = 3573284
04
Y = -7732273
36 feet Y = -2356796
92 meter
Z = 17231550
74 Z = 5252176
67
XDOT = 10054
623360 XDOT = 3064
649200
YDOT = 21761
611627 feet/sec YDOT = 6632
939224 meter/sec
ZDOT = 2943
036964 ZDOT = 897
037667
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 12133
54971004
00016717 00000-0 10270-3 0 9030
2 25544 51
6360 300
6057 0010936 307
7522 52
2640 15
55985824 12463
Satellite: ISS
Catalog Number: 25544
Epoch time: 12133
54971004 = yrday
fracday
Element set: 903
Inclination: 51
6360 deg
RA of node: 300
6057 deg
Eccentricity:
0010936
Arg of perigee: 307
7522 deg
Mean anomaly: 52
2640 deg
Mean motion: 15
55985824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1246
Checksum: 287
Coasting Arc #5 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2012/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2853459
46 A = 6772769
29 meter
Y = -3474134
63 meter E =
0006290
Z = -5068505
17 I = 51
30565
XDOT = 4364
080977 Wp = 49
29357
YDOT = -6070
150380 meter/sec RA = 295
16189 deg
ZDOT = 1709
240623 TA = 237
26839
MA = 237
32904
Ha = 218
411 n
mi
Hp = 213
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9361743
63 X = -2789777
14
Y = -11398079
50 feet Y = -3505687
58 meter
Z = -16628953
97 Z = -5082212
62
XDOT = 14317
850976 XDOT = 4423
331143
YDOT = -19915
191537 feet/sec YDOT = -6021
017285 meter/sec
ZDOT = 5607
744826 ZDOT = 1730
584983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14686491
16 X = -4476442
51
Y = -16778
84 feet Y = -5114
19 meter
Z = -16684941
30 Z = -5085570
11
XDOT = -6425
144777 XDOT = -1958
384128
YDOT = -22579
649219 feet/sec YDOT = -6882
277082 meter/sec
ZDOT = 5696
018647 ZDOT = 1736
146484
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 12134
51305745
00016717 00000-0 10270-3 0 9042
2 25544 51
6367 295
7892 0010848 310
8792 49
1421 15
56044603 12618
Satellite: ISS
Catalog Number: 25544
Epoch time: 12134
51305745 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 295
7892 deg
Eccentricity:
0010848
Arg of perigee: 310
8792 deg
Mean anomaly: 49
1421 deg
Mean motion: 15
56044603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 304
Coasting Arc #6 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2012/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1375439
74 A = 6777241
30 meter
Y = 5361240
02 meter E =
0010018
Z = 3915795
14 I = 51
30777
XDOT = -4977
175338 Wp = 18
39574
YDOT = 4222
441819 meter/sec RA = 290
12717 deg
ZDOT = -4020
661049 TA = 113
87600
MA = 113
77099
Ha = 218
703 n
mi
Hp = 213
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4512597
56 X = 1296364
85
Y = 17589370
14 feet Y = 5376178
83 meter
Z = 12847096
91 Z = 3922285
04
XDOT = -16329
315413 XDOT = -5004
490017
YDOT = 13853
155573 feet/sec YDOT = 4166
631311 meter/sec
ZDOT = -13191
145173 ZDOT = -4044
906390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16569504
58 X = 5050385
00
Y = 7384318
48 feet Y = 2250740
27 meter
Z = 12873256
63 Z = 3923768
62
XDOT = 1387
497630 XDOT = 422
909278
YDOT = 20126
846848 feet/sec YDOT = 6134
662919 meter/sec
ZDOT = -13291
156134 ZDOT = -4051
144390
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 12135
54061753
00016717 00000-0 10270-3 0 9055
2 25544 51
6360 290
6504 0010909 314
6261 45
4002 15
56041016 12772
Satellite: ISS
Catalog Number: 25544
Epoch time: 12135
54061753 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 290
6504 deg
Eccentricity:
0010909
Arg of perigee: 314
6261 deg
Mean anomaly: 45
4002 deg
Mean motion: 15
56041016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 271
Coasting Arc #7 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2012/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 87730
