[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 14th 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) : 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
There are no maneuvers
Coasting Arc #1 (Orbit 3857)
---------------------------------------
Vector Time (GMT): 2012/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 202456
72 A = 6764835
70 meter
Y = 4524351
42 meter E =
0021739
Z = 5006249
91 I = 51
78304
XDOT = -7184
638307 Wp = 53
32684
YDOT = -1883
905221 meter/sec RA = 26
93282 deg
ZDOT = 1999
838045 TA = 17
38623
MA = 17
31191
Ha = 220
625 n
mi
Hp = 201
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 664228
08 X = 127530
48
Y = 14843672
63 feet Y = 4526196
65 meter
Z = 16424704
42 Z = 5007051
27
XDOT = -23571
647989 XDOT = -7172
752785
YDOT = -6180
791407 feet/sec YDOT = -1964
181750 meter/sec
ZDOT = 6561
148441 ZDOT = 1964
964689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8664942
67 X = -2641074
53
Y = 12066457
01 feet Y = 3677856
10 meter
Z = 16427602
23 Z = 5007133
16
XDOT = -13968
134491 XDOT = -4257
487393
YDOT = -18738
594584 feet/sec YDOT = -5711
523629 meter/sec
ZDOT = 6418
325020 ZDOT = 1956
305466
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 12044
55150661
00016717 00000-0 10270-3 0 9007
2 25544 51
6392 27
2103 0020538 38
5506 321
7112 15
58864008 38584
Satellite: ISS
Catalog Number: 25544
Epoch time: 12044
55150661 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 27
2103 deg
Eccentricity:
0020538
Arg of perigee: 38
5506 deg
Mean anomaly: 321
7112 deg
Mean motion: 15
58864008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3858
Checksum: 285
Coasting Arc #2 (Orbit 3872)
---------------------------------------
Vector Time (GMT): 2012/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3244082
07 A = 6764583
92 meter
Y = -3042850
78 meter E =
0029562
Z = -5116700
28 I = 51
75452
XDOT = 6333
248848 Wp = 65
04905
YDOT = 3968
126931 meter/sec RA = 21
89256 deg
ZDOT = 1675
321386 TA = 221
01101
MA = 221
23367
Ha = 220
711 n
mi
Hp = 200
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10643313
88 X = 3302722
22
Y = -9983106
22 feet Y = -3006245
64 meter
Z = -16787074
43 Z = -5100798
39
XDOT = 20778
375486 XDOT = 6280
267515
YDOT = 13018
789144 feet/sec YDOT = 4038
653010 meter/sec
ZDOT = 5496
461241 ZDOT = 1705
958930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14586548
38 X = 4445979
94
Y = -1539068
92 feet Y = -469108
21 meter
Z = -16721611
20 Z = -5096747
09
XDOT = 8670
183608 XDOT = 2642
671964
YDOT = 21799
100308 feet/sec YDOT = 6644
365774 meter/sec
ZDOT = 5621
732276 ZDOT = 1713
503998
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 12045
51310073
00016717 00000-0 10270-3 0 9010
2 25544 51
6394 22
3823 0020595 42
2177 318
0559 15
58857760 38738
Satellite: ISS
Catalog Number: 25544
Epoch time: 12045
51310073 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 22
3823 deg
Eccentricity:
0020595
Arg of perigee: 42
2177 deg
Mean anomaly: 318
0559 deg
Mean motion: 15
58857760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 302
Coasting Arc #3 (Orbit 3888)
---------------------------------------
Vector Time (GMT): 2012/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5870866
66 A = 6771073
50 meter
Y = 893119
49 meter E =
0030739
Z = 3244856
21 I = 51
74799
XDOT = -3413
818731 Wp = 63
16089
YDOT = -4959
261961 meter/sec RA = 16
86792 deg
ZDOT = -4763
256690 TA = 79
20598
MA = 78
86012
Ha = 220
734 n
mi
Hp = 200
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19261373
55 X = -5896179
91
Y = 2930182
05 feet Y = 827326
30 meter
Z = 10645853
71 Z = 3216274
74
