[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 28th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
278/21:06:37
060 -8
0 10
1 10
1
N/A -0
3 -0
1 211
4
000/00:03:14
119 -6
2 -0
1 207
1
Coasting Arc #1 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2011/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3237507
10 A = 6757577
59 meter
Y = -3351142
78 meter E =
0009425
Z = -4899466
01 I = 51
69041
XDOT = 6656
870628 Wp = 165
76386
YDOT = 3047
097386 meter/sec RA = 10
18241 deg
ZDOT = 2306
621788 TA = 126
79688
MA = 126
71036
Ha = 209
348 n
mi
Hp = 205
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10621742
46 X = 3298540
40
Y = -10994562
94 feet Y = -3314598
39 meter
Z = -16074363
56 Z = -4883589
47
XDOT = 21840
126731 XDOT = 6611
097451
YDOT = 9997
038668 feet/sec YDOT = 3121
282966 meter/sec
ZDOT = 7567
656784 ZDOT = 2338
849343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9893808
58 X = -3015632
85
Y = 11742889
09 feet Y = 3579232
60 meter
Z = -16009500
26 Z = -4879695
68
XDOT = -21604
751240 XDOT = -6585
128178
YDOT = -7670
892402 feet/sec YDOT = -2338
088004 meter/sec
ZDOT = 7698
739386 ZDOT = 2346
575765
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 11269
51192544
00016717 00000-0 10270-3 0 9007
2 25544 51
6414 10
6630 0010861 238
8473 121
1619 15
61577564 16735
Satellite: ISS
Catalog Number: 25544
Epoch time: 11269
51192544 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 10
6630 deg
Eccentricity:
0010861
Arg of perigee: 238
8473 deg
Mean anomaly: 121
1619 deg
Mean motion: 15
61577564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 296
Coasting Arc #2 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2011/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6377223
86 A = 6766123
66 meter
Y = 1010575
98 meter E =
0010797
Z = 1997889
24 I = 51
68880
XDOT = -2486
702639 Wp = 161
40205
YDOT = -4654
313644 meter/sec RA = 5
14573 deg
ZDOT = -5584
980937 TA = 356
46717
MA = 356
47479
Ha = 209
134 n
mi
Hp = 205
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20922650
47 X = -6397755
81
Y = 3315538
00 feet Y = 939147
42 meter
Z = 6554754
73 Z = 1966858
44
XDOT = -8158
473225 XDOT = -2407
341318
YDOT = -15270
057887 feet/sec YDOT = -4681
678463 meter/sec
ZDOT = -18323
428271 ZDOT = -5596
868064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20580456
03 X = 6272923
00
Y = -5180395
71 feet Y = -1578984
61 meter
Z = 6428315
06 Z = 1959350
43
XDOT = 9005
777878 XDOT = 2744
961097
YDOT = 12987
804708 feet/sec YDOT = 3958
682875 meter/sec
ZDOT = -18371
563688 ZDOT = -5599
652612
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 11270
53585060
00016717 00000-0 10270-3 0 9011
2 25544 51
6412 5
5016 0010809 242
7905 117
2151 15
61576173 16899
Satellite: ISS
Catalog Number: 25544
Epoch time: 11270
53585060 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 5
5016 deg
Eccentricity:
0010809
Arg of perigee: 242
7905 deg
Mean anomaly: 117
2151 deg
Mean motion: 15
61576173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 284
Coasting Arc #3 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2011/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6201717
65 A = 6765594
49 meter
Y = 1684974
71 meter E =
0003304
Z = 2110937
55 I = 51
65804
XDOT = -3067
303030 Wp = 79
78918
YDOT = 4361
195023 meter/sec RA =
14172 deg
ZDOT = 5523
500211 TA = 303
65666
MA = 303
68817
Ha = 208
637 n
mi
Hp = 205
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20346842
70 X = 6172160
32
Y = 5528132
26 feet Y = 1754161
09 meter
Z = 6925648
12 Z = 2140993
89
XDOT = -10063
330150 XDOT = -3142
675315
YDOT = 14308
382621 feet/sec YDOT = 4326
473742 meter/sec
ZDOT = 18121
719854 ZDOT = 5508
415500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20778701
17 X = -6333348
12
Y = -3330292
03 feet Y = -1015073
01 meter
Z = 7047949
25 Z = 2148214
93
XDOT = 8344
627536 XDOT = 2543
442473
YDOT = -13797
791351 feet/sec YDOT = -4205
