[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 18th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22066 02 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 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
292/16:15:56
370 -1
1 5
9 5
9
N/A -5
7 -0
0 215
8
000/00:01:52
739 0
8 0
0 203
8
299/12:43:09
785 -5
7 7
3 7
3
N/A -4
5 -0
0 218
1
000/00:02:19
570 -0
1 0
0 204
7
Coasting Arc #1 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2011/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4246678
31 A = 6757953
30 meter
Y = -40201
51 meter E =
0016583
Z = -5263476
65 I = 51
27356
XDOT = -435
701263 Wp = 31
64166
YDOT = -7649
964814 meter/sec RA = 264
19425 deg
ZDOT = 424
455907 TA = 242
33965
MA = 242
50806
Ha = 213
840 n
mi
Hp = 202
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13932671
62 X = -4220343
71
Y = -131894
71 feet Y = -87543
34 meter
Z = -17268624
18 Z = -5284043
38
XDOT = -1429
466085 XDOT = -352
187431
YDOT = -25098
309757 feet/sec YDOT = -7654
370131 meter/sec
ZDOT = 1392
571874 ZDOT = 422
542273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12603475
18 X = 3841539
24
Y = -5691207
09 feet Y = -1734679
92 meter
Z = -17352368
46 Z = -5289001
91
XDOT = 11437
881496 XDOT = 3486
266280
YDOT = 21250
695150 feet/sec YDOT = 6477
211882 meter/sec
ZDOT = 1385
178826 ZDOT = 422
202506
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 11290
51528320
00016717 00000-0 10270-3 0 9006
2 25544 51
6378 264
9380 0016170 337
7557 22
2896 15
60833726 20019
Satellite: ISS
Catalog Number: 25544
Epoch time: 11290
51528320 = yrday
fracday
Element set: 900
Inclination: 51
6378 deg
RA of node: 264
9380 deg
Eccentricity:
0016170
Arg of perigee: 337
7557 deg
Mean anomaly: 22
2896 deg
Mean motion: 15
60833726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 299
Coasting Arc #2 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2011/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3759845
36 A = 6764137
86 meter
Y = 4339211
93 meter E =
0017505
Z = 3585345
27 I = 51
29906
XDOT = -2468
846043 Wp = 22
71224
YDOT = 5785
715603 meter/sec RA = 259
11166 deg
ZDOT = -4390
155904 TA = 114
54591
MA = 114
36334
Ha = 213
985 n
mi
Hp = 202
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12335450
66 X = 3693626
81
Y = 14236259
62 feet Y = 4380886
66 meter
Z = 11762943
80 Z = 3603449
89
XDOT = -8099
888593 XDOT = -2512
032700
YDOT = 18982
006571 feet/sec YDOT = 5757
865884 meter/sec
ZDOT = -14403
398636 ZDOT = -4402
254748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17242965
92 X = -5255656
01
Y = -7468594
73 feet Y = -2276427
67 meter
Z = 11836447
82 Z = 3607749
29
XDOT = -1605
282270 XDOT = -489
290036
YDOT = -19318
567602 feet/sec YDOT = -5888
299405 meter/sec
ZDOT = -14452
963710 ZDOT = -4405
263339
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 11291
53966511
00016717 00000-0 10270-3 0 9018
2 25544 51
6377 259
7788 0016259 341
3224 18
7334 15
60909556 20171
Satellite: ISS
Catalog Number: 25544
Epoch time: 11291
53966511 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 259
7788 deg
Eccentricity:
0016259
Arg of perigee: 341
3224 deg
Mean anomaly: 18
7334 deg
Mean motion: 15
60909556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 323
Coasting Arc #3 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2011/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1839475
79 A = 6769529
15 meter
Y = -6497870
43 meter E =
0024482
Z = 17143