XDOT = -11200
192686 XDOT = -3334
971061
YDOT = -16270
544491 feet/sec YDOT = -4996
996516 meter/sec
ZDOT = -15627
482580 ZDOT = -4779
649115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17374830
66 X = -5295848
38
Y = -8954593
36 feet Y = -2729360
06 meter
Z = 10528589
48 Z = 3209114
08
XDOT = -111
312571 XDOT = -33
928071
YDOT = -18425
392566 feet/sec YDOT = -5616
059654 meter/sec
ZDOT = -15694
257147 ZDOT = -4783
609579
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 12046
53878659
00016717 00000-0 10270-3 0 9023
2 25544 51
6394 17
2313 0020611 45
7091 314
5751 15
58912765 38896
Satellite: ISS
Catalog Number: 25544
Epoch time: 12046
53878659 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 17
2313 deg
Eccentricity:
0020611
Arg of perigee: 45
7091 deg
Mean anomaly: 314
5751 deg
Mean motion: 15
58912765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 323
Coasting Arc #4 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2012/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6646831
54 A = 6775384
67 meter
Y = 1217699
23 meter E =
0032333
Z = -223457
60 I = 51
73342
XDOT = -680
718658 Wp = 47
18930
YDOT = 4717
406039 meter/sec RA = 11
87616 deg
ZDOT = 6030
024521 TA = 310
39813
MA = 310
67986
Ha = 220
710 n
mi
Hp = 200
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21807190
10 X = 6633806
47
Y = 3995076
22 feet Y = 1291955
37 meter
Z = -733128
60 Z = -191199
84
XDOT = -2233
328930 XDOT = -762
710977
YDOT = 15477
053933 feet/sec YDOT = 4709
335345 meter/sec
ZDOT = 19783
545017 ZDOT = 6026
518558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15601884
02 X = 4755454
25
Y = 15756639
70 feet Y = 4802623
78 meter
Z = -600976
22 Z = -183177
55
XDOT = -9637
542366 XDOT = -2937
522913
YDOT = 10209
655820 feet/sec YDOT = 3111
903094 meter/sec
ZDOT = 19768
753851 ZDOT = 6025
516174
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 12047
50035459
00016717 00000-0 10270-3 0 9035
2 25544 51
6395 12
4035 0020587 49
7328 310
5624 15
58935961 39040
Satellite: ISS
Catalog Number: 25544
Epoch time: 12047
50035459 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 12
4035 deg
Eccentricity:
0020587
Arg of perigee: 49
7328 deg
Mean anomaly: 310
5624 deg
Mean motion: 15
58935961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 309
Coasting Arc #5 (Orbit 3919)
---------------------------------------
Vector Time (GMT): 2012/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5308422
31 A = 6771487
81 meter
Y = -3005435
11 meter E =
0023390
Z = -2971624
56 I = 51
69171
XDOT = 4707
768160 Wp = 61
91442
YDOT = -3401
449240 meter/sec RA = 6
88357 deg
ZDOT = -4988
898404 TA = 152
01061
MA = 151
88463
Ha = 220
719 n
mi
Hp = 200
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17416083
71 X = -5259985
27
Y = -9860351
42 feet Y = -3064526
34 meter
Z = -9749424
39 Z = -2997294
35
XDOT = 15445
433597 XDOT = 4769
688317
YDOT = -11159
610366 feet/sec YDOT = -3348
457870 meter/sec
ZDOT = -16367
776916 ZDOT = -4965
878423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8900801
22 X = -2712964
21
Y = -17867964
25 feet Y = -5446155
50 meter
Z = -9854408
62 Z = -3003623
75
XDOT = 17824
086920 XDOT = 5432
781693
YDOT = 61
446479 feet/sec YDOT = 18
728887 meter/sec
ZDOT = -16273
091898 ZDOT = -4960
038411
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 12048
52601258
00016717 00000-0 10270-3 0 9045
2 25544 51
6404 7
2521 0020642 53
0624 307
2418 15
58956742 39204
Satellite: ISS
Catalog Number: 25544
Epoch time: 12048
52601258 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 7
2521 deg
Eccentricity:
0020642
Arg of perigee: 53
0624 deg
