[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 7th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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 2442)
---------------------------------------
Vector Time (GMT): 2011/063/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2675168
19 A = 6730336
12 meter
Y = 4635296
41 meter E =
0015699
Z = 4075483
58 I = 51
51248
XDOT = -6673
688978 Wp = 57
80401
YDOT = -485
843873 meter/sec RA = 337
25240 deg
ZDOT = -3809
154734 TA = 71
48163
MA = 71
31112
Ha = 194
813 n
mi
Hp = 185
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8776798
53 X = -2746599
62
Y = 15207665
37 feet Y = 4604982
11 meter
Z = 13371009
13 Z = 4062313
92
XDOT = -21895
305047 XDOT = -6649
256436
YDOT = -1593
975961 feet/sec YDOT = -560
336915 meter/sec
ZDOT = -12497
226817 ZDOT = -3841
515329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12855614
49 X = -3918391
30
Y = 12019190
61 feet Y = 3663449
30 meter
Z = 13317709
90 Z = 4059237
98
XDOT = -19563
713077 XDOT = -5963
019746
YDOT = -6864
040234 feet/sec YDOT = -2092
159463 meter/sec
ZDOT = -12627
835586 ZDOT = -3848
964287
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 11063
54673180
00016717 00000-0 10270-3 0 9002
2 25544 51
6473 337
6020 0006556 26
8574 333
2926 15
72135752 24432
Satellite: ISS
Catalog Number: 25544
Epoch time: 11063
54673180 = yrday
fracday
Element set: 900
Inclination: 51
6473 deg
RA of node: 337
6020 deg
Eccentricity:
0006556
Arg of perigee: 26
8574 deg
Mean anomaly: 333
2926 deg
Mean motion: 15
72135752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2443
Checksum: 298
Coasting Arc #2 (Orbit 2458)
---------------------------------------
Vector Time (GMT): 2011/064/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6059920
14 A = 6733777
66 meter
Y = -644277
37 meter E =
0018256
Z = 2840024
36 I = 51
49738
XDOT = -1799
680830 Wp = 64
71831
YDOT = 5513
711398 meter/sec RA = 332
17045 deg
ZDOT = 5073
255630 TA = 327
94958
MA = 328
06047
Ha = 194
674 n
mi
Hp = 185
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19881627
76 X = 6052878
13
Y = -2113770
91 feet Y = -576550
72 meter
Z = 9317665
21 Z = 2869445
83
XDOT = -5904
464666 XDOT = -1885
846911
YDOT = 18089
604323 feet/sec YDOT = 5493
105088 meter/sec
ZDOT = 16644
539470 ZDOT = 5064
303020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19656309
73 X = 5991243
21
Y = 3339038
59 feet Y = 1017738
96 meter
Z = 9436437
02 Z = 2876226
00
XDOT = -10438
671062 XDOT = -3181
706940
YDOT = 14352
550165 feet/sec YDOT = 4374
657290 meter/sec
ZDOT = 16608
242159 ZDOT = 5062
192210
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 11064
56375141
00016717 00000-0 10270-3 0 9012
2 25544 51
6477 332
3938 0006571 30
2386 329
9154 15
72177849 24598
Satellite: ISS
Catalog Number: 25544
Epoch time: 11064
56375141 = yrday
fracday
Element set: 901
Inclination: 51
6477 deg
RA of node: 332
3938 deg
Eccentricity:
0006571
Arg of perigee: 30
2386 deg
Mean anomaly: 329
9154 deg
Mean motion: 15
72177849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2459
Checksum: 324
Coasting Arc #3 (Orbit 2473)
---------------------------------------
Vector Time (GMT): 2011/065/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 468045
63 A = 6727575
10 meter
Y = -4785642
92 meter E =
0014201
Z = -4716475
01 I = 51
45068
XDOT = 6934
694700 Wp = 82
23579
YDOT = -1956
295388 meter/sec RA = 326
99283 deg
ZDOT = 2681
934523 TA = 214
20815
MA = 214
29972
Ha = 194
691 n
mi
Hp = 184
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1535582
76 X = 544436
24
Y = -15700928
21 feet Y = -4779982
38 meter
Z = -15473999
37 Z = -4714015
17
XDOT = 22751
623030 XDOT = 6943