566804 meter/sec
ZDOT = 18060
024805 ZDOT = 5504
695561
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 11271
55974409
00016717 00000-0 10270-3 0 9024
2 25544 51
6417
3390 0010721 247
5734 112
4287 15
61644591 17054
Satellite: ISS
Catalog Number: 25544
Epoch time: 11271
55974409 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node:
3390 deg
Eccentricity:
0010721
Arg of perigee: 247
5734 deg
Mean anomaly: 112
4287 deg
Mean motion: 15
61644591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 292
Coasting Arc #4 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2011/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2724937
85 A = 6756937
16 meter
Y = -3705471
41 meter E =
0001986
Z = -4951501
07 I = 51
59814
XDOT = 7008
208674 Wp = 89
87805
YDOT = -2300
394876 meter/sec RA = 355
09790 deg
ZDOT = -2136
023593 TA = 159
33606
MA = 159
32803
Ha = 208
256 n
mi
Hp = 205
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8940084
79 X = -2659246
14
Y = -12157058
43 feet Y = -3735576
44 meter
Z = -16245082
24 Z = -4964579
14
XDOT = 22992
810609 XDOT = 7043
787845
YDOT = -7547
227285 feet/sec YDOT = -2221
826040 meter/sec
ZDOT = -7007
951419 ZDOT = -2101
890586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10278998
90 X = 3133038
86
Y = 10969758
72 feet Y = 3343582
46 meter
Z = -16298112
11 Z = -4967664
57
XDOT = -21123
215229 XDOT = -6438
356002
YDOT = 9591
458901 feet/sec YDOT = 2923
476673 meter/sec
ZDOT = -6868
812119 ZDOT = -2093
613934
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 11272
51961825
00016717 00000-0 10270-3 0 9030
2 25544 51
6410 355
5002 0010769 251
7681 108
2304 15
61666183 17203
Satellite: ISS
Catalog Number: 25544
Epoch time: 11272
51961825 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 355
5002 deg
Eccentricity:
0010769
Arg of perigee: 251
7681 deg
Mean anomaly: 108
2304 deg
Mean motion: 15
61666183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 287
Coasting Arc #5 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2011/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2160410
06 A = 6757449
54 meter
Y = 4245002
60 meter E =
0004047
Z = 4797094
37 I = 51
57056
XDOT = -7199
338596 Wp = 285
11445
YDOT = -785
376547 meter/sec RA = 350
01570 deg
ZDOT = -2548
048253 TA = 189
94844
MA = 189
95645
Ha = 207
776 n
mi
Hp = 205
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7087959
53 X = -2231021
71
Y = 13927173
90 feet Y = 4220449
04 meter
Z = 15738498
60 Z = 4786427
19
XDOT = -23619
877283 XDOT = -7177
643146
YDOT = -2576
694709 feet/sec YDOT = -865
762798 meter/sec
ZDOT = -8359
738363 ZDOT = -2582
970400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5149489
01 X = 1569564
25
Y = -14800737
26 feet Y = -4511264
72 meter
Z = 15694795
97 Z = 4783773
81
XDOT = 22617
778891 XDOT = 6893
899006
YDOT = -1143
623334 feet/sec YDOT = -348
576392 meter/sec
ZDOT = -8501
897332 ZDOT = -2591
378307
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 11273
54345369
00016717 00000-0 10270-3 0 9044
2 25544 51
6412 350
3374 0010671 256
5383 103
4585 15
61757307 17368
Satellite: ISS
Catalog Number: 25544
Epoch time: 11273
54345369 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 350
3374 deg
Eccentricity:
0010671
Arg of perigee: 256
5383 deg
Mean anomaly: 103
4585 deg
Mean motion: 15
61757307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 306
Coasting Arc #6 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2011/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5830219
82 A = 6766100
30 meter
Y = -2968872
19 meter E =
0007256
Z = -1708507
01 I = 51
56883
XDOT = 3566
635036 Wp = 307
77232
YDOT = 3720
430485 meter/sec RA = 344
97244 deg
ZDOT = 5693
888226 TA = 33
41112
MA = 33
36536
Ha = 207
307 n
mi
Hp = 205
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19128017
79 X = 5871284
73
Y = -9740394
32 feet Y = -2903445
56 meter
Z = -5605337
96 Z = -1680083
61
XDOT = 11701
558517 XDOT = 3497
107167