75 I = 51
32439
XDOT = 4630
124239 Wp = 10
88106
YDOT = -1291
270672 meter/sec RA = 254
07734 deg
ZDOT = 6005
011674 TA = 349
30525
MA = 349
35722
Ha = 213
961 n
mi
Hp = 202
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6035025
56 X = -1766761
89
Y = -21318472
56 feet Y = -6518034
01 meter
Z = 56245
91 Z = 8384
31
XDOT = 15190
696321 XDOT = 4615
047800
YDOT = -4236
452336 feet/sec YDOT = -1239
577904 meter/sec
ZDOT = 19701
481870 ZDOT = 6027
468461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15005623
20 X = 4573713
95
Y = 16301312
98 feet Y = 4968640
20 meter
Z = 20897
13 Z = 6369
45
XDOT = -10349
958352 XDOT = -3154
667306
YDOT = 9486
385449 feet/sec YDOT = 2891
450285 meter/sec
ZDOT = 19793
001925 ZDOT = 6032
906987
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 11292
56401083
00016717 00000-0 10270-3 0 9021
2 25544 51
6376 254
6195 0016056 345
3820 14
6870 15
60970179 20334
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
56401083 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 254
6195 deg
Eccentricity:
0016056
Arg of perigee: 345
3820 deg
Mean anomaly: 14
6870 deg
Mean motion: 15
60970179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2033
Checksum: 299
Coasting Arc #4 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2011/292/16:16:52
739
Vector Time (MET): N/A
Weight (LBS) : 870891
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4387649
46 A = 6761247
50 meter
Y = -282985
05 meter E =
0014869
Z = -5138035
42 I = 51
29126
XDOT = -1109
985548 Wp = 20
22822
YDOT = -7470
730884 meter/sec RA = 253
16427 deg
ZDOT = 1374
251200 TA = 262
94942
MA = 263
11854
Ha = 215
813 n
mi
Hp = 203
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14395175
41 X = -4359199
08
Y = -928428
63 feet Y = -331891
52 meter
Z = -16857071
59 Z = -5159281
71
XDOT = -3641
684870 XDOT = -1033
039796
YDOT = -24510
271930 feet/sec YDOT = -7482
713152 meter/sec
ZDOT = 4508
698163 ZDOT = 1369
045979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 625037
86 X = 190511
54
Y = -14309723
46 feet Y = -4361603
71 meter
Z = -16943584
61 Z = -5164404
59
XDOT = 23382
980123 XDOT = 7127
132341
YDOT = -4234
927931 feet/sec YDOT = -1290
806033 meter/sec
ZDOT = 4487
870440 ZDOT = 1367
902910
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 11292
69205255
00016717 00000-0 10270-3 0 9039
2 25544 51
6412 253
9759 0018605 332
4020 27
6146 15
59884158 20355
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
69205255 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 253
9759 deg
Eccentricity:
0018605
Arg of perigee: 332
4020 deg
Mean anomaly: 27
6146 deg
Mean motion: 15
59884158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 308
Coasting Arc #5 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2011/293/16:16:52
739
Vector Time (MET): N/A
Weight (LBS) : 870891
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4384339
65 A = 6768141
10 meter
Y = 4062644
98 meter E =
0017056
Z = 3188833
48 I = 51
32403
XDOT = -1815
285797 Wp = 18
38673
YDOT = 5721
118033 meter/sec RA = 248
09905 deg
ZDOT = -4770
080398 TA = 124
53357
MA = 124
37245
Ha = 216
026 n
mi
Hp = 203
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14384316
44 X = 4323093
59
Y = 13328887
73 feet Y = 4111331
05 meter
Z = 10462052
08 Z = 3209983
82
XDOT = -5955
662065 XDOT = -1855
953169
YDOT = 18770
072286 feet/sec YDOT = 5700
590792 meter/sec
ZDOT = -15649
870072 ZDOT = -4778