026812
YDOT = -6418
291957 feet/sec YDOT = -1878
700529 meter/sec
ZDOT = 8798
997779 ZDOT = 2715
643206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5569473
33 X = 1697575
47
Y = -14770563
37 feet Y = -4502067
71 meter
Z = -15463933
59 Z = -4713406
96
XDOT = 22507
462673 XDOT = 6860
274623
YDOT = -837
584110 feet/sec YDOT = -255
295637 meter/sec
ZDOT = 8935
103489 ZDOT = 2723
419543
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 11065
51717794
00016717 00000-0 10270-3 0 9023
2 25544 51
6480 327
5114 0006497 32
7781 327
3783 15
72237352 24740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11065
51717794 = yrday
fracday
Element set: 902
Inclination: 51
6480 deg
RA of node: 327
5114 deg
Eccentricity:
0006497
Arg of perigee: 32
7781 deg
Mean anomaly: 327
3783 deg
Mean motion: 15
72237352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2474
Checksum: 317
Coasting Arc #4 (Orbit 2489)
---------------------------------------
Vector Time (GMT): 2011/066/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5874299
58 A = 6735583
11 meter
Y = 2727177
57 meter E =
0008195
Z = -1856314
71 I = 51
45298
XDOT = -641
120402 Wp = 92
79578
YDOT = -5199
000183 meter/sec RA = 321
89522 deg
ZDOT = -5630
992967 TA = 107
83200
MA = 107
74259
Ha = 194
648 n
mi
Hp = 184
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19272636
43 X = -5895341
27
Y = 8947432
98 feet Y = 2661369
74 meter
Z = -6090271
37 Z = -1884903
14
XDOT = -2103
413391 XDOT = -555
582515
YDOT = -17057
087213 feet/sec YDOT = -5205
691941 meter/sec
ZDOT = -18474
386376 ZDOT = -5633
899143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20811559
18 X = -6343363
24
Y = 4117091
03 feet Y = 1254889
35 meter
Z = -6205726
65 Z = -1891505
48
XDOT = 2420
110382 XDOT = 737
649645
YDOT = -15524
890973 feet/sec YDOT = -4731
986769 meter/sec
ZDOT = -18485
967803 ZDOT = -5634
522986
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 11066
53413693
00016717 00000-0 10270-3 0 9038
2 25544 51
6480 322
3028 0006304 36
3904 323
7686 15
72257075 24905
Satellite: ISS
Catalog Number: 25544
Epoch time: 11066
53413693 = yrday
fracday
Element set: 903
Inclination: 51
6480 deg
RA of node: 322
3028 deg
Eccentricity:
0006304
Arg of perigee: 36
3904 deg
Mean anomaly: 323
7686 deg
Mean motion: 15
72257075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2490
Checksum: 297
Coasting Arc #5 (Orbit 2505)
---------------------------------------
Vector Time (GMT): 2011/067/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1532486
86 A = 6725542
27 meter
Y = 4127060
42 meter E =
0011137
Z = 5079463
87 I = 51
39655
XDOT = -6261
139512 Wp = 45
01221
YDOT = 4218
383503 meter/sec RA = 316
72722 deg
ZDOT = -1528
630181 TA = 59
75375
MA = 59
64355
Ha = 194
501 n
mi
Hp = 184
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5027844
02 X = 1461548
48
Y = 13540224
47 feet Y = 4143801
49 meter
Z = 16664907
71 Z = 5086735
90
XDOT = -20541
796300 XDOT = -6300
419188
YDOT = 13839
840890 feet/sec YDOT = 4148
147869 meter/sec
ZDOT = -5015
190884 ZDOT = -1559
142367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1813488
75 X = 552751
37
Y = 14295209
10 feet Y = 4357179
73 meter
Z = 16694139
64 Z = 5088373
76
XDOT = -22020
571380 XDOT = -6711
870157
YDOT = 8831
763464 feet/sec YDOT = 2691
921504 meter/sec
ZDOT = -5138
446027 ZDOT = -1566
198349
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 11067
55106248
00016717 00000-0 10270-3 0 9047
2 25544 51
6477 317
0939 0006380 38
5947 321
5671 15
72375124 25062
Satellite: ISS
Catalog Number: 25544
Epoch time: 11067
55106248 = yrday
fracday
Element set: 904
Inclination: 51
6477 deg
RA of node: 317
0939 deg