35 A = 6781972
83 meter
Y = -6470013
66 meter E =
0013629
Z = -2000735
89 I = 51
31579
XDOT = 5045
045946 Wp = 347
64006
YDOT = -1645
122778 meter/sec RA = 285
11115 deg
ZDOT = 5547
313338 TA = 350
12338
MA = 350
15014
Ha = 218
807 n
mi
Hp = 212
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 287829
22 X = 169792
07
Y = -21227078
94 feet Y = -6468573
74 meter
Z = -6564094
13 Z = -2000110
49
XDOT = 16551
988012 XDOT = 5036
119193
YDOT = -5397
384443 feet/sec YDOT = -1588
755965 meter/sec
ZDOT = 18199
846909 ZDOT = 5571
800497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16713853
42 X = -5094382
52
Y = -13090472
16 feet Y = -3989975
92 meter
Z = -6560922
18 Z = -1999769
08
XDOT = 4682
649279 XDOT = 1427
271500
YDOT = -15141
036173 feet/sec YDOT = -4614
987826 meter/sec
ZDOT = 18300
606587 ZDOT = 5578
024888
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 12136
50394368
00016717 00000-0 10270-3 0 9064
2 25544 51
6373 285
8333 0010902 318
4896 41
5429 15
56076145 12929
Satellite: ISS
Catalog Number: 25544
Epoch time: 12136
50394368 = yrday
fracday
Element set: 906
Inclination: 51
6373 deg
RA of node: 285
8333 deg
Eccentricity:
0010902
Arg of perigee: 318
4896 deg
Mean anomaly: 41
5429 deg
Mean motion: 15
56076145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1292
Checksum: 317
Coasting Arc #8 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2012/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1443524
88 A = 6783489
40 meter
Y = 6620530
58 meter E =
0001105
Z = -323715
27 I = 51
31367
XDOT = -4625
912431 Wp = 68
79292
YDOT = -1299
845479 meter/sec RA = 280
10775 deg
ZDOT = -5972
128541 TA = 114
71190
MA = 114
70039
Ha = 219
027 n
mi
Hp = 212
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4735974
01 X = -1515877
15
Y = 21720900
87 feet Y = 6603983
66 meter
Z = -1062057
97 Z = -330903
52
XDOT = -15176
878055 XDOT = -4582
021818
YDOT = -4264
584906 feet/sec YDOT = -1351
329732 meter/sec
ZDOT = -19593
597577 ZDOT = -5994
494760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14735164
16 X = 4491278
04
Y = 16644427
95 feet Y = 5073221
64 meter
Z = -1092202
59 Z = -332903
35
XDOT = -11121
216833 XDOT = -3389
746891
YDOT = 8557
143244 feet/sec YDOT = 2608
217261 meter/sec
ZDOT = -19685
370024 ZDOT = -6000
100783
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 12137
53147933
00016717 00000-0 10270-3 0 9073
2 25544 51
6366 280
6946 0011069 322
7080 37
3304 15
56121071 13084
Satellite: ISS
Catalog Number: 25544
Epoch time: 12137
53147933 = yrday
fracday
Element set: 907
Inclination: 51
6366 deg
RA of node: 280
6946 deg
Eccentricity:
0011069
Arg of perigee: 322
7080 deg
Mean anomaly: 37
3304 deg
Mean motion: 15
56121071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 291
Coasting Arc #9 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2012/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2586000
06 A = 6780609
02 meter
Y = -5700063
33 meter E =
0014057
Z = 2582517
88 I = 51
30137
XDOT = 3837
818171 Wp = 30
33701
YDOT = 4109
948620 meter/sec RA = 275
10168 deg
ZDOT = 5227
840530 TA = 358
91820
MA = 358
92124
Ha = 219
018 n
mi
Hp = 212
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8484252
17 X = 2637001
63
Y = -18700995
19 feet Y = -5670860
02 meter
Z = 8472827
70 Z = 2595204
42
XDOT = 12591
266966 XDOT = 3766
178553
YDOT = 13484
083400 feet/sec YDOT = 4152
464708 meter/sec
ZDOT = 17151
707777 ZDOT = 5246
310946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10416353
64 X = -3174904
59
Y = -17672419
92 feet Y = -5386553
59 meter
Z = 8525474
