[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 26th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
060/10:21:41
428 2
6 4
2 4
2
N/A -3
3 -0
0 220
0
000/00:01:22
856 0
2 0
0 201
5
Coasting Arc #1 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2012/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 125211
71 A = 6763942
20 meter
Y = -4588111
83 meter E =
0032023
Z = -4995815
77 I = 51
46458
XDOT = 7105
038611 Wp = 88
63727
YDOT = -1998
640903 meter/sec RA = 331
66314 deg
ZDOT = 2025
612196 TA = 201
07235
MA = 201
20459
Ha = 220
332 n
mi
Hp = 199
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 410799
58 X = 200775
75
Y = -15052860
35 feet Y = -4586289
69 meter
Z = -16390471
70 Z = -4995023
46
XDOT = 23310
494129 XDOT = 7117
019944
YDOT = -6557
220812 feet/sec YDOT = -1919
120763 meter/sec
ZDOT = 6645
709305 ZDOT = 2060
156911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7293175
25 X = 2222959
82
Y = -13178992
07 feet Y = -4016956
78 meter
Z = -16386844
90 Z = -4994710
33
XDOT = 22747
672671 XDOT = 6933
490630
YDOT = 4197
809265 feet/sec YDOT = 1279
492264 meter/sec
ZDOT = 6787
475492 ZDOT = 2068
822530
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 12055
51247879
00016717 00000-0 10270-3 0 9003
2 25544 51
6429 332
1691 0020153 78
9151 281
4269 15
59236826 296
Satellite: ISS
Catalog Number: 25544
Epoch time: 12055
51247879 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 332
1691 deg
Eccentricity:
0020153
Arg of perigee: 78
9151 deg
Mean anomaly: 281
4269 deg
Mean motion: 15
59236826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 29
Checksum: 313
Coasting Arc #2 (Orbit 44)
---------------------------------------
Vector Time (GMT): 2012/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3493294
49 A = 6771017
30 meter
Y = 5030029
92 meter E =
0033222
Z = 2860298
94 I = 51
46171
XDOT = -5699
327680 Wp = 89
03524
YDOT = -1059
058484 meter/sec RA = 326
62004 deg
ZDOT = -5046
985055 TA = 58
21209
MA = 57
88892
Ha = 220
345 n
mi
Hp = 199
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11460939
93 X = -3563176
18
Y = 16502722
84 feet Y = 4990575
31 meter
Z = 9384182
86 Z = 2843158
62
XDOT = -18698
581627 XDOT = -5662
544683
YDOT = -3474
601326 feet/sec YDOT = -1122
586745 meter/sec
ZDOT = -16558
349919 ZDOT = -5074
582322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17592176
68 X = -5362095
45
Y = 9773927
87 feet Y = 2979093
21 meter
Z = 9313514
20 Z = 2838759
13
XDOT = -14472
762831 XDOT = -4411
298111
YDOT = -10002
315733 feet/sec YDOT = -3048
705835 meter/sec
ZDOT = -16671
379904 ZDOT = -5081
436595
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 12056
53792505
00016717 00000-0 10270-3 0 9018
2 25544 51
6425 327
0172 0020164 82
9554 277
3894 15
59260686 450
Satellite: ISS
Catalog Number: 25544
Epoch time: 12056
53792505 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 327
0172 deg
Eccentricity:
0020164
Arg of perigee: 82
9554 deg
Mean anomaly: 277
3894 deg
Mean motion: 15
59260686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 45
Checksum: 312
Coasting Arc #3 (Orbit 60)
---------------------------------------
Vector Time (GMT): 2012/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5465812
44 A = 6774304
75 meter
Y = -3972728
39 meter E =
0031300
Z = 352099
62 I = 51
44852
XDOT = 2547
277681 Wp = 71
54967
YDOT = 4073
499748 meter/sec RA = 321
60922 deg
ZDOT = 5991
558701 TA = 292
26564
MA = 292
59727
Ha = 220
240 n
mi
Hp = 199
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17932455
52 X = 5508119
66
Y = -13033885
79 feet Y = -3911369
71 meter
Z = 1155182
48 Z = 378755
15
XDOT = 8357
210240 XDOT = 2472
432321
YDOT = 13364
500486 feet/sec YDOT = 4101
567053 meter/sec
ZDOT = 19657
344818 ZDOT = 6003
750958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21757475
21 X = 6631678
44
Y = -4219270
37 feet Y = -1286033
61 meter
Z = 1264759
50 Z = 385498
70
XDOT = 1496
