[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 24th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 3698)
---------------------------------------
Vector Time (GMT): 2011/143/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1743938
95 A = 6721053
61 meter
Y = -5105253
59 meter E =
0003650
Z = -4011366
64 I = 51
31753
XDOT = 4743
500858 Wp = 85
45451
YDOT = -4663
540175 meter/sec RA = 287
67550 deg
ZDOT = 3876
352193 TA = 224
69481
MA = 224
72423
Ha = 187
092 n
mi
Hp = 182
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5721584
47 X = -1667234
98
Y = -16749519
65 feet Y = -5124326
14 meter
Z = -13160651
69 Z = -4019652
81
XDOT = 15562
666858 XDOT = 4776
466356
YDOT = -15300
328659 feet/sec YDOT = -4610
311496 meter/sec
ZDOT = 12717
690922 ZDOT = 3899
475701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2881372
68 X = -878242
39
Y = -17438554
74 feet Y = -5315271
49 meter
Z = -13193945
22 Z = -4021514
50
XDOT = 16469
081523 XDOT = 5019
776048
YDOT = -12406
105337 feet/sec YDOT = -3781
380907 meter/sec
ZDOT = 12811
485925 ZDOT = 3904
940910
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 11143
31706211
00016717 00000-0 10270-3 0 9008
2 25544 51
6475 288
3576 0004155 308
6956 51
3836 15
75433838 36991
Satellite: ISS
Catalog Number: 25544
Epoch time: 11143
31706211 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 288
3576 deg
Eccentricity:
0004155
Arg of perigee: 308
6956 deg
Mean anomaly: 51
3836 deg
Mean motion: 15
75433838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 323
Coasting Arc #2 (Orbit 3714)
---------------------------------------
Vector Time (GMT): 2011/144/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3958021
79 A = 6721762
95 meter
Y = 3930282
83 meter E =
0005247
Z = -3757033
56 I = 51
31102
XDOT = -2081
432137 Wp = 32
99999
YDOT = -6107
946330 meter/sec RA = 282
55817 deg
ZDOT = -4195
232223 TA = 192
70163
MA = 192
71485
Ha = 187
197 n
mi
Hp = 182
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12985635
81 X = -3983425
84
Y = 12894628
72 feet Y = 3885880
06 meter
Z = -12326225
58 Z = -3776323
01
XDOT = -6828
845593 XDOT = -1992
597568
YDOT = -20039
193996 feet/sec YDOT = -6130
725160 meter/sec
ZDOT = -13763
885245 ZDOT = -4205
128471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14627916
31 X = -4458588
89
Y = 10908130
04 feet Y = 3324798
04 meter
Z = -12404466
44 Z = -3780881
37
XDOT = -3005
681730 XDOT = -916
131791
YDOT = -19733
737174 feet/sec YDOT = -6014
843091 meter/sec
ZDOT = -13803
657018 ZDOT = -4207
354659
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 11144
33195880
00016717 00000-0 10270-3 0 9016
2 25544 51
6464 283
1355 0004242 313
0572 47
0237 15
75474160 37157
Satellite: ISS
Catalog Number: 25544
Epoch time: 11144
33195880 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 283
1355 deg
Eccentricity:
0004242
Arg of perigee: 313
0572 deg
Mean anomaly: 47
0237 deg
Mean motion: 15
75474160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3715
Checksum: 287
Coasting Arc #3 (Orbit 3730)
---------------------------------------
Vector Time (GMT): 2011/145/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1924804
36 A = 6723022
43 meter
Y = 5547781
08 meter E =
0010131
Z = 3268324
20 I = 51
31105
XDOT = -4346
063813 Wp = 73
43358
YDOT = 4285
105861 meter/sec RA = 277
33550 deg
ZDOT = -4699
316318 TA = 68
02706
MA = 67
91943
Ha = 187
158 n
mi
Hp = 182
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6314974
94 X = 1846748
01
Y = 18201381
51 feet Y = 5568868
77 meter
Z = 10722848
42 Z = 3277485
66
XDOT = -14258
739545 XDOT = -4370
829226
YDOT = 14058
746262 feet/sec YDOT = 4236
367364 meter/sec
ZDOT = -15417
