[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 2nd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 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
There are no maneuvers
Coasting Arc #1 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2011/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4188807
93 A = 6759599
35 meter
Y = 822440
66 meter E =
0012349
Z = 5233136
05 I = 51
30267
XDOT = -2321
268659 Wp = 41
20079
YDOT = 7291
744598 meter/sec RA = 291
98255 deg
ZDOT = 720
243232 TA = 41
95053
MA = 41
85600
Ha = 214
905 n
mi
Hp = 202
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13742808
18 X = 4153878
93
Y = 2698296
13 feet Y = 869086
99 meter
Z = 17169081
53 Z = 5253399
96
XDOT = -7615
710825 XDOT = -2406
132566
YDOT = 23923
046582 feet/sec YDOT = 7265
312232 meter/sec
ZDOT = 2363
002730 ZDOT = 708
760909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6477216
47 X = -1974255
58
Y = -12302828
34 feet Y = -3749902
08 meter
Z = 17251348
38 Z = 5258210
99
XDOT = 22502
617182 XDOT = 6858
797717
YDOT = -8637
164314 feet/sec YDOT = -2632
607683 meter/sec
ZDOT = 2315
967969 ZDOT = 705
907037
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 11213
54927377
00016717 00000-0 10270-3 0 9009
2 25544 51
6412 292
4129 0011968 27
2631 332
9151 15
60296722 7995
Satellite: ISS
Catalog Number: 25544
Epoch time: 11213
54927377 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 292
4129 deg
Eccentricity:
0011968
Arg of perigee: 27
2631 deg
Mean anomaly: 332
9151 deg
Mean motion: 15
60296722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 308
Coasting Arc #2 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2011/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2280347
91 A = 6763110
36 meter
Y = -4612748
74 meter E =
0016518
Z = -4397595
40 I = 51
30300
XDOT = 4402
460180 Wp = 64
18595
YDOT = -5329
693744 meter/sec RA = 286
89934 deg
ZDOT = 3324
391268 TA = 239
46384
MA = 239
62697
Ha = 215
116 n
mi
Hp = 201
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7481456
38 X = -2207235
50
Y = -15133690
08 feet Y = -4637840
10 meter
Z = -14427806
43 Z = -4408495
59
XDOT = 14443
766994 XDOT = 4445
581699
YDOT = -17485
871864 feet/sec YDOT = -5280
221705 meter/sec
ZDOT = 10906
795498 ZDOT = 3345
882611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6855166
00 X = -2089454
60
Y = 15386190
97 feet Y = 4689711
01 meter
Z = -14471841
28 Z = -4411017
22
XDOT = -21514
686297 XDOT = -6557
676383
YDOT = 703
634947 feet/sec YDOT = 214
467932 meter/sec
ZDOT = 10994
370809 ZDOT = 3351
084223
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 11214
51000260
00016717 00000-0 10270-3 0 9011
2 25544 51
6400 287
5799 0012155 31
4023 328
7856 15
60310636 8145
Satellite: ISS
Catalog Number: 25544
Epoch time: 11214
51000260 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 287
5799 deg
Eccentricity:
0012155
Arg of perigee: 31
4023 deg
Mean anomaly: 328
7856 deg
Mean motion: 15
60310636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 814
Checksum: 270
Coasting Arc #3 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2011/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -263599
83 A = 6770579
07 meter
Y = 6622537
91 meter E =
0019314
Z = 1377073
59 I = 51
32008
XDOT = -4943
087946 Wp = 80
26729
YDOT = 1020
395816 meter/sec RA = 281
85433 deg
ZDOT = -5780
905126 TA = 84
62772
MA = 84
40740
Ha = 215
262 n
mi
Hp = 201
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -864828
83 X = -344324
21
Y = 21727486
58 feet Y = 6619138
80 meter
Z = 4517957
97 Z = 1375597
06
XDOT = -16217
480138 XDOT = -4926
048695
YDOT = 3347
755302 feet/sec YDOT = 965
214544 meter/sec
ZDOT = -18966
224168 ZDOT = -5804