YDOT = 12206
136761 feet/sec YDOT = 3759
926249 meter/sec
ZDOT = 18680
735649 ZDOT = 5711
046109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17383658
86 X = -5298539
22
Y = 12643218
11 feet Y = 3853652
88 meter
Z = -5489407
98 Z = -1673171
55
XDOT = -12448
348281 XDOT = -3794
256556
YDOT = -8957
071595 feet/sec YDOT = -2730
115422 meter/sec
ZDOT = 18750
370291 ZDOT = 5715
112865
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 11274
50327378
00016717 00000-0 10270-3 0 9052
2 25544 51
6404 345
4974 0010593 261
0476 98
9482 15
61737879 17510
Satellite: ISS
Catalog Number: 25544
Epoch time: 11274
50327378 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 345
4974 deg
Eccentricity:
0010593
Arg of perigee: 261
0476 deg
Mean anomaly: 98
9482 deg
Mean motion: 15
61737879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 336
Coasting Arc #7 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2011/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6302435
17 A = 6764477
48 meter
Y = 242354
18 meter E =
0007818
Z = -2431999
35 I = 51
53452
XDOT = 1864
062115 Wp = 233
69153
YDOT = -5196
729596 meter/sec RA = 339
95909 deg
ZDOT = -5341
112404 TA = 333
66303
MA = 333
70275
Ha = 206
704 n
mi
Hp = 205
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20677280
75 X = -6292862
51
Y = 795125
28 feet Y = 171929
95 meter
Z = -7979000
48 Z = -2462593
56
XDOT = 6115
689354 XDOT = 1947
980783
YDOT = -17049
637783 feet/sec YDOT = -5175
415464 meter/sec
ZDOT = -17523
334658 ZDOT = -5331
852719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20172198
85 X = 6148486
21
Y = -4388699
54 feet Y = -1337675
62 meter
Z = -8103599
32 Z = -2469977
07
XDOT = -3464
821507 XDOT = -1056
077595
YDOT = 16404
523561 feet/sec YDOT = 5000
098781 meter/sec
ZDOT = -17485
300002 ZDOT = -5329
519441
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 11275
52705267
00016717 00000-0 10270-3 0 9063
2 25544 51
6396 340
3344 0010416 264
4905 95
5064 15
61810801 17676
Satellite: ISS
Catalog Number: 25544
Epoch time: 11275
52705267 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 340
3344 deg
Eccentricity:
0010416
Arg of perigee: 264
4905 deg
Mean anomaly: 95
5064 deg
Mean motion: 15
61810801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1767
Checksum: 303
Coasting Arc #8 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2011/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3426357
01 A = 6755789
52 meter
Y = 2859141
50 meter E =
0007069
Z = 5078338
73 I = 51
47821
XDOT = -6107
438718 Wp = 243
17204
YDOT = 4336
217489 meter/sec RA = 334
89879 deg
ZDOT = 1678
040308 TA = 190
59481
MA = 190
60971
Ha = 206
384 n
mi
Hp = 204
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11241328
78 X = 3369461
13
Y = 9380385
48 feet Y = 2897139
17 meter
Z = 16661216
30 Z = 5094845
74
XDOT = -20037
528601 XDOT = -6163
624879
YDOT = 14226
435331 feet/sec YDOT = 4267
606274 meter/sec
ZDOT = 5505
381587 ZDOT = 1648
233634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12732571
14 X = -3880887
68
Y = -7071232
08 feet Y = -2155311
54 meter
Z = 16728255
80 Z = 5098772
37
XDOT = 16454
782424 XDOT = 5015
417683
YDOT = -16882
291420 feet/sec YDOT = -5145
722425 meter/sec
ZDOT = 5383
731697 ZDOT = 1640
961421
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 11276
55079987
00016717 00000-0 10270-3 0 9071
2 25544 51
6401 335
1708 0010451 268
8842 91
1117 15
61872506 17835
Satellite: ISS
Catalog Number: 25544
Epoch time: 11276
55079987 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 335
1708 deg
Eccentricity:
0010451
Arg of perigee: 268
8842 deg
Mean anomaly: 91
1117 deg
Mean motion: 15
61872506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 320
Coasting Arc #9 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2011/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1123045
84 A = 6757901
57 meter
Y = -4858194
31 meter E =
0002982
Z = -4562132
71 I = 51
45795
XDOT = 6944