55 Z = 2598564
64
XDOT = 16928
840746 XDOT = 5159
910660
YDOT = -1666
537742 feet/sec YDOT = -507
960704 meter/sec
ZDOT = 17227
217833 ZDOT = 5250
855995
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 12138
55900311
00016717 00000-0 10270-3 0 9084
2 25544 51
6380 275
5562 0010934 325
9089 34
1362 15
56142626 13247
Satellite: ISS
Catalog Number: 25544
Epoch time: 12138
55900311 = yrday
fracday
Element set: 908
Inclination: 51
6380 deg
RA of node: 275
5562 deg
Eccentricity:
0010934
Arg of perigee: 325
9089 deg
Mean anomaly: 34
1362 deg
Mean motion: 15
56142626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 295
Coasting Arc #10 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2012/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3479031
96 A = 6775476
25 meter
Y = 3887668
97 meter E =
0012922
Z = -4333114
18 I = 51
28262
XDOT = -2738
763129 Wp = 11
75786
YDOT = -6282
695820 meter/sec RA = 270
07945 deg
ZDOT = -3427
274243 TA = 223
21554
MA = 223
31700
Ha = 219
334 n
mi
Hp = 211
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11414146
86 X = -3501196
42
Y = 12754819
46 feet Y = 3848640
60 meter
Z = -14216253
88 Z = -4350069
09
XDOT = -8985
443338 XDOT = -2651
655961
YDOT = -20612
519094 feet/sec YDOT = -6312
835125 meter/sec
ZDOT = -11244
338069 ZDOT = -3440
368053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4173826
62 X = 1272182
35
Y = 16539397
30 feet Y = 5041208
30 meter
Z = -14286271
41 Z = -4354455
52
XDOT = -20852
732444 XDOT = -6355
912849
YDOT = -4526
149309 feet/sec YDOT = -1379
570309 meter/sec
ZDOT = -11297
562664 ZDOT = -3443
497100
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 12139
52229705
00016717 00000-0 10270-3 0 9094
2 25544 51
6383 270
7396 0011082 329
9264 30
1252 15
56129791 13394
Satellite: ISS
Catalog Number: 25544
Epoch time: 12139
52229705 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 270
7396 deg
Eccentricity:
0011082
Arg of perigee: 329
9264 deg
Mean anomaly: 30
1252 deg
Mean motion: 15
56129791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 312
Coasting Arc #11 (Orbit 1354)
---------------------------------------
Vector Time (GMT): 2012/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4078079
12 A = 6771677
91 meter
Y = -1413356
30 meter E =
0008424
Z = 5218600
82 I = 51
27215
XDOT = 1404
504141 Wp = 346
17727
YDOT = 7483
510122 meter/sec RA = 265
03746 deg
ZDOT = 937
568948 TA = 94
85795
MA = 94
76176
Ha = 219
353 n
mi
Hp = 211
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13379524
67 X = 4068229
20
Y = -4636995
72 feet Y = -1367808
16 meter
Z = 17121393
77 Z = 5238388
29
XDOT = 4607
953219 XDOT = 1316
163037
YDOT = 24552
198562 feet/sec YDOT = 7498
722143 meter/sec
ZDOT = 3076
013610 ZDOT = 944
178074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3399580
16 X = 1036192
03
Y = -13644088
71 feet Y = -4158718
24 meter
Z = 17202826
29 Z = 5243421
45
XDOT = 22055
534007 XDOT = 6722
526765
YDOT = 9372
682556 feet/sec YDOT = 2856
793643 meter/sec
ZDOT = 3102
489088 ZDOT = 945
638674
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 12140
54979702
00016717 00000-0 10270-3 0 9109
2 25544 51
6390 265
6005 0011181 333
6407 26
4177 15
56178273 13554
Satellite: ISS
Catalog Number: 25544
Epoch time: 12140
54979702 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 265
6005 deg
Eccentricity:
0011181
Arg of perigee: 333
6407 deg
Mean anomaly: 26
4177 deg
Mean motion: 15
56178273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1355
Checksum: 297
Coasting Arc #12 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2012/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4336807