876854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16999629
82 X = 5181487
17
Y = -13561024
59 feet Y = -4133400
30 meter
Z = 4511623
26 Z = 1375142
77
XDOT = 12089
566447 XDOT = 3684
899853
YDOT = 8733
492778 feet/sec YDOT = 2661
968599 meter/sec
ZDOT = -19063
647376 ZDOT = -5810
599720
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 11215
53476598
00016717 00000-0 10270-3 0 9026
2 25544 51
6397 282
4228 0012299 34
7430 325
4527 15
60321703 8302
Satellite: ISS
Catalog Number: 25544
Epoch time: 11215
53476598 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 282
4228 deg
Eccentricity:
0012299
Arg of perigee: 34
7430 deg
Mean anomaly: 325
4527 deg
Mean motion: 15
60321703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 302
Coasting Arc #4 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2011/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2529031
58 A = 6769183
93 meter
Y = -5838060
69 meter E =
0025112
Z = 2268364
59 I = 51
30987
XDOT = 3911
439322 Wp = 56
37939
YDOT = 3809
929057 meter/sec RA = 276
83130 deg
ZDOT = 5415
182200 TA = 329
10398
MA = 329
25150
Ha = 215
301 n
mi
Hp = 201
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8297347
70 X = 2583106
77
Y = -19153742
42 feet Y = -5809477
21 meter
Z = 7442141
04 Z = 2280781
70
XDOT = 12832
806174 XDOT = 3842
239589
YDOT = 12499
767247 feet/sec YDOT = 3853
282123 meter/sec
ZDOT = 17766
345800 ZDOT = 5434
015740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19765365
34 X = -6024483
36
Y = 6654661
74 feet Y = 2028340
90 meter
Z = 7492870
00 Z = 2283826
78
XDOT = 1285
824880 XDOT = 391
919423
YDOT = -16379
092606 feet/sec YDOT = -4992
347426 meter/sec
ZDOT = 17842
656203 ZDOT = 5438
441611
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 11216
55951643
00016717 00000-0 10270-3 0 9039
2 25544 51
6394 277
2660 0012353 38
7226 321
4813 15
60314368 8469
Satellite: ISS
Catalog Number: 25544
Epoch time: 11216
55951643 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 277
2660 deg
Eccentricity:
0012353
Arg of perigee: 38
7226 deg
Mean anomaly: 321
4813 deg
Mean motion: 15
60314368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 302
Coasting Arc #5 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2011/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3971220
90 A = 6761266
05 meter
Y = 2572043
06 meter E =
0023417
Z = -4851819
60 I = 51
28065
XDOT = -1684
443973 Wp = 57
14806
YDOT = -7085
948910 meter/sec RA = 271
77320 deg
ZDOT = -2373
563243 TA = 189
43104
MA = 189
47509
Ha = 215
397 n
mi
Hp = 201
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13028939
97 X = -3976117
80
Y = 8438461
47 feet Y = 2527607
25 meter
Z = -15918043
30 Z = -4871123
40
XDOT = -5526
390989 XDOT = -1593
552091
YDOT = -23247
863877 feet/sec YDOT = -7104
277093 meter/sec
ZDOT = -7787
280982 ZDOT = -2381
525694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14984812
32 X = 4567370
79
Y = 3729579
53 feet Y = 1136775
84 meter
Z = -15996582
38 Z = -4875758
31
XDOT = -13027
602706 XDOT = -3970
813305
YDOT = 18747
308732 feet/sec YDOT = 5714
179701 meter/sec
ZDOT = -7819
275914 ZDOT = -2383
315299
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 11217
52020775
00016717 00000-0 10270-3 0 9041
2 25544 51
6391 272
4311 0012330 42
1297 318
0805 15
60326059 8618
Satellite: ISS
Catalog Number: 25544
Epoch time: 11217
52020775 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 272
4311 deg
Eccentricity:
0012330
Arg of perigee: 42
1297 deg
Mean anomaly: 318
0805 deg
Mean motion: 15
60326059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 273
Coasting Arc #6 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2011/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4134829