Eccentricity:
0006380
Arg of perigee: 38
5947 deg
Mean anomaly: 321
5671 deg
Mean motion: 15
72375124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2506
Checksum: 313
Coasting Arc #6 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2011/068/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4895738
86 A = 6736479
08 meter
Y = -4541193
77 meter E =
0019841
Z = 808385
79 I = 51
41187
XDOT = 2756
151104 Wp = 49
84245
YDOT = 4045
126738 meter/sec RA = 311
60823 deg
ZDOT = 5948
842845 TA = 319
00207
MA = 319
15106
Ha = 194
549 n
mi
Hp = 184
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16062135
36 X = 4942228
52
Y = -14898929
68 feet Y = -4486186
64 meter
Z = 2652184
34 Z = 832282
44
XDOT = 9042
490500 XDOT = 2681
814672
YDOT = 13271
413181 feet/sec YDOT = 4075
532564 meter/sec
ZDOT = 19517
200934 ZDOT = 5962
051225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18750327
35 X = 5715099
78
Y = -11308138
46 feet Y = -3446720
60 meter
Z = 2748746
73 Z = 837818
00
XDOT = 5202
667035 XDOT = 1585
772912
YDOT = 13447
897917 feet/sec YDOT = 4098
919285 meter/sec
ZDOT = 19570
391973 ZDOT = 5965
055473
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 11068
56795933
00016717 00000-0 10270-3 0 9055
2 25544 51
6476 311
8847 0006383 42
3102 317
8552 15
72385668 25228
Satellite: ISS
Catalog Number: 25544
Epoch time: 11068
56795933 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 311
8847 deg
Eccentricity:
0006383
Arg of perigee: 42
3102 deg
Mean anomaly: 317
8552 deg
Mean motion: 15
72385668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 327
Coasting Arc #7 (Orbit 2536)
---------------------------------------
Vector Time (GMT): 2011/069/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3139456
81 A = 6724591
76 meter
Y = -2819113
30 meter E =
0019770
Z = -5252604
52 I = 51
35251
XDOT = 4789
906599 Wp = 78
99281
YDOT = -5997
912656 meter/sec RA = 306
45490 deg
ZDOT = 361
086283 TA = 194
42827
MA = 194
48481
Ha = 194
493 n
mi
Hp = 184
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10300055
14 X = -3082183
57
Y = -9249059
37 feet Y = -2853900
74 meter
Z = -17232954
46 Z = -5267716
59
XDOT = 15714
916663 XDOT = 4854
866318
YDOT = -19678
191130 feet/sec YDOT = -5943
985784 meter/sec
ZDOT = 1184
666283 ZDOT = 384
513710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8283469
04 X = -2524801
36
Y = -10996245
58 feet Y = -3351655
65 meter
Z = -17293862
45 Z = -5271169
27
XDOT = 18314
086499 XDOT = 5582
133565
YDOT = -15783
061024 feet/sec YDOT = -4810
677000 meter/sec
ZDOT = 1279
372770 ZDOT = 389
952820
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 11069
52127034
00016717 00000-0 10270-3 0 9064
2 25544 51
6472 307
0007 0006329 45
0940 315
0735 15
72444452 25375
Satellite: ISS
Catalog Number: 25544
Epoch time: 11069
52127034 = yrday
fracday
Element set: 906
Inclination: 51
6472 deg
RA of node: 307
0007 deg
Eccentricity:
0006329
Arg of perigee: 45
0940 deg
Mean anomaly: 315
0735 deg
Mean motion: 15
72444452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2537
Checksum: 283
Coasting Arc #8 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2011/070/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3391552
80 A = 6736616
15 meter
Y = 5814634
72 meter E =
0014574
Z = 155795
18 I = 51
37572
XDOT = -4226
117317 Wp = 108
17256
YDOT = -2291
775599 meter/sec RA = 301
31367 deg
ZDOT = -6009
644962 TA = 70
13029
MA = 69
97329
Ha = 194
521 n
mi
Hp = 184
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11127141
74 X = -3457077
90
Y = 19076885
57 feet Y = 5776341
96 meter
Z = 511139
03 Z = 139159
65
XDOT = -13865
214295 XDOT = -4170
982602
YDOT = -7518
948817 feet/sec YDOT = -2338