998172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12768693
24 X = -3891897
70
Y = 14823040
79 feet Y = 4518062
83 meter
Z = 10547998
67 Z = 3215029
99
XDOT = -17899
931870 XDOT = -5455
899234
YDOT = -4203
699442 feet/sec YDOT = -1281
287590 meter/sec
ZDOT = -15686
466533 ZDOT = -4781
234999
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 11293
71707711
00016717 00000-0 10270-3 0 9048
2 25544 51
6407 248
8211 0018522 336
3233 23
7068 15
59921164 20519
Satellite: ISS
Catalog Number: 25544
Epoch time: 11293
71707711 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 248
8211 deg
Eccentricity:
0018522
Arg of perigee: 336
3233 deg
Mean anomaly: 23
7068 deg
Mean motion: 15
59921164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 291
Coasting Arc #6 (Orbit 2066)
---------------------------------------
Vector Time (GMT): 2011/294/16:16:52
739
Vector Time (MET): N/A
Weight (LBS) : 870891
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2900102
40 A = 6772369
53 meter
Y = -6096576
56 meter E =
0026061
Z = 218945
73 I = 51
35136
XDOT = 4424
519267 Wp = 6
20848
YDOT = -1887
686517 meter/sec RA = 243
07379 deg
ZDOT = 6002
003717 TA = 356
17016
MA = 356
19007
Ha = 216
088 n
mi
Hp = 203
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9514771
64 X = -2832777
34
Y = -20001891
60 feet Y = -6128630
83 meter
Z = 718325
90 Z = 205020
84
XDOT = 14516
139326 XDOT = 4416
142009
YDOT = -6193
197234 feet/sec YDOT = -1838
255287 meter/sec
ZDOT = 19691
613244 ZDOT = 6023
477982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19441152
69 X = 5925663
34
Y = -10617251
01 feet Y = -3236138
11 meter
Z = 661892
81 Z = 201744
93
XDOT = 6209
559544 XDOT = 1892
673749
YDOT = 12612
471886 feet/sec YDOT = 3844
281431 meter/sec
ZDOT = 19779
168383 ZDOT = 6028
690523
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 11294
74206476
00016717 00000-0 10270-3 0 9055
2 25544 51
6411 243
6654 0018597 339
8251 20
2168 15
59980831 20674
Satellite: ISS
Catalog Number: 25544
Epoch time: 11294
74206476 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 243
6654 deg
Eccentricity:
0018597
Arg of perigee: 339
8251 deg
Mean anomaly: 20
2168 deg
Mean motion: 15
59980831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2067
Checksum: 323
Coasting Arc #7 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2011/295/16:16:52
739
Vector Time (MET): N/A
Weight (LBS) : 870891
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 254728
72 A = 6766900
63 meter
Y = 5768031
56 meter E =
0018227
Z = -3546586
28 I = 51
34801
XDOT = -5733
600477 Wp = 359
27548
YDOT = -2486
408519 meter/sec RA = 238
04665 deg
ZDOT = -4437
444767 TA = 222
80834
MA = 222
95042
Ha = 216
217 n
mi
Hp = 203
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 835724
14 X = 207439
38
Y = 18923988
07 feet Y = 5770615
40 meter
Z = -11635781
75 Z = -3545464
13
XDOT = -18811
025188 XDOT = -5683
814293
YDOT = -8157
508265 feet/sec YDOT = -2550
247147 meter/sec
ZDOT = -14558
545825 ZDOT = -4465
177756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18807209
20 X = -5732437
36
Y = 2281428
26 feet Y = 695379
33 meter
Z = -11631472
10 Z = -3545272
70
XDOT = 6939
654011 XDOT = 2115
206543
YDOT = -17895
717162 feet/sec YDOT = -5454
614591 meter/sec
ZDOT = -14671
398690 ZDOT = -4471
842321
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 11295
70295825
00016717 00000-0 10270-3 0 9069
2 25544 51
6410 238
8326 0018532 342
8749 17
1779 15
60022125 20825
Satellite: ISS