704454 ZDOT = -4720
489402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3899075
50 X = 1188438
21
Y = 18846091
80 feet Y = 5744288
78 meter
Z = 10759679
82 Z = 3279550
41
XDOT = -14455
477618 XDOT = -4406
029578
YDOT = 11869
827973 feet/sec YDOT = 3617
923566 meter/sec
ZDOT = -15503
579865 ZDOT = -4725
491143
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 11145
34681973
00016717 00000-0 10270-3 0 9022
2 25544 51
6469 277
9121 0004478 317
1339 42
9475 15
75572021 37312
Satellite: ISS
Catalog Number: 25544
Epoch time: 11145
34681973 = yrday
fracday
Element set: 902
Inclination: 51
6469 deg
RA of node: 277
9121 deg
Eccentricity:
0004478
Arg of perigee: 317
1339 deg
Mean anomaly: 42
9475 deg
Mean motion: 15
75572021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3731
Checksum: 318
Coasting Arc #4 (Orbit 3746)
---------------------------------------
Vector Time (GMT): 2011/146/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3668945
83 A = 6719186
36 meter
Y = -3496043
69 meter E =
0005818
Z = 4406732
84 I = 51
29380
XDOT = 2354
845671 Wp = 88
95270
YDOT = 6576
629610 meter/sec RA = 272
21251 deg
ZDOT = 3253
330448 TA = 328
27730
MA = 328
31234
Ha = 187
206 n
mi
Hp = 182
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12037223
85 X = 3686359
37
Y = -11469959
62 feet Y = -3454918
22 meter
Z = 14457784
90 Z = 4424598
74
XDOT = 7725
871624 XDOT = 2265
325354
YDOT = 21576
868800 feet/sec YDOT = 6602
462187 meter/sec
ZDOT = 10673
656326 ZDOT = 3264
553305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13132829
56 X = 4002886
45
Y = -10093722
04 feet Y = -3076566
48 meter
Z = 14530238
78 Z = 4428816
78
XDOT = 4520
218558 XDOT = 1377
762616
YDOT = 21328
129773 feet/sec YDOT = 6500
813955 meter/sec
ZDOT = 10718
792414 ZDOT = 3267
087928
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 11146
36165014
00016717 00000-0 10270-3 0 9039
2 25544 51
6455 272
6880 0004405 322
0512 38
0341 15
75558986 37478
Satellite: ISS
Catalog Number: 25544
Epoch time: 11146
36165014 = yrday
fracday
Element set: 903
Inclination: 51
6455 deg
RA of node: 272
6880 deg
Eccentricity:
0004405
Arg of perigee: 322
0512 deg
Mean anomaly: 38
0341 deg
Mean motion: 15
75558986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3747
Checksum: 301
Coasting Arc #5 (Orbit 3761)
---------------------------------------
Vector Time (GMT): 2011/147/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2204062
53 A = 6725067
29 meter
Y = -5893392
75 meter E =
0007588
Z = -2362847
11 I = 51
31367
XDOT = 4112
420961 Wp = 12
00920
YDOT = -3686
813038 meter/sec RA = 266
99490 deg
ZDOT = 5369
960431 TA = 321
22275
MA = 321
27718
Ha = 187
238 n
mi
Hp = 182
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7231176
28 X = -2126519
29
Y = -19335278
04 feet Y = -5917606
18 meter
Z = -7752123
08 Z = -2373366
59
XDOT = 13492
194755 XDOT = 4127
255460
YDOT = -12095
843302 feet/sec YDOT = -3640
742872 meter/sec
ZDOT = 17617
980417 ZDOT = 5389
974516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5370468
10 X = -1636918
68
Y = -19915897
09 feet Y = -6070365
43 meter
Z = -7794447
71 Z = -2375747
66
XDOT = 12992
557489 XDOT = 3960
131523
YDOT = -10417
125349 feet/sec YDOT = -3175
139806 meter/sec
ZDOT = 17699
134545 ZDOT = 5394
696209
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 11147
31301968
00016717 00000-0 10270-3 0 9046
2 25544 51
6449 267
7902 0004307 324
8821 35
2058 15
75633604 37627
Satellite: ISS
Catalog Number: 25544
Epoch time: 11147
31301968 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 267
7902 deg
Eccentricity:
0004307
Arg of perigee: 324
8821 deg
Mean anomaly: 35
2058 deg
Mean motion: 15