68 A = 6772332
58 meter
Y = -1218260
28 meter E =
0011459
Z = -5062659
78 I = 51
27838
XDOT = 90
244992 Wp = 50
34674
YDOT = -7468
770991 meter/sec RA = 259
99177 deg
ZDOT = 1729
754477 TA = 236
40694
MA = 236
51638
Ha = 219
522 n
mi
Hp = 211
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14228371
66 X = -4298268
82
Y = -3996916
93 feet Y = -1266541
20 meter
Z = -16609776
17 Z = -5083634
68
XDOT = 296
079370 XDOT = 165
352694
YDOT = -24503
841834 feet/sec YDOT = -7467
342024 meter/sec
ZDOT = 5675
047498 ZDOT = 1730
374645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10920518
98 X = -3328574
19
Y = 9813118
50 feet Y = 2991038
52 meter
Z = -16695853
98 Z = -5088896
29
XDOT = -19866
822788 XDOT = -6055
407586
YDOT = -12502
304295 feet/sec YDOT = -3810
702349 meter/sec
ZDOT = 5678
271845 ZDOT = 1730
737258
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 12141
51306900
00016717 00000-0 10270-3 0 9112
2 25544 51
6393 260
7848 0011143 337
9387 22
1286 15
56192064 13705
Satellite: ISS
Catalog Number: 25544
Epoch time: 12141
51306900 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 260
7848 deg
Eccentricity:
0011143
Arg of perigee: 337
9387 deg
Mean anomaly: 22
1286 deg
Mean motion: 15
56192064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1370
Checksum: 291
Coasting Arc #13 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2012/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4193016
22 A = 6776985
57 meter
Y = 3662212
08 meter E =
0014490
Z = 3867824
25 I = 51
30025
XDOT = -1696
821292 Wp = 31
80306
YDOT = 6268
069007 meter/sec RA = 254
95528 deg
ZDOT = -4076
272540 TA = 101
21879
MA = 101
05589
Ha = 219
787 n
mi
Hp = 211
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13756614
90 X = 4132963
67
Y = 12015131
50 feet Y = 3708764
80 meter
Z = 12689712
09 Z = 3888048
58
XDOT = -5566
998988 XDOT = -1746
984075
YDOT = 20564
530864 feet/sec YDOT = 6248
814058 meter/sec
ZDOT = -13373
597571 ZDOT = -4084
636936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17370821
25 X = 5294626
32
Y = -5454780
63 feet Y = -1662617
14 meter
Z = 12772492
66 Z = 3893055
76
XDOT = 14331
278468 XDOT = 4368
173677
YDOT = 14095
945622 feet/sec YDOT = 4296
444226 meter/sec
ZDOT = -13408
534376 ZDOT = -4086
921278
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 12142
54054755
00016717 00000-0 10270-3 0 9125
2 25544 51
6395 255
6461 0011129 341
9891 18
0867 15
56164120 13868
Satellite: ISS
Catalog Number: 25544
Epoch time: 12142
54054755 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 255
6461 deg
Eccentricity:
0011129
Arg of perigee: 341
9891 deg
Mean anomaly: 18
0867 deg
Mean motion: 15
56164120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1386
Checksum: 307
Coasting Arc #14 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2012/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3600512
78 A = 6781795
76 meter
Y = -5408748
72 meter E =
0016522
Z = -1907523
79 I = 51
32580
XDOT = 3255
948113 Wp = 5
44467
YDOT = -4132
482109 meter/sec RA = 249
93949 deg
ZDOT = 5592
000931 TA = 333
40547
MA = 333
49014
Ha = 219
948 n
mi
Hp = 210
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11812705
98 X = -3530497
01
Y = -17745238
58 feet Y = -5448620
18 meter
Z = -6258280
14 Z = -1924845
71
XDOT = 10682
244465 XDOT = 3274
751345
YDOT = -13558
012168 feet/sec YDOT = -4095
967597 meter/sec
ZDOT = 18346
459748 ZDOT = 5607
863584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21261671
61 X = -6480557
51
Y = 1218539
31 feet Y = 371410
78 meter
Z = -6328986
29 Z = -1929075
02
XDOT = -6287
377154 XDOT = -1916
392557
YDOT = -14414