726673 meter/sec
ZDOT = -19716
682946 ZDOT = -6030
041229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14218181
67 X = -4333701
77
Y = 16901136
59 feet Y = 5151466
43 meter
Z = 443848
53 Z = 135285
03
XDOT = -11032
072004 XDOT = -3362
575547
YDOT = -8715
636622 feet/sec YDOT = -2656
526042 meter/sec
ZDOT = -19798
931694 ZDOT = -6034
714380
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 11070
53810643
00016717 00000-0 10270-3 0 9073
2 25544 51
6471 301
7915 0006195 49
9996 310
1709 15
72437746 25531
Satellite: ISS
Catalog Number: 25544
Epoch time: 11070
53810643 = yrday
fracday
Element set: 907
Inclination: 51
6471 deg
RA of node: 301
7915 deg
Eccentricity:
0006195
Arg of perigee: 49
9996 deg
Mean anomaly: 310
1709 deg
Mean motion: 15
72437746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 318
Coasting Arc #9 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2011/071/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4101147
82 A = 6724485
24 meter
Y = 1105177
68 meter E =
0008020
Z = 5206406
80 I = 51
32041
XDOT = -2847
358129 Wp = 72
12682
YDOT = 7122
173726 meter/sec RA = 296
17601 deg
ZDOT = 732
559895 TA = 10
88656
MA = 10
86921
Ha = 194
326 n
mi
Hp = 184
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13455209
37 X = 4063193
18
Y = 3625911
04 feet Y = 1150827
24 meter
Z = 17081387
15 Z = 5226237
73
XDOT = -9341
726146 XDOT = -2930
346613
YDOT = 23366
711701 feet/sec YDOT = 7089
868865 meter/sec
ZDOT = 2403
411730 ZDOT = 718
525655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12638247
61 X = 3852137
87
Y = 5632503
03 feet Y = 1716786
92 meter
Z = 17161389
34 Z = 5230791
47
XDOT = -12419
808889 XDOT = -3785
557749
YDOT = 20732
925602 feet/sec YDOT = 6319
395724 meter/sec
ZDOT = 2346
587203 ZDOT = 715
239779
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 11071
55490884
00016717 00000-0 10270-3 0 9088
2 25544 51
6468 296
5814 0006266 52
1733 307
9996 15
72516926 25697
Satellite: ISS
Catalog Number: 25544
Epoch time: 11071
55490884 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 296
5814 deg
Eccentricity:
0006266
Arg of perigee: 52
1733 deg
Mean anomaly: 307
9996 deg
Mean motion: 15
72516926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 349
Coasting Arc #10 (Orbit 2583)
---------------------------------------
Vector Time (GMT): 2011/072/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1533277
41 A = 6735745
62 meter
Y = -6458886
91 meter E =
0015602
Z = -1105997
80 I = 51
34533
XDOT = 4967
578439 Wp = 44
04961
YDOT = 182
844685 meter/sec RA = 291
01233 deg
ZDOT = 5879
597131 TA = 303
80200
MA = 303
95047
Ha = 194
370 n
mi
Hp = 184
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5030437
71 X = 1610760
62
Y = -21190573
84 feet Y = -6441307
69 meter
Z = -3628601
71 Z = -1098360
75
XDOT = 16297
829524 XDOT = 4936
603005
YDOT = 599
884136 feet/sec YDOT = 238
222221 meter/sec
ZDOT = 19290
016834 ZDOT = 5903
654046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7895643
44 X = 2406592
12
Y = -20303409
58 feet Y = -6188479
24 meter
Z = -3597616
97 Z = -1096553
65
XDOT = 14468
418888 XDOT = 4409
974077
YDOT = 2226
846239 feet/sec YDOT = 678
742734 meter/sec
ZDOT = 19387
101749 ZDOT = 5909
188613
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 11072
50813246
00016717 00000-0 10270-3 0 9096
2 25544 51
6458 291
6966 0006189 53
9420 306
2315 15
72562177 25849
Satellite: ISS
Catalog Number: 25544
Epoch time: 11072
50813246 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 291
6966 deg
Eccentricity:
0006189
Arg of perigee: 53
9420 deg
Mean anomaly: 306
2315 deg
Mean motion: 15
72562177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2584