75633604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3762
Checksum: 307
Coasting Arc #6 (Orbit 3777)
---------------------------------------
Vector Time (GMT): 2011/148/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3567473
03 A = 6716764
71 meter
Y = 2885991
20 meter E =
0012436
Z = -4916067
97 I = 51
28858
XDOT = -2685
159374 Wp = 54
86182
YDOT = -6898
557457 meter/sec RA = 261
86105 deg
ZDOT = -2097
942945 TA = 194
66755
MA = 194
70367
Ha = 187
358 n
mi
Hp = 181
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11704307
85 X = -3575597
96
Y = 9468475
07 feet Y = 2846052
51 meter
Z = -16128831
93 Z = -4933418
45
XDOT = -8809
578000 XDOT = -2597
627271
YDOT = -22633
062523 feet/sec YDOT = -6928
094954 meter/sec
ZDOT = -6883
014911 ZDOT = -2110
775528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12285583
07 X = -3744645
72
Y = 8569323
89 feet Y = 2611929
92 meter
Z = -16199172
77 Z = -4937507
86
XDOT = -6418
835313 XDOT = -1956
461003
YDOT = -22332
046514 feet/sec YDOT = -6806
807777 meter/sec
ZDOT = -6934
664035 ZDOT = -2113
685598
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 11148
32778213
00016717 00000-0 10270-3 0 9050
2 25544 51
6445 262
5667 0004288 330
8357 29
2567 15
75691744 37787
Satellite: ISS
Catalog Number: 25544
Epoch time: 11148
32778213 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 262
5667 deg
Eccentricity:
0004288
Arg of perigee: 330
8357 deg
Mean anomaly: 29
2567 deg
Mean motion: 15
75691744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3778
Checksum: 341
Coasting Arc #7 (Orbit 3793)
---------------------------------------
Vector Time (GMT): 2011/149/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2489132
08 A = 6726389
92 meter
Y = 6115998
84 meter E =
0010358
Z = 1262825
09 I = 51
32794
XDOT = -4115
190816 Wp = 107
10748
YDOT = 2887
224972 meter/sec RA = 256
65887 deg
ZDOT = -5835
389309 TA = 58
97076
MA = 58
86909
Ha = 187
344 n
mi
Hp = 181
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8166443
83 X = 2414422
15
Y = 20065613
00 feet Y = 6143415
98 meter
Z = 4143126
95 Z = 1274736
57
XDOT = -13501
282206 XDOT = -4118
822831
YDOT = 9472
522873 feet/sec YDOT = 2841
186661 meter/sec
ZDOT = -19144
978047 ZDOT = -5855
389715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6965332
94 X = 2123033
48
Y = 20503757
53 feet Y = 6249545
29 meter
Z = 4191085
18 Z = 1277442
76
XDOT = -12417
293573 XDOT = -3784
791081
YDOT = 8172
307945 feet/sec YDOT = 2490
919462 meter/sec
ZDOT = -19226
045835 ZDOT = -5860
098770
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 11149
34250848
00016717 00000-0 10270-3 0 9063
2 25544 51
6450 257
3423 0004638 333
6499 26
4428 15
75785429 37949
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
34250848 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 257
3423 deg
Eccentricity:
0004638
Arg of perigee: 333
6499 deg
Mean anomaly: 26
4428 deg
Mean motion: 15
75785429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3794
Checksum: 336
Coasting Arc #8 (Orbit 3809)
---------------------------------------
Vector Time (GMT): 2011/150/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3675603
42 A = 6715327
72 meter
Y = -2136830
01 meter E =
0002841
Z = 5196648
99 I = 51
29792
XDOT = 3010
782398 Wp = 26
71221
YDOT = 7050
874072 meter/sec RA = 251
50511 deg
ZDOT = 772
084509 TA = 55
92458
MA = 55
89762
Ha = 187
409 n
mi
Hp = 181
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12059066
34 X = 3673979
95
Y = -7010597
14 feet Y = -2095736
86 meter
Z = 17049373
33 Z = 5214501
13
XDOT = 9877
895008 XDOT = 2927
963700
YDOT = 23132
788950 feet/sec YDOT = 7084
079315 meter/sec
ZDOT = 2533
085660 ZDOT = 786