849729 XDOT = 456
239797
YDOT = 14009
653959 feet/sec YDOT = 4270
142527 meter/sec
ZDOT = 19706
983971 ZDOT = 6006
688714
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 12057
56335040
00016717 00000-0 10270-3 0 9020
2 25544 51
6427 321
8656 0020078 86
4102 273
9349 15
59291825 617
Satellite: ISS
Catalog Number: 25544
Epoch time: 12057
56335040 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 321
8656 deg
Eccentricity:
0020078
Arg of perigee: 86
4102 deg
Mean anomaly: 273
9349 deg
Mean motion: 15
59291825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 61
Checksum: 301
Coasting Arc #4 (Orbit 75)
---------------------------------------
Vector Time (GMT): 2012/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5611514
68 A = 6768852
49 meter
Y = 1436217
72 meter E =
0025167
Z = -3524700
80 I = 51
40808
XDOT = 1237
340853 Wp = 88
39383
YDOT = -6090
584255 meter/sec RA = 316
59054 deg
ZDOT = -4478
698169 TA = 133
29424
MA = 133
08407
Ha = 220
104 n
mi
Hp = 199
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18410481
25 X = -5610035
65
Y = 4712000
38 feet Y = 1373474
28 meter
Z = -11563979
01 Z = -3551957
57
XDOT = 4059
517233 XDOT = 1327
111344
YDOT = -19982
231809 feet/sec YDOT = -6076
245969 meter/sec
ZDOT = -14693
891629 ZDOT = -4472
468741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18667239
80 X = -5689774
69
Y = -3175533
72 feet Y = -967902
68 meter
Z = -11675809
25 Z = -3558786
66
XDOT = 11704
045968 XDOT = 3567
393211
YDOT = -15193
964691 feet/sec YDOT = -4631
120438 meter/sec
ZDOT = -14667
864664 ZDOT = -4470
765150
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 12058
52466709
00016717 00000-0 10270-3 0 9035
2 25544 51
6432 317
0350 0019946 90
1084 270
2357 15
59331218 760
Satellite: ISS
Catalog Number: 25544
Epoch time: 12058
52466709 = yrday
fracday
Element set: 903
Inclination: 51
6432 deg
RA of node: 317
0350 deg
Eccentricity:
0019946
Arg of perigee: 90
1084 deg
Mean anomaly: 270
2357 deg
Mean motion: 15
59331218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 76
Checksum: 299
Coasting Arc #5 (Orbit 91)
---------------------------------------
Vector Time (GMT): 2012/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3962831
55 A = 6762508
02 meter
Y = 1758689
88 meter E =
0023373
Z = 5170406
78 I = 51
36554
XDOT = -4309
313857 Wp = 98
26961
YDOT = 6267
364443 meter/sec RA = 311
53297 deg
ZDOT = 1163
229328 TA = 340
52664
MA = 340
61578
Ha = 219
934 n
mi
Hp = 199
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13001415
84 X = 3917754
54
Y = 5769979
93 feet Y = 1802753
02 meter
Z = 16963276
85 Z = 5189548
27
XDOT = -14138
168823 XDOT = -4384
727166
YDOT = 20562
219302 feet/sec YDOT = 6218
753456 meter/sec
ZDOT = 3816
369187 ZDOT = 1142
111461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9604229
99 X = 2927369
30
Y = 10364620
17 feet Y = 3159136
23 meter
Z = 17041586
16 Z = 5194275
46
XDOT = -20331
652359 XDOT = -6197
087639
YDOT = 12666
358814 feet/sec YDOT = 3860
706166 meter/sec
ZDOT = 3729
311011 ZDOT = 1136
693996
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 12059
55005222
00016717 00000-0 10270-3 0 9049
2 25544 51
6429 311
8830 0019928 93
9875 266
3559 15
59381216 921
Satellite: ISS
Catalog Number: 25544
Epoch time: 12059
55005222 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 311
8830 deg
Eccentricity:
0019928
Arg of perigee: 93
9875 deg
Mean anomaly: 266
3559 deg
Mean motion: 15
59381216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 92
Checksum: 324
Coasting Arc #6 (Orbit 105)
---------------------------------------
Vector Time (GMT): 2012/060/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2981443
59 A = 6764484
93 meter
Y = -3056318
47 meter E =
0031279
Z = -5273979
20 I = 51
34587
XDOT = 4936
052576 Wp = 96
10697
YDOT = -5818
557617 meter/sec RA = 306
81596 deg
ZDOT = 581
214435 TA = 179
47603
MA = 179
47275
Ha = 220
024 n
mi
Hp = 201