Catalog Number: 25544
Epoch time: 11295
70295825 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 238
8326 deg
Eccentricity:
0018532
Arg of perigee: 342
8749 deg
Mean anomaly: 17
1779 deg
Mean motion: 15
60022125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 308
Coasting Arc #8 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2011/296/16:16:52
739
Vector Time (MET): N/A
Weight (LBS) : 870891
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2802931
91 A = 6760261
84 meter
Y = -3234173
92 meter E =
0016414
Z = 5232234
96 I = 51
34375
XDOT = 5095
347022 Wp = 355
56964
YDOT = 5689
078894 meter/sec RA = 232
97697 deg
ZDOT = 803
218188 TA = 86
82700
MA = 86
63921
Ha = 216
190 n
mi
Hp = 202
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9195970
84 X = 2813471
13
Y = -10610806
82 feet Y = -3202770
40 meter
Z = 17166125
21 Z = 5245877
70
XDOT = 16717
017789 XDOT = 5027
449972
YDOT = 18664
957002 feet/sec YDOT = 5745
678630 meter/sec
ZDOT = 2635
230275 ZDOT = 827
806291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11384857
50 X = 3470104
57
Y = 8100872
36 feet Y = 2469145
89 meter
Z = 17221842
02 Z = 5249217
45
XDOT = -16496
292276 XDOT = -5028
069886
YDOT = 17482
001255 feet/sec YDOT = 5328
513983 meter/sec
ZDOT = 2735
138558 ZDOT = 833
670232
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 11296
72787654
00016717 00000-0 10270-3 0 9079
2 25544 51
6412 233
6763 0018460 347
0923 12
9758 15
60091157 20984
Satellite: ISS
Catalog Number: 25544
Epoch time: 11296
72787654 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 233
6763 deg
Eccentricity:
0018460
Arg of perigee: 347
0923 deg
Mean anomaly: 12
9758 deg
Mean motion: 15
60091157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 327
Coasting Arc #9 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2011/297/16:16:52
739
Vector Time (MET): N/A
Weight (LBS) : 870891
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5065304
26 A = 6763207
88 meter
Y = -278037
27 meter E =
0015965
Z = -4469957
36 I = 51
37311
XDOT = -2452
968550 Wp = 22
08808
YDOT = -6533
396629 meter/sec RA = 227
89724 deg
ZDOT = 3204
312639 TA = 280
10641
MA = 280
28647
Ha = 216
226 n
mi
Hp = 202
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16618452
28 X = -5040104
04
Y = -912195
75 feet Y = -334540
11 meter
Z = -14665214
43 Z = -4494503
85
XDOT = -8047
797081 XDOT = -2395
294792
YDOT = -21435
028309 feet/sec YDOT = -6560
504462 meter/sec
ZDOT = 10512
836742 ZDOT = 3192
536572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -862271
38 X = -262820
32
Y = -16532362
83 feet Y = -5039064
19 meter
Z = -14765196
88 Z = -4500432
01
XDOT = 19237
191516 XDOT = 5863
495974
YDOT = -10296
746159 feet/sec YDOT = -3138
448229 meter/sec
ZDOT = 10465
149680 ZDOT = 3189
777622
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 11297
68870401
00016717 00000-0 10270-3 0 9089
2 25544 51
6409 228
8424 0018483 350
2009 9
8784 15
60151425 21133
Satellite: ISS
Catalog Number: 25544
Epoch time: 11297
68870401 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 228
8424 deg
Eccentricity:
0018483
Arg of perigee: 350
2009 deg
Mean anomaly: 9
8784 deg
Mean motion: 15
60151425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 306
Coasting Arc #10 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2011/298/16:16:52
739
Vector Time (MET): N/A
Weight (LBS) : 870891
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5592358
51 A = 6770670
33 meter