11 A = 6760284
98 meter
Y = 1832872
56 meter E =
0017836
Z = 5016192
43 I = 51
27832
XDOT = -1039
750501 Wp = 48
38451
YDOT = 7392
306998 meter/sec RA = 266
68282 deg
ZDOT = -1828
139504 TA = 59
45423
MA = 59
27832
Ha = 215
260 n
mi
Hp = 201
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13565712
30 X = 4089658
73
Y = 6013361
42 feet Y = 1878857
88 meter
Z = 16457324
24 Z = 5036169
64
XDOT = -3411
254924 XDOT = -1113
454748
YDOT = 24252
975715 feet/sec YDOT = 7380
267881 meter/sec
ZDOT = -5997
833019 ZDOT = -1833
369150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5001202
12 X = -1524366
40
Y = -13874521
03 feet Y = -4228954
01 meter
Z = 16538386
57 Z = 5040900
23
XDOT = 18806
870232 XDOT = 5732
334047
YDOT = -14016
069039 feet/sec YDOT = -4272
097843 meter/sec
ZDOT = -6019
436184 ZDOT = -1834
724149
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 11218
54493067
00016717 00000-0 10270-3 0 9053
2 25544 51
6392 267
2742 0012384 45
3958 314
8206 15
60393974 8773
Satellite: ISS
Catalog Number: 25544
Epoch time: 11218
54493067 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 267
2742 deg
Eccentricity:
0012384
Arg of perigee: 45
3958 deg
Mean anomaly: 314
8206 deg
Mean motion: 15
60393974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 330
Coasting Arc #7 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2011/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3022592
58 A = 6767857
55 meter
Y = -5392239
31 meter E =
0017265
Z = -2752081
23 I = 51
30676
XDOT = 3474
651788 Wp = 52
29021
YDOT = -4543
638729 meter/sec RA = 261
61832 deg
ZDOT = 5118
686973 TA = 276
30394
MA = 276
50055
Ha = 215
422 n
mi
Hp = 200
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9916642
33 X = -2948701
90
Y = -17691073
84 feet Y = -5425626
42 meter
Z = -9029137
91 Z = -2766585
77
XDOT = 11399
776207 XDOT = 3500
336013
YDOT = -14906
951209 feet/sec YDOT = -4504
639848 meter/sec
ZDOT = 16793
592431 ZDOT = 5135
628676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5579204
96 X = -1700541
67
Y = 19471094
36 feet Y = 5934789
56 meter
Z = -9087803
71 Z = -2769962
57
XDOT = -17115
187476 XDOT = -5216
709143
YDOT = 2916
938746 feet/sec YDOT = 889
082930 meter/sec
ZDOT = 16862
635253 ZDOT = 5139
731225
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 11219
50559936
00016717 00000-0 10270-3 0 9069
2 25544 51
6393 262
4397 0012548 49
6876 310
5374 15
60405370 8925
Satellite: ISS
Catalog Number: 25544
Epoch time: 11219
50559936 = yrday
fracday
Element set: 906
Inclination: 51
6393 deg
RA of node: 262
4397 deg
Eccentricity:
0012548
Arg of perigee: 49
6876 deg
Mean anomaly: 310
5374 deg
Mean motion: 15
60405370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 328
Coasting Arc #8 (Orbit 907)
---------------------------------------
Vector Time (GMT): 2011/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 815625
65 A = 6770735
30 meter
Y = 6657627
87 meter E =
0016368
Z = -937226
50 I = 51
32231
XDOT = -4902
994642 Wp = 90
61046
YDOT = -216
629185 meter/sec RA = 256
59320 deg
ZDOT = -5895
166875 TA = 99
60001
MA = 99
41504
Ha = 215
543 n
mi
Hp = 200
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2675937
17 X = 745670
95
Y = 21842611
11 feet Y = 6666357
64 meter
Z = -3074890
10 Z = -933433
58
XDOT = -16085
940428 XDOT = -4871
570621
YDOT = -710
725673 feet/sec YDOT = -271
281234 meter/sec
ZDOT = -19341
098671 ZDOT = -5918
908965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13278037
65 X = 4047145
88
Y = -17551257
25 feet Y = -5349623
21 meter
Z = -3059793
15 Z = -932624
95
XDOT = 9684
509448 XDOT = 2951
838480
YDOT = 10663
821532 feet/sec YDOT = 3250