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9781639
07 X = -2921426
08
Y = -10027291
55 feet Y = -3089323
54 meter
Z = -17303081
38 Z = -5288316
83
XDOT = 16194
398214 XDOT = 4997
926617
YDOT = -19089
755962 feet/sec YDOT = -5763
013641 meter/sec
ZDOT = 1906
871507 ZDOT = 605
343950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 628488
85 X = 191563
40
Y = -13921334
07 feet Y = -4243222
63 meter
Z = -17361599
10 Z = -5291815
41
XDOT = 23972
791124 XDOT = 7306
906735
YDOT = -1420
899854 feet/sec YDOT = -433
090276 meter/sec
ZDOT = 2006
233159 ZDOT = 611
499867
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 12060
44724984
00016717 00000-0 10270-3 0 9053
2 25544 51
6425 307
3742 0016574 97
8789 262
4248 15
58606751 1061
Satellite: ISS
Catalog Number: 25544
Epoch time: 12060
44724984 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 307
3742 deg
Eccentricity:
0016574
Arg of perigee: 97
8789 deg
Mean anomaly: 262
4248 deg
Mean motion: 15
58606751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 106
Checksum: 328
Coasting Arc #7 (Orbit 121)
---------------------------------------
Vector Time (GMT): 2012/061/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 414373
18 A = 6769386
31 meter
Y = 5421787
94 meter E =
0026869
Z = 4008016
47 I = 51
34467
XDOT = -5729
617397 Wp = 92
10546
YDOT = 3334
477044 meter/sec RA = 301
75673 deg
ZDOT = -3896
696189 TA = 38
44925
MA = 38
25809
Ha = 219
952 n
mi
Hp = 201
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1359492
04 X = 334245
04
Y = 17788018
17 feet Y = 5425973
90 meter
Z = 13149660
34 Z = 4009834
55
XDOT = -18797
957340 XDOT = -5747
549301
YDOT = 10939
885315 feet/sec YDOT = 3270
304467 meter/sec
ZDOT = -12784
436315 ZDOT = -3924
573810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11808741
86 X = -3599304
52
Y = 13365280
26 feet Y = 4073737
42 meter
Z = 13156681
78 Z = 4010156
61
XDOT = -19941
174187 XDOT = -6078
069892
YDOT = -4851
411163 feet/sec YDOT = -1478
710123 meter/sec
ZDOT = -12898
958958 ZDOT = -3931
602690
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 12061
47311494
00016717 00000-0 10270-3 0 9066
2 25544 51
6420 302
2254 0016578 101
5657 258
7360 15
58632324 1225
Satellite: ISS
Catalog Number: 25544
Epoch time: 12061
47311494 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 302
2254 deg
Eccentricity:
0016578
Arg of perigee: 101
5657 deg
Mean anomaly: 258
7360 deg
Mean motion: 15
58632324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 122
Checksum: 285
Coasting Arc #8 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2012/062/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1968937
24 A = 6775356
70 meter
Y = -6339375
65 meter E =
0021373
Z = -1366416
91 I = 51
35070
XDOT = 5017
923183 Wp = 82
78353
YDOT = 328
128811 meter/sec RA = 296
72899 deg
ZDOT = 5788
814507 TA = 262
25566
MA = 262
49839
Ha = 219
850 n
mi
Hp = 201
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6459767
86 X = 2046316
73
Y = -20798476
53 feet Y = -6316925
19 meter
Z = -4482995
11 Z = -1356663
79
XDOT = 16463
002568 XDOT = 4985
760690
YDOT = 1076
538093 feet/sec YDOT = 384
062773 meter/sec
ZDOT = 18992
173581 ZDOT = 5813
112859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19221038
09 X = 5858572
41
Y = -10257589
36 feet Y = -3126513
24 meter
Z = -4442524
85 Z = -1354081
58
XDOT = 10137
108765 XDOT = 3089
790752
YDOT = 10842
238415 feet/sec YDOT = 3304
714269 meter/sec
ZDOT = 19091
738572 ZDOT = 5819
161917
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 12062
43484505
00016717 00000-0 10270-3 0 9078
2 25544 51
6427 297
3982 0016452 105
2325 255
0650 15
58673465 1377
Satellite: ISS
Catalog Number: 25544
Epoch time: 12062
43484505 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 297
3982 deg
Eccentricity:
0016452
Arg of perigee: 105
2325 deg
Mean anomaly: 255
0650 deg
Mean motion: 15
58673465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 309