027230 feet/sec YDOT = -4393
395500 meter/sec
ZDOT = 18412
020719 ZDOT = 5611
983915
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 12143
50379609
00016717 00000-0 10270-3 0 9131
2 25544 51
6400 250
8291 0011448 345
3730 14
7091 15
56177589 14010
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
50379609 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 250
8291 deg
Eccentricity:
0011448
Arg of perigee: 345
3730 deg
Mean anomaly: 14
7091 deg
Mean motion: 15
56177589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1401
Checksum: 295
Coasting Arc #15 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2012/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2518674
33 A = 6783151
84 meter
Y = 6282676
01 meter E =
0005996
Z = -474739
19 I = 51
34158
XDOT = -4608
312638 Wp = 62
22209
YDOT = 1401
223573 meter/sec RA = 244
93817 deg
ZDOT = -5960
294557 TA = 122
91836
MA = 122
86067
Ha = 220
065 n
mi
Hp = 210
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8263367
22 X = 2450539
17
Y = 20612454
08 feet Y = 6310460
47 meter
Z = -1557543
29 Z = -462668
21
XDOT = -15119
135951 XDOT = -4594
684855
YDOT = 4597
190200 feet/sec YDOT = 1349
767483 meter/sec
ZDOT = -19554
772169 ZDOT = -5982
648486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22023975
85 X = 6712907
84
Y = 2872525
51 feet Y = 875545
78 meter
Z = -1508484
99 Z = -459786
23
XDOT = -3122
860050 XDOT = -951
847743
YDOT = 13724
067237 feet/sec YDOT = 4183
095694 meter/sec
ZDOT = -19646
774645 ZDOT = -5988
336912
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 12144
53125095
00016717 00000-0 10270-3 0 9144
2 25544 51
6394 245
6911 0011319 349
2824 10
8087 15
56221923 14178
Satellite: ISS
Catalog Number: 25544
Epoch time: 12144
53125095 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 245
6911 deg
Eccentricity:
0011319
Arg of perigee: 349
2824 deg
Mean anomaly: 10
8087 deg
Mean motion: 15
56221923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1417
Checksum: 296
Coasting Arc #16 (Orbit 1424)
---------------------------------------
Vector Time (GMT): 2012/145/00:28:46
715
Vector Time (MET): N/A
Weight (LBS) : 911399
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -16148
03 A = 6780089
98 meter
Y = 5862385
27 meter E =
0009605
Z = -3417609
29 I = 51
33203
XDOT = -5533
220307 Wp = 12
53988
YDOT = -2682
807453 meter/sec RA = 242
34967 deg
ZDOT = -4569
019625 TA = 207
62906
MA = 207
68014
Ha = 220
328 n
mi
Hp = 212
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -52979
09 X = -65099
10
Y = 19233547
46 feet Y = 5861931
40 meter
Z = -11212628
92 Z = -3417805
94
XDOT = -18153
609932 XDOT = -5480
613920
YDOT = -8801
861722 feet/sec YDOT = -2744
388662 meter/sec
ZDOT = -14990
221868 ZDOT = -4595
772521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17888901
68 X = -5452537
23
Y = -7063261
84 feet Y = -2152882
21 meter
Z = -11213952
51 Z = -3418012
73
XDOT = 14316
684497 XDOT = 4363
725435
YDOT = -12250
736444 feet/sec YDOT = -3734
024468 meter/sec
ZDOT = -15099
951022 ZDOT = -4602
465071
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 12145
04498333
00016717 00000-0 10270-3 0 9150
2 25544 51
6393 243
1245 0009780 343
3003 16
7827 15
55604120 14252
Satellite: ISS
Catalog Number: 25544
Epoch time: 12145
04498333 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 243
1245 deg
Eccentricity:
0009780
Arg of perigee: 343
3003 deg
Mean anomaly: 16
7827 deg
Mean motion: 15
55604120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1425
Checksum: 286
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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