Mean anomaly: 307
2418 deg
Mean motion: 15
58956742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 283
Coasting Arc #6 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2012/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2203794
14 A = 6764540
65 meter
Y = 4003790
11 meter E =
0023407
Z = 4965681
96 I = 51
63897
XDOT = -7269
822058 Wp = 69
78744
YDOT = 1415
443189 meter/sec RA = 1
85746 deg
ZDOT = 2085
119490 TA = 359
99360
MA = 359
99363
Ha = 220
581 n
mi
Hp = 200
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7230295
72 X = 2134737
67
Y = 13135794
32 feet Y = 4028048
27 meter
Z = 16291607
48 Z = 4976219
79
XDOT = -23851
122239 XDOT = -7295
238281
YDOT = 4643
842485 feet/sec YDOT = 1334
005487 meter/sec
ZDOT = 6840
943209 ZDOT = 2049
742240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1156307
74 X = -352442
60
Y = 14902718
95 feet Y = 4542348
74 meter
Z = 16334462
45 Z = 4978744
15
XDOT = -21491
192342 XDOT = -6550
515426
YDOT = -9006
567522 feet/sec YDOT = -2745
201781 meter/sec
ZDOT = 6695
767737 ZDOT = 2040
870006
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 12049
55165466
00016717 00000-0 10270-3 0 9056
2 25544 51
6408 2
1023 0020411 56
7981 303
5128 15
59005638 39363
Satellite: ISS
Catalog Number: 25544
Epoch time: 12049
55165466 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 2
1023 deg
Eccentricity:
0020411
Arg of perigee: 56
7981 deg
Mean anomaly: 303
5128 deg
Mean motion: 15
59005638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 293
Coasting Arc #7 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2012/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1600588
72 A = 6764192
15 meter
Y = -4152083
49 meter E =
0031800
Z = -5119226
52 I = 51
60703
XDOT = 7428
688200 Wp = 76
33488
YDOT = 876
827694 meter/sec RA = 356
80513 deg
ZDOT = 1627
331176 TA = 209
31284
MA = 209
49161
Ha = 220
739 n
mi
Hp = 200
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5251275
33 X = 1671766
51
Y = -13622321
17 feet Y = -4133786
95 meter
Z = -16795362
59 Z = -5111278
11
XDOT = 24372
336613 XDOT = 7410
426247
YDOT = 2876
731280 feet/sec YDOT = 959
797822 meter/sec
ZDOT = 5339
013046 ZDOT = 1663
373954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11750791
88 X = 3581641
37
Y = -8727436
91 feet Y = -2660122
77 meter
Z = -16762412
30 Z = -5109183
27
XDOT = 18494
366517 XDOT = 5637
082914
YDOT = 14463
060132 feet/sec YDOT = 4408
340728 meter/sec
ZDOT = 5486
714738 ZDOT = 1672
350652
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 12050
51318324
00016717 00000-0 10270-3 0 9068
2 25544 51
6411 357
2732 0020531 60
2223 300
0971 15
58979706 39510
Satellite: ISS
Catalog Number: 25544
Epoch time: 12050
51318324 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 357
2732 deg
Eccentricity:
0020531
Arg of perigee: 60
2223 deg
Mean anomaly: 300
0971 deg
Mean motion: 15
58979706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 282
Coasting Arc #8 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2012/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4928636
23 A = 6770750
92 meter
Y = 3307645
27 meter E =
0032345
Z = 3239994
10 I = 51
59966
XDOT = -5205
584801 Wp = 74
66493
YDOT = -3053
706947 meter/sec RA = 351
76955 deg
ZDOT = -4753
293139 TA = 67
64669
MA = 67
30422
Ha = 220
777 n
mi
Hp = 199
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16170066
36 X = -4980995
38
Y = 10851854
56 feet Y = 3252237
66 meter
Z = 10629901
91 Z = 3215924
33
XDOT = -17078
690291 XDOT = -5147
960994
YDOT = -10018
723580 feet/sec YDOT = -3111
597108 meter/sec
ZDOT = -15594
793764 ZDOT = -4778