Coasting Arc #9 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2012/063/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3727615
49 A = 6774664
49 meter
Y = 5340130
39 meter E =
0022703
Z = -1858583
52 I = 51
33578
XDOT = -3180
997010 Wp = 118
62549
YDOT = -4152
393806 meter/sec RA = 291
71673 deg
ZDOT = -5613
719923 TA = 81
95152
MA = 81
69399
Ha = 219
754 n
mi
Hp = 201
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12229709
61 X = -3778024
44
Y = 17520112
84 feet Y = 5298163
95 meter
Z = -6097714
95 Z = -1876814
50
XDOT = -10436
341896 XDOT = -3107
057985
YDOT = -13623
339259 feet/sec YDOT = -4187
552558 meter/sec
ZDOT = -18417
716283 ZDOT = -5628
992976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20911783
08 X = -6373911
48
Y = 4277328
29 feet Y = 1303729
66 meter
Z = -6172849
39 Z = -1881484
49
XDOT = 2232
468628 XDOT = 680
456438
YDOT = -15461
140953 feet/sec YDOT = -4712
555762 meter/sec
ZDOT = -18479
998711 ZDOT = -5632
703607
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 12063
46067234
00016717 00000-0 10270-3 0 9089
2 25544 51
6429 292
2485 0016336 109
4309 250
8613 15
58662430 1530
Satellite: ISS
Catalog Number: 25544
Epoch time: 12063
46067234 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 292
2485 deg
Eccentricity:
0016336
Arg of perigee: 109
4309 deg
Mean anomaly: 250
8613 deg
Mean motion: 15
58662430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 303
Coasting Arc #10 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2012/064/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4430537
35 A = 6767913
02 meter
Y = -2699013
18 meter E =
0025878
Z = 4330894
37 I = 51
30312
XDOT = 804
810444 Wp = 110
96886
YDOT = 6838
938801 meter/sec RA = 286
68167 deg
ZDOT = 3413
076789 TA = 304
22776
MA = 304
47267
Ha = 219
609 n
mi
Hp = 201
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14535883
71 X = 4439350
90
Y = -8855030
11 feet Y = -2649418
61 meter
Z = 14208971
04 Z = 4352438
87
XDOT = 2640
454214 XDOT = 711
696619
YDOT = 22437
463258 feet/sec YDOT = 6847
418285 meter/sec
ZDOT = 11197
758494 ZDOT = 3416
759825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16628213
97 X = 5068279
62
Y = 3268460
26 feet Y = 996226
69 meter
Z = 14297482
27 Z = 4357872
60
XDOT = -13062
119349 XDOT = -3981
333977
YDOT = 17040
744666 feet/sec YDOT = 5194
018974 meter/sec
ZDOT = 11212
342467 ZDOT = 3417
521984
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 12064
48647987
00016717 00000-0 10270-3 0 9092
2 25544 51
6427 287
0996 0016355 112
4913 247
7976 15
58713647 1694
Satellite: ISS
Catalog Number: 25544
Epoch time: 12064
48647987 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 287
0996 deg
Eccentricity:
0016355
Arg of perigee: 112
4913 deg
Mean anomaly: 247
7976 deg
Mean motion: 15
58713647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 360
Coasting Arc #11 (Orbit 183)
---------------------------------------
Vector Time (GMT): 2012/065/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4138835
39 A = 6763903
06 meter
Y = -937762
85 meter E =
0030296
Z = -5292582
77 I = 51
28204
XDOT = 1596
452857 Wp = 103
77111
YDOT = -7485
324181 meter/sec RA = 281
61274 deg
ZDOT = 71
114523 TA = 166
95050
MA = 166
87194
Ha = 219
505 n
mi
Hp = 201
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13578856
25 X = -4102331
91
Y = -3076649
78 feet Y = -983842
22 meter
Z = -17364116
68 Z = -5312599
86
XDOT = 5237
706223 XDOT = 1679
691156
YDOT = -24558
150201 feet/sec YDOT = -7467
006243 meter/sec
ZDOT = 233
315364 ZDOT = 79
072675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8025240
60 X = -2446093
33
Y = -11251347
07 feet Y = -3429410
59 meter
Z = -17446098
75 Z = -5317570
90
XDOT = 19408
728712 XDOT = 5915
780511
YDOT = -14290
932435 feet/sec YDOT = -4355
876206 meter/sec
ZDOT = 266
481978 ZDOT = 81
223707
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 12065
44815557
00016717 00000-0 10270-3 0 9101