332803 meter/sec
ZDOT = -19437
548040 ZDOT = -5924
564643
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 11220
53029800
00016717 00000-0 10270-3 0 9077
2 25544 51
6396 257
2821 0012662 53
1483 307
0832 15
60415180 9081
Satellite: ISS
Catalog Number: 25544
Epoch time: 11220
53029800 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 257
2821 deg
Eccentricity:
0012662
Arg of perigee: 53
1483 deg
Mean anomaly: 307
0832 deg
Mean motion: 15
60415180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 908
Checksum: 282
Coasting Arc #9 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2011/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1782201
68 A = 6763834
83 meter
Y = -5053026
66 meter E =
0021339
Z = 4106837
93 I = 51
30592
XDOT = 4752
515983 Wp = 78
12246
YDOT = 4739
109960 meter/sec RA = 251
55356 deg
ZDOT = 3756
380533 TA = 333
08511
MA = 333
19565
Ha = 215
569 n
mi
Hp = 200
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5847118
36 X = 1818623
26
Y = -16578171
44 feet Y = -5032893
71 meter
Z = 13473877
72 Z = 4115583
72
XDOT = 15592
244038 XDOT = 4680
921653
YDOT = 15548
261023 feet/sec YDOT = 4791
854854 meter/sec
ZDOT = 12324
083115 ZDOT = 3779
294329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15544878
34 X = -4738078
92
Y = 8149613
05 feet Y = 2484002
06 meter
Z = 13509644
96 Z = 4117739
78
XDOT = -90
918850 XDOT = -27
712066
YDOT = -20823
200072 feet/sec YDOT = -6346
911382 meter/sec
ZDOT = 12416
969468 ZDOT = 3784
692294
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 11221
55498387
00016717 00000-0 10270-3 0 9081
2 25544 51
6383 252
1252 0012788 57
2279 303
0107 15
60417786 9249
Satellite: ISS
Catalog Number: 25544
Epoch time: 11221
55498387 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 252
1252 deg
Eccentricity:
0012788
Arg of perigee: 57
2279 deg
Mean anomaly: 303
0107 deg
Mean motion: 15
60417786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 314
Coasting Arc #10 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2011/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4001592
51 A = 6759114
53 meter
Y = 1411788
31 meter E =
0026484
Z = -5283347
28 I = 51
30174
XDOT = -2855
332879 Wp = 77
58179
YDOT = -7102
447764 meter/sec RA = 246
47076 deg
ZDOT = 271
485803 TA = 194
98181
MA = 195
06041
Ha = 215
590 n
mi
Hp = 200
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13128584
34 X = -3991417
05
Y = 4631851
42 feet Y = 1367097
37 meter
Z = -17333816
54 Z = -5302761
74
XDOT = -9367
890024 XDOT = -2777
018510
YDOT = -23301
993977 feet/sec YDOT = -7133
939979 meter/sec
ZDOT = 890
701455 ZDOT = 257
804598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12761787
14 X = 3889792
72
Y = 5311039
70 feet Y = 1618804
90 meter
Z = -17412771
65 Z = -5307412
80
XDOT = -8308
989408 XDOT = -2532
579972
YDOT = 22632
300589 feet/sec YDOT = 6898
325219 meter/sec
ZDOT = 835
420594 ZDOT = 254
636197
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 11222
51561381
00016717 00000-0 10270-3 0 9094
2 25544 51
6393 247
2907 0012633 60
2386 300
0025 15
60424754 9399
Satellite: ISS
Catalog Number: 25544
Epoch time: 11222
51561381 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 247
2907 deg
Eccentricity:
0012633
Arg of perigee: 60
2386 deg
Mean anomaly: 300
0025 deg
Mean motion: 15
60424754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 287
Coasting Arc #11 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2011/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4912288
01 A = 6764698
34 meter
Y = 2694673
09 meter E =
0023929
Z = 3776849
51 I = 51
33254
XDOT = -297
204996 Wp = 72
74492
YDOT = 6441
599570 meter/sec RA = 241
39174 deg
ZDOT = -4180