510737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12232320
87 X = 3728411
40
Y = -6516727
90 feet Y = -1986298
67 meter
Z = 17121719
18 Z = 5218700
01
XDOT = 8436
446418 XDOT = 2571
428868
YDOT = 22623
604708 feet/sec YDOT = 6895
674715 meter/sec
ZDOT = 2591
188783 ZDOT = 789
794341
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 11150
35720638
00016717 00000-0 10270-3 0 9076
2 25544 51
6444 252
1176 0004375 340
0692 20
0300 15
75744610 38100
Satellite: ISS
Catalog Number: 25544
Epoch time: 11150
35720638 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 252
1176 deg
Eccentricity:
0004375
Arg of perigee: 340
0692 deg
Mean anomaly: 20
0300 deg
Mean motion: 15
75744610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3810
Checksum: 270
Coasting Arc #9 (Orbit 3824)
---------------------------------------
Vector Time (GMT): 2011/151/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2743131
48 A = 6726936
27 meter
Y = -6132600
79 meter E =
0014648
Z = -62305
45 I = 51
34956
XDOT = 4373
963205 Wp = 29
80021
YDOT = -2011
371706 meter/sec RA = 246
32584 deg
ZDOT = 6018
894993 TA = 329
51940
MA = 329
60447
Ha = 187
404 n
mi
Hp = 181
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8999775
18 X = -2674049
00
Y = -20120081
33 feet Y = -6162889
88 meter
Z = -204414
22 Z = -75464
79
XDOT = 14350
272981 XDOT = 4366
890582
YDOT = -6598
988537 feet/sec YDOT = -1962
499754 meter/sec
ZDOT = 19747
030817 ZDOT = 6040
126534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8521910
71 X = -2597478
38
Y = -20326489
56 feet Y = -6195514
02 meter
Z = -257432
54 Z = -78465
44
XDOT = 12900
833054 XDOT = 3932
173915
YDOT = -5639
527807 feet/sec YDOT = -1718
928075 meter/sec
ZDOT = 19833
056151 ZDOT = 6045
115515
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 11151
30845072
00016717 00000-0 10270-3 0 9083
2 25544 51
6451 247
2199 0004294 342
7990 17
3028 15
75842641 38253
Satellite: ISS
Catalog Number: 25544
Epoch time: 11151
30845072 = yrday
fracday
Element set: 908
Inclination: 51
6451 deg
RA of node: 247
2199 deg
Eccentricity:
0004294
Arg of perigee: 342
7990 deg
Mean anomaly: 17
3028 deg
Mean motion: 15
75842641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3825
Checksum: 310
Coasting Arc #10 (Orbit 3840)
---------------------------------------
Vector Time (GMT): 2011/152/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4015938
52 A = 6714834
68 meter
Y = 1365371
12 meter E =
0014233
Z = -5217198
57 I = 51
32300
XDOT = -3223
203585 Wp = 78
36426
YDOT = -6954
783819 meter/sec RA = 241
15054 deg
ZDOT = 665
313964 TA = 197
96977
MA = 198
02014
Ha = 187
471 n
mi
Hp = 180
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13175651
31 X = -4005563
41
Y = 4479564
05 feet Y = 1320521
27 meter
Z = -17116793
22 Z = -5236682
80
XDOT = -10574
814913 XDOT = -3148
426307
YDOT = -22817
532215 feet/sec YDOT = -6990
409638 meter/sec
ZDOT = 2182
788595 ZDOT = 649
836040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13100957
04 X = -3993171
71
Y = 4395543
46 feet Y = 1339761
65 meter
Z = -17195726
62 Z = -5241257
47
XDOT = -10121
913828 XDOT = -3085
159335
YDOT = -21928
944195 feet/sec YDOT = -6683
942191 meter/sec
ZDOT = 2120
410259 ZDOT = 646
301047
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 11152
32308092
00016717 00000-0 10270-3 0 9093
2 25544 51
6454 241
9963 0004304 348
3508 11
7556 15
75896840 38417
Satellite: ISS
Catalog Number: 25544
Epoch time: 11152
32308092 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 241
9963 deg
Eccentricity:
0004304
Arg of perigee: 348
3508 deg
Mean anomaly: 11
7556 deg
Mean motion: 15
75896840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3841