Y = 3496083
20 meter E =
0015947
Z = 1555719
90 I = 51
41987
XDOT = -1449
342714 Wp = 41
83196
YDOT = 4886
909303 meter/sec RA = 222
85778 deg
ZDOT = -5726
476192 TA = 121
08930
MA = 120
93271
Ha = 216
408 n
mi
Hp = 202
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18347632
90 X = 5545291
38
Y = 11470089
22 feet Y = 3558357
33 meter
Z = 5104067
93 Z = 1582773
66
XDOT = -4755
061398 XDOT = -1476
062497
YDOT = 16033
167005 feet/sec YDOT = 4870
552037 meter/sec
ZDOT = -18787
651547 ZDOT = -5733
582543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9107333
24 X = -2775915
17
Y = 19598964
83 feet Y = 5973764
48 meter
Z = 5214129
64 Z = 1589266
72
XDOT = -15055
297544 XDOT = -4588
854691
YDOT = -1950
920141 feet/sec YDOT = -594
640459 meter/sec
ZDOT = -18816
814652 ZDOT = -5735
365106
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 11298
71355229
00016717 00000-0 10270-3 0 9091
2 25544 51
6411 223
6866 0018398 354
3069 5
7875 15
60194618 21299
Satellite: ISS
Catalog Number: 25544
Epoch time: 11298
71355229 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 223
6866 deg
Eccentricity:
0018398
Arg of perigee: 354
3069 deg
Mean anomaly: 5
7875 deg
Mean motion: 15
60194618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 334
Coasting Arc #11 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2011/299/12:44:19
570
Vector Time (MET): N/A
Weight (LBS) : 870208
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2949915
01 A = 6763545
46 meter
Y = 3038267
92 meter E =
0019381
Z = -5280075
35 I = 51
40269
XDOT = -5799
072975 Wp = 25
68898
YDOT = -5007
714983 meter/sec RA = 218
56701 deg
ZDOT = 375
986474 TA = 247
80362
MA = 248
00937
Ha = 218
070 n
mi
Hp = 204
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9678198
84 X = -2958019
91
Y = 9968070
60 feet Y = 3005234
57 meter
Z = -17323081
87 Z = -5294426
28
XDOT = -19025
829971 XDOT = -5744
471237
YDOT = -16429
511100 feet/sec YDOT = -5072
258457 meter/sec
ZDOT = 1233
551425 ZDOT = 347
946689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -238471
66 X = -72686
16
Y = -13818081
60 feet Y = -4211751
27 meter
Z = -17381682
37 Z = -5297936
79
XDOT = 24073
276025 XDOT = 7337
534532
YDOT = -1751
074916 feet/sec YDOT = -533
727634 meter/sec
ZDOT = 1119
533469 ZDOT = 341
233801
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 11299
54621764
00016717 00000-0 10270-3 0 9105
2 25544 51
6410 219
4972 0019333 340
2411 19
7994 15
58893957 21425
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
54621764 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 219
4972 deg
Eccentricity:
0019333
Arg of perigee: 340
2411 deg
Mean anomaly: 19
7994 deg
Mean motion: 15
58893957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 324
Coasting Arc #12 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2011/300/12:44:19
570
Vector Time (MET): N/A
Weight (LBS) : 870208
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5403768
84 A = 6768222
65 meter
Y = -316343
09 meter E =
0021540
Z = 4073711
98 I = 51
44271
XDOT = 3240
906469 Wp = 13
45710
YDOT = 5801
330427 meter/sec RA = 213
50924 deg
ZDOT = -3823
905238 TA = 116
28216
MA = 116
06069
Ha = 218
189 n
mi
Hp = 204
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17728900
38 X = 5387114
71
Y = -1037871
02 feet Y = -256007
87 meter
Z = 13365196
78 Z = 4099923
77
XDOT = 10632
895241 XDOT = 3194
370335
YDOT = 19033
236308 feet/sec YDOT = 5837
311959 meter/sec
ZDOT = -12545