483623 Wp = 195
20400
YDOT = -1245
524665 meter/sec RA = 329
80760 deg
ZDOT = 3032
579953 TA = 105
13620
MA = 105
10321
Ha = 206
386 n
mi
Hp = 205
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3684533
60 X = 1199449
69
Y = -15938957
72 feet Y = -4845208
73 meter
Z = -14967627
02 Z = -4556491
15
XDOT = 22783
738919 XDOT = 6943
163454
YDOT = -4086
367010 feet/sec YDOT = -1167
874444 meter/sec
ZDOT = 9949
409294 ZDOT = 3066
313125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -367043
11 X = -111874
74
Y = 16376435
70 feet Y = 4991537
60 meter
Z = -14944351
86 Z = -4555038
45
XDOT = -20177
110329 XDOT = -6149
983228
YDOT = 8762
374222 feet/sec YDOT = 2670
771663 meter/sec
ZDOT = 10086
853781 ZDOT = 3074
473032
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 11277
51053718
00016717 00000-0 10270-3 0 9083
2 25544 51
6396 330
3299 0010239 273
3762 86
6224 15
61915019 17987
Satellite: ISS
Catalog Number: 25544
Epoch time: 11277
51053718 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 330
3299 deg
Eccentricity:
0010239
Arg of perigee: 273
3762 deg
Mean anomaly: 86
6224 deg
Mean motion: 15
61915019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 324
Coasting Arc #10 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2011/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4837109
98 A = 6766038
60 meter
Y = 4573709
88 meter E =
0006131
Z = 1186052
23 I = 51
46071
XDOT = -4097
313282 Wp = 165
69208
YDOT = -2814
996934 meter/sec RA = 324
76209 deg
ZDOT = -5854
233251 TA = 1
34927
MA = 1
34762
Ha = 206
808 n
mi
Hp = 205
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15869783
40 X = -4893656
22
Y = 15005609
84 feet Y = 4519302
26 meter
Z = 3891247
47 Z = 1162415
95
XDOT = -13442
628878 XDOT = -4037
092132
YDOT = -9235
554247 feet/sec YDOT = -2860
479237 meter/sec
ZDOT = -19206
802003 ZDOT = -5873
991529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12102218
80 X = 3688756
29
Y = -18201554
23 feet Y = -5547833
73 meter
Z = 3794717
70 Z = 1156629
96
XDOT = 13738
036361 XDOT = 4187
353483
YDOT = 5112
948015 feet/sec YDOT = 1558
426555 meter/sec
ZDOT = -19287
088463 ZDOT = -5878
704563
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 11278
53422658
00016717 00000-0 10270-3 0 9090
2 25544 51
6401 325
1663 0010232 278
0803 81
9193 15
61976467 18148
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
53422658 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 325
1663 deg
Eccentricity:
0010232
Arg of perigee: 278
0803 deg
Mean anomaly: 81
9193 deg
Mean motion: 15
61976467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 312
Coasting Arc #11 (Orbit 1819)
---------------------------------------
Vector Time (GMT): 2011/278/21:08:14
119
Vector Time (MET): N/A
Weight (LBS) : 870493
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3332462
30 A = 6769055
45 meter
Y = 5227778
05 meter E =
0011002
Z = 2699770
16 I = 51
44293
XDOT = -5613
946923 Wp = 132
30723
YDOT = -908
551485 meter/sec RA = 322
82572 deg
ZDOT = -5164
098076 TA = 16
99091
MA = 16
95409
Ha = 211
366 n
mi
Hp = 207
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10933275
26 X = -3403787
64
Y = 17151502
79 feet Y = 5190113
80 meter
Z = 8857513
66 Z = 2683407
49
XDOT = -18418
461033 XDOT = -5578
283855
YDOT = -2980
811960 feet/sec YDOT = -971
131019 meter/sec
ZDOT = -16942
578990 ZDOT = -5191
283904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18015029
02 X = -5490980
85
Y = 9505303
13 feet Y = 2897216
39 meter
Z = 8790565
73 Z = 2679364
44
XDOT = -13771
638844 XDOT = -4197
595520
YDOT = -10311
020830 feet/sec YDOT = -3142
799149 meter/sec
ZDOT = -17053
227814 ZDOT = -5197
823838
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 11278
91816071
00016717 00000-0 10270-3 0 9100
2 25544 51
6402 323
2310 0006984 228
2219 131
8340 15
60066447 18207
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
91816071 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 323