Checksum: 319
Coasting Arc #11 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2011/073/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4412230
01 A = 6725029
87 meter
Y = 768054
50 meter E =
0019359
Z = -5034229
87 I = 51
29865
XDOT = 679
366735 Wp = 70
83664
YDOT = -7455
260504 meter/sec RA = 285
88924 deg
ZDOT = -1732
025542 TA = 182
37067
MA = 182
37986
Ha = 194
299 n
mi
Hp = 183
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14475820
24 X = -4396035
66
Y = 2519863
85 feet Y = 718804
58 meter
Z = -16516502
19 Z = -5055624
81
XDOT = 2228
893488 XDOT = 771
096103
YDOT = -24459
516089 feet/sec YDOT = -7447
150610 meter/sec
ZDOT = -5682
498498 ZDOT = -1728
502072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14574706
74 X = -4442370
62
Y = 785198
79 feet Y = 239328
59 meter
Z = -16602870
72 Z = -5060555
00
XDOT = 5223
403177 XDOT = 1592
093288
YDOT = -22951
988252 feet/sec YDOT = -6995
766019 meter/sec
ZDOT = -5668
099905 ZDOT = -1727
636851
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 11073
52487374
00016717 00000-0 10270-3 0 9100
2 25544 51
6446 286
4858 0006121 57
7125 302
4629 15
72620977 26006
Satellite: ISS
Catalog Number: 25544
Epoch time: 11073
52487374 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 286
4858 deg
Eccentricity:
0006121
Arg of perigee: 57
7125 deg
Mean anomaly: 302
4629 deg
Mean motion: 15
72620977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 310
Coasting Arc #12 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2011/074/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 332340
71 A = 6734286
06 meter
Y = 6444721
67 meter E =
0018450
Z = 1904041
15 I = 51
32385
XDOT = -4924
732217 Wp = 97
36261
YDOT = 1921
198202 meter/sec RA = 280
70906 deg
ZDOT = -5599
174643 TA = 61
38446
MA = 61
19899
Ha = 194
181 n
mi
Hp = 183
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1090356
66 X = 251000
61
Y = 21144099
98 feet Y = 6447983
43 meter
Z = 6246854
17 Z = 1905457
66
XDOT = -16157
257931 XDOT = -4918
650179
YDOT = 6303
143707 feet/sec YDOT = 1866
160525 meter/sec
ZDOT = -18369
995549 ZDOT = -5623
083846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1114822
64 X = -339797
94
Y = 21141176
25 feet Y = 6443830
52 meter
Z = 6252428
80 Z = 1905740
30
XDOT = -15065
847744 XDOT = -4592
070392
YDOT = 4709
644402 feet/sec YDOT = 1435
499614 meter/sec
ZDOT = -18466
540058 ZDOT = -5628
601410
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 11074
54158197
00016717 00000-0 10270-3 0 9112
2 25544 51
6450 281
2756 0006131 59
8316 300
3453 15
72707225 26168
Satellite: ISS
Catalog Number: 25544
Epoch time: 11074
54158197 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 281
2756 deg
Eccentricity:
0006131
Arg of perigee: 59
8316 deg
Mean anomaly: 300
3453 deg
Mean motion: 15
72707225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 294
Coasting Arc #13 (Orbit 2631)
---------------------------------------
Vector Time (GMT): 2011/075/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4047629
68 A = 6726141
43 meter
Y = -2554784
07 meter E =
0012146
Z = 4715506
06 I = 51
29014
XDOT = 1417
978403 Wp = 94
49935
YDOT = 7105
051726 meter/sec RA = 275
59694 deg
ZDOT = 2625
509998 TA = 329
57736
MA = 329
64779
Ha = 194
137 n
mi
Hp = 183
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13279624
94 X = 4052990
35
Y = -8381837
50 feet Y = -2509490
66 meter
Z = 15470820
42 Z = 4735182
25
XDOT = 4652
160115 XDOT = 1325
669001
YDOT = 23310
537160 feet/sec YDOT = 7120
392510 meter/sec
ZDOT = 8613
877945 ZDOT = 2632
173577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13852535
61 X = 4222252
85
Y = -7228112
34 feet Y = -2203128