440744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19504285
87 X = -5944906
33
Y = 954412
98 feet Y = 290905
08 meter
Z = 10530932
37 Z = 3209828
19
XDOT = -9339
654509 XDOT = -2846
726694
YDOT = -15907
015805 feet/sec YDOT = -4848
458417 meter/sec
ZDOT = -15697
635031 ZDOT = -4784
639157
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 12051
53879783
00016717 00000-0 10270-3 0 9073
2 25544 51
6417 352
1223 0020554 63
9961 296
3308 15
59021872 39670
Satellite: ISS
Catalog Number: 25544
Epoch time: 12051
53879783 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 352
1223 deg
Eccentricity:
0020554
Arg of perigee: 63
9961 deg
Mean anomaly: 296
3308 deg
Mean motion: 15
59021872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 327
Coasting Arc #9 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2012/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6545393
00 A = 6775124
13 meter
Y = -1696877
55 meter E =
0031741
Z = -193575
42 I = 51
58442
XDOT = 1344
542771 Wp = 58
58987
YDOT = 4584
685375 meter/sec RA = 346
76706 deg
ZDOT = 6015
803600 TA = 299
31709
MA = 299
63387
Ha = 220
741 n
mi
Hp = 199
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21474386
50 X = 6564821
68
Y = -5567183
57 feet Y = -1623574
31 meter
Z = -635089
95 Z = -161731
73
XDOT = 4411
229565 XDOT = 1263
953347
YDOT = 15041
618684 feet/sec YDOT = 4599
270774 meter/sec
ZDOT = 19736
888453 ZDOT = 6022
139030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21386525
80 X = 6518613
06
Y = 5908320
30 feet Y = 1800856
03 meter
Z = -504393
67 Z = -153739
19
XDOT = -3367
554721 XDOT = -1026
430679
YDOT = 13615
148591 feet/sec YDOT = 4149
897290 meter/sec
ZDOT = 19762
472460 ZDOT = 6023
601606
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 12052
50029822
00016717 00000-0 10270-3 0 9083
2 25544 51
6417 347
2943 0020515 67
5226 292
8099 15
59026045 39827
Satellite: ISS
Catalog Number: 25544
Epoch time: 12052
50029822 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 347
2943 deg
Eccentricity:
0020515
Arg of perigee: 67
5226 deg
Mean anomaly: 292
8099 deg
Mean motion: 15
59026045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 314
Coasting Arc #10 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2012/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6045918
71 A = 6771008
62 meter
Y = -539777
45 meter E =
0024344
Z = -3027701
62 I = 51
54284
XDOT = 2910
346871 Wp = 77
08423
YDOT = -5084
247498 meter/sec RA = 341
76378 deg
ZDOT = -4933
340542 TA = 137
66625
MA = 137
47813
Ha = 220
686 n
mi
Hp = 199
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19835691
32 X = -6024725
93
Y = -1770923
40 feet Y = -607268
45 meter
Z = -9933404
26 Z = -3057020
18
XDOT = 9548
382123 XDOT = 2990
948126
YDOT = -16680
602027 feet/sec YDOT = -5051
252021 meter/sec
ZDOT = -16185
500467 ZDOT = -4919
006278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16438812
90 X = -5010550
17
Y = -11133501
86 feet Y = -3393491
37 meter
Z = -10053551
94 Z = -3064322
63
XDOT = 15710
674680 XDOT = 4788
613643
YDOT = -8717
525384 feet/sec YDOT = -2657
101737 meter/sec
ZDOT = -16126
308889 ZDOT = -4915
298949
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 12053
52588403
00016717 00000-0 10270-3 0 9092
2 25544 51
6427 342
1430 0020548 71
3427 288
9957 15
59067124 39984
Satellite: ISS
Catalog Number: 25544
Epoch time: 12053
52588403 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 342
1430 deg
Eccentricity:
0020548
Arg of perigee: 71
3427 deg
Mean anomaly: 288
9957 deg
Mean motion: 15
59067124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 330
Coasting Arc #11 (Orbit 4013)
---------------------------------------