2310 deg
Eccentricity:
0006984
Arg of perigee: 228
2219 deg
Mean anomaly: 131
8340 deg
Mean motion: 15
60066447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1820
Checksum: 281
Coasting Arc #12 (Orbit 1835)
---------------------------------------
Vector Time (GMT): 2011/279/21:08:14
119
Vector Time (MET): N/A
Weight (LBS) : 870493
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5409533
10 A = 6771650
79 meter
Y = -3975964
60 meter E =
0006607
Z = 861532
22 I = 51
42896
XDOT = 2242
287043 Wp = 55
93487
YDOT = 4339
939888 meter/sec RA = 317
81066 deg
ZDOT = 5920
620262 TA = 313
43468
MA = 313
48964
Ha = 211
050 n
mi
Hp = 207
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17747812
01 X = 5449405
90
Y = -13044503
29 feet Y = -3915248
88 meter
Z = 2826549
26 Z = 887908
89
XDOT = 7356
584788 XDOT = 2164
829047
YDOT = 14238
647926 feet/sec YDOT = 4364
581922 meter/sec
ZDOT = 19424
607159 ZDOT = 5931
324771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21808949
25 X = 6647367
73
Y = -2982201
50 feet Y = -908975
02 meter
Z = 2934192
34 Z = 894341
83
XDOT = -665
515937 XDOT = -202
849258
YDOT = 14377
522419 feet/sec YDOT = 4382
268833 meter/sec
ZDOT = 19467
938254 ZDOT = 5933
827580
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 11279
94304943
00016717 00000-0 10270-3 0 9115
2 25544 51
6404 318
0749 0006896 233
2402 126
8121 15
60111760 18366
Satellite: ISS
Catalog Number: 25544
Epoch time: 11279
94304943 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 318
0749 deg
Eccentricity:
0006896
Arg of perigee: 233
2402 deg
Mean anomaly: 126
8121 deg
Mean motion: 15
60111760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1836
Checksum: 295
Coasting Arc #13 (Orbit 1850)
---------------------------------------
Vector Time (GMT): 2011/280/21:08:14
119
Vector Time (MET): N/A
Weight (LBS) : 870493
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5333664
62 A = 6764752
37 meter
Y = 1019899
45 meter E =
0001790
Z = -4034011
28 I = 51
38528
XDOT = 1705
922398 Wp = 141
32585
YDOT = -6402
092984 meter/sec RA = 312
78036 deg
ZDOT = -3876
440034 TA = 88
42091
MA = 88
40040
Ha = 210
643 n
mi
Hp = 207
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17498899
66 X = -5325076
39
Y = 3346126
79 feet Y = 960302
76 meter
Z = -13234945
15 Z = -4059901
50
XDOT = 5596
858260 XDOT = 1796
216145
YDOT = -21004
242075 feet/sec YDOT = -6382
511842 meter/sec
ZDOT = -12717
979115 ZDOT = -3867
932691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16989168
95 X = -5178298
70
Y = -5096368
15 feet Y = -1553373
01 meter
Z = -13340427
17 Z = -4066162
20
XDOT = 14379
320812 XDOT = 4382
816984
YDOT = -14754
933877 feet/sec YDOT = -4497
303846 meter/sec
ZDOT = -12682
965193 ZDOT = -3865
767791
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 11280
90385670
00016717 00000-0 10270-3 0 9120
2 25544 51
6409 313
2417 0006922 237
2958 122
7531 15
60171949 18512
Satellite: ISS
Catalog Number: 25544
Epoch time: 11280
90385670 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 313
2417 deg
Eccentricity:
0006922
Arg of perigee: 237
2958 deg
Mean anomaly: 122
7531 deg
Mean motion: 15
60171949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1851
Checksum: 306
Coasting Arc #14 (Orbit 1866)
---------------------------------------
Vector Time (GMT): 2011/281/21:08:14
119
Vector Time (MET): N/A
Weight (LBS) : 870493
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3333980
44 A = 6759636
27 meter
Y = 2592787
54 meter E =
0004935
Z = 5280911
13 I = 51
34842
XDOT = -4702
927843 Wp = 227
73171
YDOT = 6066
885630 meter/sec RA = 307
70532 deg
ZDOT = -12
866257 TA = 222
37220
MA = 222
41032
Ha = 210
425 n
mi
Hp = 207
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10938256
04 X = 3279085
75
Y = 8506520
79 feet Y = 2629763
80 meter
Z = 17325823
92 Z = 5296974
06
XDOT = -15429
553291 XDOT = -4770
356914
YDOT = 19904
480414 feet/sec YDOT = 6013
917591 meter/sec
ZDOT = -42