620861 ZDOT = -3808
273624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11555259
96 X = -3522043
24
Y = 13379105
88 feet Y = 4077951
47 meter
Z = 13472010
36 Z = 4106268
76
XDOT = -20136
545436 XDOT = -6137
619049
YDOT = -4741
875323 feet/sec YDOT = -1445
323598 meter/sec
ZDOT = -12482
187595 ZDOT = -3804
570779
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 11300
57189398
00016717 00000-0 10270-3 0 9114
2 25544 51
6405 214
3470 0019304 343
9794 16
0748 15
58935011 21580
Satellite: ISS
Catalog Number: 25544
Epoch time: 11300
57189398 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 214
3470 deg
Eccentricity:
0019304
Arg of perigee: 343
9794 deg
Mean anomaly: 16
0748 deg
Mean motion: 15
58935011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 308
Coasting Arc #13 (Orbit 2172)
---------------------------------------
Vector Time (GMT): 2011/301/12:44:19
570
Vector Time (MET): N/A
Weight (LBS) : 870208
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6253200
21 A = 6774455
42 meter
Y = -2191454
19 meter E =
0025759
Z = -1327659
22 I = 51
49030
XDOT = 519
050216 Wp = 2
70410
YDOT = -4992
311074 meter/sec RA = 208
48733 deg
ZDOT = 5825
502128 TA = 342
75501
MA = 342
84236
Ha = 218
220 n
mi
Hp = 204
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20515748
72 X = -6221780
49
Y = -7189810
35 feet Y = -2261205
62 meter
Z = -4355837
34 Z = -1357961
73
XDOT = 1702
920655 XDOT = 546
536694
YDOT = -16378
973339 feet/sec YDOT = -4986
353103 meter/sec
ZDOT = 19112
539790 ZDOT = 5828
090460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19266068
22 X = 5872297
59
Y = -10015879
42 feet Y = -3052840
05 meter
Z = -4479220
03 Z = -1365266
27
XDOT = 10123
155371 XDOT = 3085
537757
YDOT = 10962
789374 feet/sec YDOT = 3341
458201 meter/sec
ZDOT = 19123
311584 ZDOT = 5828
785371
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 11301
53343424
00016717 00000-0 10270-3 0 9124
2 25544 51
6410 209
5182 0019313 347
2568 12
8096 15
58986540 21738
Satellite: ISS
Catalog Number: 25544
Epoch time: 11301
53343424 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 209
5182 deg
Eccentricity:
0019313
Arg of perigee: 347
2568 deg
Mean anomaly: 12
8096 deg
Mean motion: 15
58986540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2173
Checksum: 296
Coasting Arc #14 (Orbit 2188)
---------------------------------------
Vector Time (GMT): 2011/302/12:44:19
570
Vector Time (MET): N/A
Weight (LBS) : 870208
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5156165
28 A = 6773564
05 meter
Y = 3943798
26 meter E =
0013616
Z = -1965148
07 I = 51
51442
XDOT = -4368
035213 Wp = 5
80944
YDOT = 2930
390338 meter/sec RA = 203
48492 deg
ZDOT = -5570
072101 TA = 195
91546
MA = 195
95829
Ha = 218
378 n
mi
Hp = 204
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16916552
77 X = 5121228
26
Y = 12938970
68 feet Y = 4001262
37 meter
Z = -6447336
17 Z = -1940183
67
XDOT = -14330
824190 XDOT = -4373
419811
YDOT = 9614
141529 feet/sec YDOT = 2881
514327 meter/sec
ZDOT = -18274
514766 ZDOT = -5591
305456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20974727
68 X = -6393097
00
Y = 3866113
01 feet Y = 1178391
25 meter
Z = -6345772
80 Z = -1934191
55
XDOT = 2715
049254 XDOT = 827
547013
YDOT = -15461
935930 feet/sec YDOT = -4712
798072 meter/sec
ZDOT = -18361
184036 ZDOT = -5596
488894
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 11302
55904505
00016717 00000-0 10270-3 0 9131
2 25544 51
6408 204