Vector Time (GMT): 2012/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3598490
22 A = 6764100
12 meter
Y = 2773741
54 meter E =
0024499
Z = 4989289
58 I = 51
49117
XDOT = -6061
422448 Wp = 84
91700
YDOT = 4312
150824 meter/sec RA = 336
72552 deg
ZDOT = 1968
297996 TA = 345
96885
MA = 346
03679
Ha = 220
507 n
mi
Hp = 199
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11806070
28 X = 3542969
88
Y = 9100201
90 feet Y = 2813672
18 meter
Z = 16369060
29 Z = 5006635
37
XDOT = -19886
556588 XDOT = -6118
752643
YDOT = 14147
476458 feet/sec YDOT = 4244
047920 meter/sec
ZDOT = 6457
670590 ZDOT = 1938
712761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6062548
91 X = 1847864
91
Y = 13532078
12 feet Y = 4124577
41 meter
Z = 16439935
14 Z = 5010892
23
XDOT = -23248
526164 XDOT = -7086
150775
YDOT = 2693
612163 feet/sec YDOT = 821
012987 meter/sec
ZDOT = 6336
032501 ZDOT = 1931
222706
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 12054
55145375
00016717 00000-0 10270-3 0 9105
2 25544 51
6424 336
9929 0020363 75
3496 284
9915 15
59109712 40140
Satellite: ISS
Catalog Number: 25544
Epoch time: 12054
55145375 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 336
9929 deg
Eccentricity:
0020363
Arg of perigee: 75
3496 deg
Mean anomaly: 284
9915 deg
Mean motion: 15
59109712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4014
Checksum: 319
Coasting Arc #12 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2012/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -141726
07 A = 6764044
54 meter
Y = -4509415
90 meter E =
0032857
Z = -5067684
97 I = 51
46348
XDOT = 7104
106029 Wp = 87
96096
YDOT = -2216
288481 meter/sec RA = 331
66206 deg
ZDOT = 1784
632269 TA = 199
32185
MA = 199
44672
Ha = 220
659 n
mi
Hp = 199
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -464980
55 X = -66673
07
Y = -14794671
60 feet Y = -4510581
69 meter
Z = -16626263
03 Z = -5068190
66
XDOT = 23307
434479 XDOT = 7119
691819
YDOT = -7271
287666 feet/sec YDOT = -2136
758641 meter/sec
ZDOT = 5855
092747 ZDOT = 1819
181233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6396983
71 X = 1949800
64
Y = -13346181
92 feet Y = -4067916
25 meter
Z = -16627963
33 Z = -5068203
22
XDOT = 23061
434857 XDOT = 7029
125344
YDOT = 3627
778116 feet/sec YDOT = 1105
746770 meter/sec
ZDOT = 5996
894330 ZDOT = 1827
853392
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
51291415
00016717 00000-0 10270-3 0 9110
2 25544 51
6428 332
1638 0020445 78
5800 281
7650 15
59094892 40293
Satellite: ISS
Catalog Number: 25544
Epoch time: 12055
51291415 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 332
1638 deg
Eccentricity:
0020445
Arg of perigee: 78
5800 deg
Mean anomaly: 281
7650 deg
Mean motion: 15
59094892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 307
Coasting Arc #13 (Orbit 4044)
---------------------------------------
Vector Time (GMT): 2012/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3229292
08 A = 6770874
45 meter
Y = 5072025
68 meter E =
0033328
Z = 3086135
73 I = 51
45969
XDOT = -5896
817270 Wp = 87
22338
YDOT = -761
676875 meter/sec RA = 326
61737 deg
ZDOT = -4871
547829 TA = 57
05872
MA = 56
73865
Ha = 220
694 n
mi
Hp = 199
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10594790
27 X = -3300760
04
Y = 16640504
19 feet Y = 5035514
46 meter
Z = 10125117
23 Z = 3070274
06
XDOT = -19346
513353 XDOT = -5864
197200
YDOT = -2498
939879 feet/sec YDOT = -827
436844 meter/sec
ZDOT = -15982
768467 ZDOT = -4900
114621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16878448
39 X = -5144551
07
Y = 10275926
02 feet Y = 3132102
25 meter