2 25544 51
6423 282
2715 0016145 116
1112 244
1707 15
58765119 1846
Satellite: ISS
Catalog Number: 25544
Epoch time: 12065
44815557 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 282
2715 deg
Eccentricity:
0016145
Arg of perigee: 116
1112 deg
Mean anomaly: 244
1707 deg
Mean motion: 15
58765119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 184
Checksum: 291
Coasting Arc #12 (Orbit 199)
---------------------------------------
Vector Time (GMT): 2012/066/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2938677
91 A = 6767877
07 meter
Y = 4338426
78 meter E =
0023832
Z = 4259971
02 I = 51
29062
XDOT = -3518
195793 Wp = 101
87629
YDOT = 5858
999450 meter/sec RA = 276
54487 deg
ZDOT = -3528
051017 TA = 24
18448
MA = 24
07278
Ha = 219
243 n
mi
Hp = 201
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9641331
73 X = 2869252
80
Y = 14233683
68 feet Y = 4370901
19 meter
Z = 13976282
88 Z = 4274077
58
XDOT = -11542
637116 XDOT = -3566
312709
YDOT = 19222
439141 feet/sec YDOT = 5819
387387 meter/sec
ZDOT = -11574
970528 ZDOT = -3545
259408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2021946
40 X = -616289
26
Y = 17025090
80 feet Y = 5189247
67 meter
Z = 14033799
48 Z = 4277502
08
XDOT = -19984
003348 XDOT = -6091
124220
YDOT = 7258
384086 feet/sec YDOT = 2212
355469 meter/sec
ZDOT = -11645
924521 ZDOT = -3549
677794
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 12066
47392393
00016717 00000-0 10270-3 0 9114
2 25544 51
6421 277
1220 0015987 119
6219 240
6531 15
58822551 2006
Satellite: ISS
Catalog Number: 25544
Epoch time: 12066
47392393 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 277
1220 deg
Eccentricity:
0015987
Arg of perigee: 119
6219 deg
Mean anomaly: 240
6531 deg
Mean motion: 15
58822551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 200
Checksum: 294
Coasting Arc #13 (Orbit 214)
---------------------------------------
Vector Time (GMT): 2012/067/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1195910
91 A = 6774492
55 meter
Y = -6452441
81 meter E =
0018238
Z = -1704814
98 I = 51
30944
XDOT = 4601
209517 Wp = 98
61614
YDOT = -2336
877831 meter/sec RA = 271
50845 deg
ZDOT = 5666
384768 TA = 242
59142
MA = 242
77707
Ha = 219
286 n
mi
Hp = 201
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3923592
23 X = -1115388
07
Y = -21169428
51 feet Y = -6465365
22 meter
Z = -5593225
01 Z = -1710428
13
XDOT = 15095
831749 XDOT = 4599
473460
YDOT = -7666
922019 feet/sec YDOT = -2285
433230 meter/sec
ZDOT = 18590
501208 ZDOT = 5688
732917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10517674
33 X = 3205787
14
Y = -18779373
85 feet Y = -5723953
15 meter
Z = -5615789
33 Z = -1711692
59
XDOT = 15057
341224 XDOT = 4589
477605
YDOT = 2894
606923 feet/sec YDOT = 882
276190 meter/sec
ZDOT = 18682
270007 ZDOT = 5694
355898
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 12067
43556502
00016717 00000-0 10270-3 0 9126
2 25544 51
6413 272
2937 0015941 123
3606 236
9077 15
58810399 2156
Satellite: ISS
Catalog Number: 25544
Epoch time: 12067
43556502 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 272
2937 deg
Eccentricity:
0015941
Arg of perigee: 123
3606 deg
Mean anomaly: 236
9077 deg
Mean motion: 15
58810399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 215
Checksum: 306
Coasting Arc #14 (Orbit 230)
---------------------------------------
Vector Time (GMT): 2012/068/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -853772
53 A = 6774715
71 meter
Y = 6529259
02 meter E =
0023834
Z = -1562751
63 I = 51
30980
XDOT = -4717
421142 Wp = 132
66886
YDOT = -1970
911583 meter/sec RA = 266
49309 deg
ZDOT = -5728
804066 TA = 64
53887
MA = 64
29247
Ha = 219
200 n
mi
Hp = 202
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2801090
98 X = -919129
17
Y = 21421453
49 feet Y = 6519345
96 meter
Z = -5127137
91 Z = -1567058
85
XDOT = -15477
103483 XDOT = -4667
202529
YDOT = -6466
245352 feet/sec YDOT = -2023