3676 0019189 350
7298 9
3501 15
59013957 21899
Satellite: ISS
Catalog Number: 25544
Epoch time: 11302
55904505 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 204
3676 deg
Eccentricity:
0019189
Arg of perigee: 350
7298 deg
Mean anomaly: 9
3501 deg
Mean motion: 15
59013957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2189
Checksum: 314
Coasting Arc #15 (Orbit 2204)
---------------------------------------
Vector Time (GMT): 2011/303/12:44:19
570
Vector Time (MET): N/A
Weight (LBS) : 870208
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2239801
42 A = 6766369
61 meter
Y = -4517209
72 meter E =
0017122
Z = 4498228
54 I = 51
51880
XDOT = 6994
171210 Wp = 22
85965
YDOT = -322
255724 meter/sec RA = 198
45865 deg
ZDOT = 3170
424642 TA = 35
39809
MA = 35
28456
Ha = 218
506 n
mi
Hp = 203
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7348429
87 X = -2210974
54
Y = -14820241
88 feet Y = -4542095
50 meter
Z = 14757967
66 Z = 4487417
31
XDOT = 22946
755939 XDOT = 6981
853321
YDOT = -1057
269436 feet/sec YDOT = -244
111580 meter/sec
ZDOT = 10401
655648 ZDOT = 3204
372921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16047643
52 X = 4891321
74
Y = 4171910
16 feet Y = 1271598
22 meter
Z = 14714105
60 Z = 4484859
39
XDOT = -13981
062608 XDOT = -4261
427883
YDOT = 16737
997438 feet/sec YDOT = 5101
741619 meter/sec
ZDOT = 10540
045797 ZDOT = 3212
605959
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 11303
58462229
00016717 00000-0 10270-3 0 9148
2 25544 51
6405 199
2160 0019271 354
9083 5
1873 15
59075638 22055
Satellite: ISS
Catalog Number: 25544
Epoch time: 11303
58462229 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 199
2160 deg
Eccentricity:
0019271
Arg of perigee: 354
9083 deg
Mean anomaly: 5
1873 deg
Mean motion: 15
59075638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2205
Checksum: 307
Coasting Arc #16 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2011/304/12:44:19
570
Vector Time (MET): N/A
Weight (LBS) : 870208
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1483790
62 A = 6762825
21 meter
Y = 3963287
06 meter E =
0023197
Z = -5286125
46 I = 51
53652
XDOT = -7347
287978 Wp = 37
86420
YDOT = -2140
082571 meter/sec RA = 193
40216 deg
ZDOT = 476
857591 TA = 236
58040
MA = 236
80249
Ha = 218
483 n
mi
Hp = 203
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4868079
46 X = -1502319
26
Y = 13002910
29 feet Y = 3946590
91 meter
Z = -17342931
29 Z = -5293378
72
XDOT = -24105
275520 XDOT = -7325
127595
YDOT = -7021
268278 feet/sec YDOT = -2222
120551 meter/sec
ZDOT = 1564
493410 ZDOT = 441
217845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6848505
38 X = -2087424
44
Y = -12034912
61 feet Y = -3668241
36 meter
Z = -17372679
46 Z = -5295192
70
XDOT = 20058
995352 XDOT = 6113
981783
YDOT = -13373
404567 feet/sec YDOT = -4076
213712 meter/sec
ZDOT = 1419
300018 ZDOT = 432
602645
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 11304
54606973
00016717 00000-0 10270-3 0 9152
2 25544 51
6402 194
3868 0019285 357
9621 2
1452 15
59151881 22201
Satellite: ISS
Catalog Number: 25544
Epoch time: 11304
54606973 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 194
3868 deg
Eccentricity:
0019285
Arg of perigee: 357
9621 deg
Mean anomaly: 2
1452 deg
Mean motion: 15
59151881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 307
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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