212130 ZDOT = -35
877643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5880997
12 X = 1792527
92
Y = 12456111
60 feet Y = 3796622
82 meter
Z = 17391080
24 Z = 5300801
26
XDOT = -21797
051281 XDOT = -6643
741231
YDOT = 10466
519615 feet/sec YDOT = 3190
195179 meter/sec
ZDOT = -136
255394 ZDOT = -41
530644
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 11281
92869111
00016717 00000-0 10270-3 0 9131
2 25544 51
6405 308
0855 0006945 241
0364 119
0095 15
60231801 18670
Satellite: ISS
Catalog Number: 25544
Epoch time: 11281
92869111 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 308
0855 deg
Eccentricity:
0006945
Arg of perigee: 241
0364 deg
Mean anomaly: 119
0095 deg
Mean motion: 15
60231801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1867
Checksum: 295
Coasting Arc #15 (Orbit 1881)
---------------------------------------
Vector Time (GMT): 2011/282/21:08:14
119
Vector Time (MET): N/A
Weight (LBS) : 870493
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -314597
57 A = 6764746
07 meter
Y = -5446874
79 meter E =
0005046
Z = -4003415
48 I = 51
34783
XDOT = 5769
029432 Wp = 175
20042
YDOT = -3210
652241 meter/sec RA = 302
62862 deg
ZDOT = 3910
347087 TA = 135
55287
MA = 135
51237
Ha = 210
255 n
mi
Hp = 207
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1032144
26 X = -234218
12
Y = -17870324
10 feet Y = -5449943
84 meter
Z = -13134565
23 Z = -4004747
94
XDOT = 18927
261917 XDOT = 5785
506873
YDOT = -10533
635961 feet/sec YDOT = -3146
046841 meter/sec
ZDOT = 12829
222726 ZDOT = 3938
413670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6862089
96 X = 2091565
02
Y = -16528491
12 feet Y = -5037884
09 meter
Z = -13139684
60 Z = -4004975
87
XDOT = 20344
972474 XDOT = 6201
147610
YDOT = -1855
244276 feet/sec YDOT = -565
478455 meter/sec
ZDOT = 12943
678944 ZDOT = 3945
233342
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 11282
88944896
00016717 00000-0 10270-3 0 9142
2 25544 51
6404 303
2512 0006904 245
3801 114
6636 15
60249418 18826
Satellite: ISS
Catalog Number: 25544
Epoch time: 11282
88944896 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 303
2512 deg
Eccentricity:
0006904
Arg of perigee: 245
3801 deg
Mean anomaly: 114
6636 deg
Mean motion: 15
60249418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1882
Checksum: 312
Coasting Arc #16 (Orbit 1897)
---------------------------------------
Vector Time (GMT): 2011/283/21:08:14
119
Vector Time (MET): N/A
Weight (LBS) : 870493
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2545639
83 A = 6771342
13 meter
Y = 6217664
42 meter E =
0011512
Z = 780389
38 I = 51
35433
XDOT = -4730
907277 Wp = 157
62745
YDOT = -1189
970466 meter/sec RA = 297
59428 deg
ZDOT = -5932
962294 TA = 13
87735
MA = 13
84574
Ha = 210
108 n
mi
Hp = 207
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8351836
71 X = -2618768
82
Y = 20399161
48 feet Y = 6188788
72 meter
Z = 2560332
60 Z = 767844
17
XDOT = -15521
349335 XDOT = -4688
427536
YDOT = -3904
102578 feet/sec YDOT = -1242
637516 meter/sec
ZDOT = -19465
099389 ZDOT = -5955
842022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16102990
57 X = -4908191
53
Y = 15060987
02 feet Y = 4590588
84 meter
Z = 2508910
75 Z = 764716
00
XDOT = -11279
394264 XDOT = -3437
959372
YDOT = -8791
456064 feet/sec YDOT = -2679
635808 meter/sec
ZDOT = -19558
187281 ZDOT = -5961
335483
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 11283
91423040
00016717 00000-0 10270-3 0 9151
2 25544 51
6402 298
0949 0006876 247
4306 112
6122 15
60251447 18980
Satellite: ISS
Catalog Number: 25544
Epoch time: 11283
91423040 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 298
0949 deg
Eccentricity:
0006876
Arg of perigee: 247
4306 deg
Mean anomaly: 112
6122 deg
Mean motion: 15
60251447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1898
Checksum: 305
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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