Z = 10059686
07 Z = 3066192
31
XDOT = -15449
697464 XDOT = -4709
067787
YDOT = -9463
555077 feet/sec YDOT = -2884
491587 meter/sec
ZDOT = -16099
796816 ZDOT = -4907
218069
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
53845654
00016717 00000-0 10270-3 0 9124
2 25544 51
6424 327
0125 0020473 82
5795 277
7686 15
59111084 40457
Satellite: ISS
Catalog Number: 25544
Epoch time: 12056
53845654 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 327
0125 deg
Eccentricity:
0020473
Arg of perigee: 82
5795 deg
Mean anomaly: 277
7686 deg
Mean motion: 15
59111084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4045
Checksum: 315
Coasting Arc #14 (Orbit 4060)
---------------------------------------
Vector Time (GMT): 2012/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5317663
88 A = 6774815
38 meter
Y = -4186205
01 meter E =
0030835
Z = 27234
31 I = 51
44868
XDOT = 2923
498451 Wp = 70
72823
YDOT = 3788
764334 meter/sec RA = 321
60551 deg
ZDOT = 6004
723477 TA = 289
56660
MA = 289
89928
Ha = 220
601 n
mi
Hp = 199
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17446403
82 X = 5363947
35
Y = -13734268
40 feet Y = -4126480
82 meter
Z = 89351
42 Z = 53179
83
XDOT = 9591
530352 XDOT = 2851
745148
YDOT = 12430
329180 feet/sec YDOT = 3821
056062 meter/sec
ZDOT = 19700
536341 ZDOT = 6018
750916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21619544
33 X = 6589637
11
Y = -5056875
62 feet Y = -1541335
69 meter
Z = 196035
77 Z = 59751
70
XDOT = 2949
249870 XDOT = 898
931360
YDOT = 13695
838701 feet/sec YDOT = 4174
491636 meter/sec
ZDOT = 19757
720577 ZDOT = 6022
153232
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
56398351
00016717 00000-0 10270-3 0 9136
2 25544 51
6426 321
8616 0020384 86
0535 274
2950 15
59135721 40616
Satellite: ISS
Catalog Number: 25544
Epoch time: 12057
56398351 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 321
8616 deg
Eccentricity:
0020384
Arg of perigee: 86
0535 deg
Mean anomaly: 274
2950 deg
Mean motion: 15
59135721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4061
Checksum: 306
Coasting Arc #15 (Orbit 4075)
---------------------------------------
Vector Time (GMT): 2012/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5675705
03 A = 6770188
68 meter
Y = 1816818
57 meter E =
0024869
Z = -3233847
44 I = 51
41086
XDOT = 781
689703 Wp = 90
65590
YDOT = -5959
036523 meter/sec RA = 316
59049 deg
ZDOT = -4751
779359 TA = 126
94740
MA = 126
71940
Ha = 220
485 n
mi
Hp = 199
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18621079
48 X = -5679890
06
Y = 5960690
84 feet Y = 1753325
67 meter
Z = -10609735
71 Z = -3261429
83
XDOT = 2564
598763 XDOT = 871
349622
YDOT = -19550
644762 feet/sec YDOT = -5949
794250 meter/sec
ZDOT = -15589
827294 ZDOT = -4747
763724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19373960
00 X = -5905183
01
Y = -2123521
25 feet Y = -647249
28 meter
Z = -10722931
47 Z = -3268349
51
XDOT = 10244
784882 XDOT = 3122
610432
YDOT = -15355
665157 feet/sec YDOT = -4680
406740 meter/sec
ZDOT = -15572
884378 ZDOT = -4746
615158
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
52540080
00016717 00000-0 10270-3 0 9142
2 25544 51
6431 317
0317 0020261 89
7659 270
5818 15
59159775 40761
Satellite: ISS
Catalog Number: 25544
Epoch time: 12058
52540080 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 317
0317 deg
Eccentricity:
0020261
Arg of perigee: 89
7659 deg
Mean anomaly: 270
5818 deg
Mean motion: 15
59159775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4076
Checksum: 317
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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