Checksum: 314
Coasting Arc #11 (Orbit 3856)
---------------------------------------
Vector Time (GMT): 2011/153/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2834946
38 A = 6725918
77 meter
Y = 5971115
41 meter E =
0005688
Z = -1237976
36 I = 51
37640
XDOT = -4884
859146 Wp = 119
68410
YDOT = 1111
769498 meter/sec RA = 235
99675 deg
ZDOT = -5846
723535 TA = 73
94469
MA = 73
88207
Ha = 187
528 n
mi
Hp = 180
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9301005
17 X = 2773979
42
Y = 19590273
67 feet Y = 6002476
83 meter
Z = -4061602
23 Z = -1224351
19
XDOT = -16026
440769 XDOT = -4868
525588
YDOT = 3647
537724 feet/sec YDOT = 1057
236334 meter/sec
ZDOT = -19182
163828 ZDOT = -5870
414493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9537096
55 X = 2906907
03
Y = 19487803
13 feet Y = 5939882
39 meter
Z = -4006675
81 Z = -1221234
79
XDOT = -14449
534822 XDOT = -4404
218214
YDOT = 3123
490878 feet/sec YDOT = 952
040020 meter/sec
ZDOT = -19278
127361 ZDOT = -5875
973220
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 11153
33767680
00016717 00000-0 10270-3 0 9109
2 25544 51
6448 236
7709 0004555 351
9688 8
1402 15
75970927 38573
Satellite: ISS
Catalog Number: 25544
Epoch time: 11153
33767680 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 236
7709 deg
Eccentricity:
0004555
Arg of perigee: 351
9688 deg
Mean anomaly: 8
1402 deg
Mean motion: 15
75970927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3857
Checksum: 336
Coasting Arc #12 (Orbit 3872)
---------------------------------------
Vector Time (GMT): 2011/154/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4553666
52 A = 6716049
02 meter
Y = -610447
85 meter E =
0009266
Z = 4896881
54 I = 51
36111
XDOT = 3216
391818 Wp = 32
91022
YDOT = 6663
526738 meter/sec RA = 230
79796 deg
ZDOT = -2150
703251 TA = 78
07856
MA = 77
97468
Ha = 187
519 n
mi
Hp = 180
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14939850
80 X = 4536366
00
Y = -2002781
65 feet Y = -559623
55 meter
Z = 16065884
31 Z = 4918961
19
XDOT = 10552
466594 XDOT = 3152
087685
YDOT = 21861
964362 feet/sec YDOT = 6699
135205 meter/sec
ZDOT = -7056
113027 ZDOT = -2135
233034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14781223
30 X = 4505316
86
Y = -2417469
19 feet Y = -736844
61 meter
Z = 16155314
76 Z = 4924139
94
XDOT = 11027
223940 XDOT = 3361
097857
YDOT = 20478
060622 feet/sec YDOT = 6241
712878 meter/sec
ZDOT = -6993
731829 ZDOT = -2131
689462
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 11154
35224288
00016717 00000-0 10270-3 0 9115
2 25544 51
6447 231
5461 0004374 357
0937 3
0202 15
75950742 38736
Satellite: ISS
Catalog Number: 25544
Epoch time: 11154
35224288 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 231
5461 deg
Eccentricity:
0004374
Arg of perigee: 357
0937 deg
Mean anomaly: 3
0202 deg
Mean motion: 15
75950742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 295
Coasting Arc #13 (Orbit 3888)
---------------------------------------
Vector Time (GMT): 2011/155/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2707052
38 A = 6723627
09 meter
Y = -5616868
20 meter E =
0015505
Z = 2492011
81 I = 51
40885
XDOT = 5588
118563 Wp = 59
69871
YDOT = -333
826420 meter/sec RA = 225
66871 deg
ZDOT = 5301
164482 TA = 328
64887
MA = 328
74122
Ha = 187
498 n
mi
Hp = 180
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8881405
46 X = -2656148
01
Y = -18428045
29 feet Y = -5646855
90 meter
Z = 8175891
75 Z = 2478983
68
XDOT = 18333
722318 XDOT = 5565
684092
YDOT = -1095
231037 feet/sec YDOT = -271
463000 meter/sec
ZDOT = 17392
271922 ZDOT = 5328
256980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9754704