384729 meter/sec
ZDOT = -18795
288929 ZDOT = -5751
598518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15549121
56 X = -4739372
25
Y = 14992121
99 feet Y = 4569598
78 meter
Z = -5145232
79 Z = -1568266
95
XDOT = -6858
506169 XDOT = -2090
472680
YDOT = -13515
599645 feet/sec YDOT = -4119
554772 meter/sec
ZDOT = -18888
593701 ZDOT = -5757
243360
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 12068
46129560
00016717 00000-0 10270-3 0 9131
2 25544 51
6407 267
1432 0015917 127
8403 232
4195 15
58805284 2316
Satellite: ISS
Catalog Number: 25544
Epoch time: 12068
46129560 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 267
1432 deg
Eccentricity:
0015917
Arg of perigee: 127
8403 deg
Mean anomaly: 232
4195 deg
Mean motion: 15
58805284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 231
Checksum: 301
Coasting Arc #15 (Orbit 246)
---------------------------------------
Vector Time (GMT): 2012/069/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2697365
53 A = 6768147
82 meter
Y = -4581849
03 meter E =
0025394
Z = 4177632
56 I = 51
29046
XDOT = 3797
944548 Wp = 120
75602
YDOT = 5590
747328 meter/sec RA = 261
45729 deg
ZDOT = 3650
151766 TA = 291
59412
MA = 291
86450
Ha = 219
044 n
mi
Hp = 202
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8849624
44 X = 2728106
37
Y = -15032313
10 feet Y = -4551512
95 meter
Z = 13706143
55 Z = 4190811
45
XDOT = 12460
447993 XDOT = 3717
413933
YDOT = 18342
346878 feet/sec YDOT = 5632
768535 meter/sec
ZDOT = 11975
563538 ZDOT = 3668
405468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16127252
84 X = 4915586
67
Y = -6534974
87 feet Y = -1991860
34 meter
Z = 13760468
02 Z = 4194190
65
XDOT = -1889
192634 XDOT = -575
825915
YDOT = 20912
893962 feet/sec YDOT = 6374
250080 meter/sec
ZDOT = 12050
018959 ZDOT = 3672
845779
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 12069
48700584
00016717 00000-0 10270-3 0 9146
2 25544 51
6401 261
9921 0015791 130
6964 229
5566 15
58843325 2473
Satellite: ISS
Catalog Number: 25544
Epoch time: 12069
48700584 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 261
9921 deg
Eccentricity:
0015791
Arg of perigee: 130
6964 deg
Mean anomaly: 229
5566 deg
Mean motion: 15
58843325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 247
Checksum: 323
Coasting Arc #16 (Orbit 261)
---------------------------------------
Vector Time (GMT): 2012/070/10:22:22
856
Vector Time (MET): N/A
Weight (LBS) : 886174
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4078985
80 A = 6763495
79 meter
Y = 1171363
89 meter E =
0028201
Z = -5288736
80 I = 51
28010
XDOT = -1929
338477 Wp = 112
38837
YDOT = -7408
231280 meter/sec RA = 256
38685 deg
ZDOT = -164
019877 TA = 156
10401
MA = 155
97285
Ha = 218
881 n
mi
Hp = 202
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13382499
35 X = -4066089
66
Y = 3843057
39 feet Y = 1125821
58 meter
Z = -17351498
68 Z = -5308521
09
XDOT = -6329
850645 XDOT = -1845
557979
YDOT = -24305
220735 feet/sec YDOT = -7429
337913 meter/sec
ZDOT = -538
122957 ZDOT = -173
188040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12940709
50 X = -3944328
25
Y = -4855386
62 feet Y = -1479921
84 meter
Z = -17432674
60 Z = -5313479
22
XDOT = 9101
303560 XDOT = 2774
077325
YDOT = -22323
612102 feet/sec YDOT = -6804
236969 meter/sec
ZDOT = -575
222211 ZDOT = -175
327730
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 12070
44858854
00016717 00000-0 10270-3 0 9159
2 25544 51
6391 257
1620 0015727 134
6581 225
5859 15
58907346 2624
Satellite: ISS
Catalog Number: 25544
Epoch time: 12070
44858854 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 257
1620 deg
Eccentricity:
0015727
Arg of perigee: 134
6581 deg
Mean anomaly: 225
5859 deg
Mean motion: 15
58907346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 262
Checksum: 327
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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