64 meter
Z = 15550291
70 Z = 4739728
91
XDOT = 2072
167320 XDOT = 631
596599
YDOT = 22607
774725 feet/sec YDOT = 6890
849736 meter/sec
ZDOT = 8640
630808 ZDOT = 2633
664270
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 11075
55826040
00016717 00000-0 10270-3 0 9124
2 25544 51
6435 276
0641 0006130 64
3490 295
8305 15
72684181 26326
Satellite: ISS
Catalog Number: 25544
Epoch time: 11075
55826040 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 276
0641 deg
Eccentricity:
0006130
Arg of perigee: 64
3490 deg
Mean anomaly: 295
8305 deg
Mean motion: 15
72684181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2632
Checksum: 294
Coasting Arc #14 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2011/076/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2081225
98 A = 6732594
36 meter
Y = -5829196
83 meter E =
0010861
Z = -2649804
94 I = 51
30984
XDOT = 4183
228389 Wp = 62
50523
YDOT = -3842
933919 meter/sec RA = 270
40272 deg
ZDOT = 5189
505151 TA = 267
21556
MA = 267
33988
Ha = 194
085 n
mi
Hp = 183
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6828169
21 X = -2003016
10
Y = -19124661
53 feet Y = -5852033
36 meter
Z = -8693585
75 Z = -2659724
72
XDOT = 13724
502587 XDOT = 4200
680737
YDOT = -12608
050916 feet/sec YDOT = -3796
056374 meter/sec
ZDOT = 17025
935535 ZDOT = 5209
869665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5460160
49 X = -1664256
92
Y = -19541424
83 feet Y = -5956226
29 meter
Z = -8733519
89 Z = -2661976
86
XDOT = 13023
044205 XDOT = 3969
423874
YDOT = -11253
929289 feet/sec YDOT = -3430
197647 meter/sec
ZDOT = 17108
205387 ZDOT = 5214
581002
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 11076
51136291
00016717 00000-0 10270-3 0 9134
2 25544 51
6424 271
1779 0005999 68
7905 291
3898 15
72770753 26478
Satellite: ISS
Catalog Number: 25544
Epoch time: 11076
51136291 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 271
1779 deg
Eccentricity:
0005999
Arg of perigee: 68
7905 deg
Mean anomaly: 291
3898 deg
Mean motion: 15
72770753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 346
Coasting Arc #15 (Orbit 2662)
---------------------------------------
Vector Time (GMT): 2011/077/12:08:39
551
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3164776
75 A = 6727240
17 meter
Y = 4055183
87 meter E =
0015186
Z = -4350695
32 I = 51
29263
XDOT = -3211
950835 Wp = 70
42006
YDOT = -6116
408837 meter/sec RA = 265
29890 deg
ZDOT = -3369
086749 TA = 165
42787
MA = 165
38404
Ha = 194
072 n
mi
Hp = 183
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10383125
81 X = -3188752
82
Y = 13304409
03 feet Y = 4019658
79 meter
Z = -14273934
79 Z = -4366128
32
XDOT = -10537
896440 XDOT = -3126
951123
YDOT = -20066
958126 feet/sec YDOT = -6151
851999 meter/sec
ZDOT = -11053
434217 ZDOT = -3384
482886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10960284
31 X = -3340694
66
Y = 12763408
17 feet Y = 3890286
81 meter
Z = -14336296
43 Z = -4369703
15
XDOT = -8507
655272 XDOT = -2593
133327
YDOT = -19774
329651 feet/sec YDOT = -6027
215678 meter/sec
ZDOT = -11115
479207 ZDOT = -3387
998062
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 11077
52797459
00016717 00000-0 10270-3 0 9146
2 25544 51
6417 265
9664 0006114 72
1239 288
0590 15
72830061 26632
Satellite: ISS
Catalog Number: 25544
Epoch time: 11077
52797459 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 265
9664 deg
Eccentricity:
0006114
Arg of perigee: 72
1239 deg
Mean anomaly: 288
0590 deg
Mean motion: 15
72830061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2663
Checksum: 322
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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