58 X = -2973233
96
Y = -18004844
02 feet Y = -5487876
46 meter
Z = 8123346
13 Z = 2475995
90
XDOT = 16847
952729 XDOT = 5135
255992
YDOT = -1206
511246 feet/sec YDOT = -367
744628 meter/sec
ZDOT = 17502
003579 ZDOT = 5334
610691
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 11155
36677190
00016717 00000-0 10270-3 0 9122
2 25544 51
6456 226
3213 0004369 359
1619
9537 15
76068528 38894
Satellite: ISS
Catalog Number: 25544
Epoch time: 11155
36677190 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 226
3213 deg
Eccentricity:
0004369
Arg of perigee: 359
1619 deg
Mean anomaly:
9537 deg
Mean motion: 15
76068528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 330
Coasting Arc #14 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2011/156/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5208663
72 A = 6718282
83 meter
Y = 14435
14 meter E =
0008444
Z = -4249463
52 I = 51
41354
XDOT = -2901
111399 Wp = 80
09887
YDOT = -6188
422952 meter/sec RA = 220
45543 deg
ZDOT = 3542
329164 TA = 225
92997
MA = 225
99953
Ha = 187
541 n
mi
Hp = 180
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17088791
73 X = -5187794
99
Y = 47359
38 feet Y = -43693
97 meter
Z = -13941809
44 Z = -4274716
40
XDOT = -9518
082019 XDOT = -2848
903555
YDOT = -20303
224907 feet/sec YDOT = -6220
573570 meter/sec
ZDOT = 11621
814842 ZDOT = 3528
361500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16968771
12 X = -5172081
44
Y = 1107876
95 feet Y = 337680
89 meter
Z = -14044091
70 Z = -4280639
15
XDOT = -10755
264309 XDOT = -3278
204561
YDOT = -18427
338406 feet/sec YDOT = -5616
652746 meter/sec
ZDOT = 11565
472029 ZDOT = 3525
155874
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 11156
31786668
00016717 00000-0 10270-3 0 9130
2 25544 51
6455 221
4234 0004546 2
8432 357
2758 15
76078477 39049
Satellite: ISS
Catalog Number: 25544
Epoch time: 11156
31786668 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 221
4234 deg
Eccentricity:
0004546
Arg of perigee: 2
8432 deg
Mean anomaly: 357
2758 deg
Mean motion: 15
76078477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 323
Coasting Arc #15 (Orbit 3919)
---------------------------------------
Vector Time (GMT): 2011/157/07:23:56
914
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2260225
44 A = 6720343
30 meter
Y = 5173827
80 meter E =
0008193
Z = -3655099
98 I = 51
44500
XDOT = -6356
951072 Wp = 48
01557
YDOT = -279
506474 meter/sec RA = 215
33953 deg
ZDOT = -4327
437544 TA = 176
00601
MA = 175
99946
Ha = 187
608 n
mi
Hp = 180
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7415437
80 X = 2219958
41
Y = 16974500
67 feet Y = 5198878
36 meter
Z = -11991797
84 Z = -3644216
99
XDOT = -20856
138687 XDOT = -6332
331345
YDOT = -917
015991 feet/sec YDOT = -350
455528 meter/sec
ZDOT = -14197
629736 ZDOT = -4358
259648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8814120
57 X = 2686543
95
Y = 16324355
38 feet Y = 4975663
52 meter
Z = -11947899
65 Z = -3641719
81
XDOT = -19587
347144 XDOT = -5970
223410
YDOT = 95
169934 feet/sec YDOT = 29
007796 meter/sec
ZDOT = -14322
472927 ZDOT = -4365
489748
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 11157
33233560
00016717 00000-0 10270-3 0 9142
2 25544 51
6456 216
1973 0004552 6
7100 353
4124 15
76131567 39206
Satellite: ISS
Catalog Number: 25544
Epoch time: 11157
33233560 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 216
1973 deg
Eccentricity:
0004552
Arg of perigee: 6
7100 deg
Mean anomaly: 353
4124 deg
Mean motion: 15
76131567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 282
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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