450820 TA = 61
53879
MA = 61
29793
Ha = 215
508 n
mi
Hp = 200
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16116430
48 X = 4863443
79
Y = 8840790
98 feet Y = 2749331
97 meter
Z = 12391238
55 Z = 3800594
29
XDOT = -975
082007 XDOT = -348
906791
YDOT = 21133
856856 feet/sec YDOT = 6437
987206 meter/sec
ZDOT = -13715
389829 ZDOT = -4182
019807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6250963
29 X = -1905293
61
Y = -17217039
37 feet Y = -5247753
60 meter
Z = 12487622
78 Z = 3806227
42
XDOT = 13331
959285 XDOT = 4063
581190
YDOT = -14861
309079 feet/sec YDOT = -4529
727007 meter/sec
ZDOT = -13722
039491 ZDOT = -4182
477637
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 11223
54027198
00016717 00000-0 10270-3 0 9103
2 25544 51
6375 242
1328 0012794 63
8135 296
4335 15
60491407 9558
Satellite: ISS
Catalog Number: 25544
Epoch time: 11223
54027198 = yrday
fracday
Element set: 910
Inclination: 51
6375 deg
RA of node: 242
1328 deg
Eccentricity:
0012794
Arg of perigee: 63
8135 deg
Mean anomaly: 296
4335 deg
Mean motion: 15
60491407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 305
Coasting Arc #12 (Orbit 969)
---------------------------------------
Vector Time (GMT): 2011/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4020773
14 A = 6770734
71 meter
Y = -5420833
28 meter E =
0023297
Z = -430955
94 I = 51
36884
XDOT = 3641
342386 Wp = 55
95103
YDOT = -3156
986250 meter/sec RA = 236
35977 deg
ZDOT = 5981
666904 TA = 299
37001
MA = 299
60246
Ha = 215
524 n
mi
Hp = 200
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13191512
92 X = -3957764
04
Y = -17784886
08 feet Y = -5465443
70 meter
Z = -1413897
45 Z = -450335
47
XDOT = 11946
661370 XDOT = 3647
316736
YDOT = -10357
566437 feet/sec YDOT = -3116
233353 meter/sec
ZDOT = 19624
891416 ZDOT = 5999
370452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1409870
36 X = -429728
48
Y = 22093034
47 feet Y = 6733956
91 meter
Z = -1492442
79 Z = -454896
56
XDOT = -14108
088020 XDOT = -4300
145228
YDOT = 378
945092 feet/sec YDOT = 115
502464 meter/sec
ZDOT = 19696
972553 ZDOT = 6003
637234
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 11224
50087769
00016717 00000-0 10270-3 0 9111
2 25544 51
6380 237
2985 0012729 67
9342 292
3164 15
60516721 9700
Satellite: ISS
Catalog Number: 25544
Epoch time: 11224
50087769 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 237
2985 deg
Eccentricity:
0012729
Arg of perigee: 67
9342 deg
Mean anomaly: 292
3164 deg
Mean motion: 15
60516721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 970
Checksum: 315
Coasting Arc #13 (Orbit 985)
---------------------------------------
Vector Time (GMT): 2011/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1368269
79 A = 6766519
39 meter
Y = 5809852
96 meter E =
0016881
Z = -3205392
84 I = 51
37095
XDOT = -5871
997506 Wp = 79
00995
YDOT = -1238
320596 meter/sec RA = 231
33438 deg
ZDOT = -4769
266980 TA = 138
26403
MA = 138
13513
Ha = 215
623 n
mi
Hp = 200
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4489074
11 X = 1318771
99
Y = 19061197
37 feet Y = 5824877
07 meter
Z = -10516380
71 Z = -3198866
11
XDOT = -19265
083680 XDOT = -5834
546334
YDOT = -4062
731615 feet/sec YDOT = -1303
775385 meter/sec
ZDOT = -15647
201378 ZDOT = -4797
701423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8523051
68 X = 2597826
15
Y = -17646279
57 feet Y = -5378586
01 meter
Z = -10490076
37 Z = -3197375
28
XDOT = 10997
651021 XDOT = 3352
084031
YDOT = 14646
530678 feet/sec YDOT = 4464
262551 meter/sec
ZDOT = -15762
729504 ZDOT = -4804
479953
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 11225
52550946
00016717 00000-0 10270-3 0 9127
2 25544 51
6368 232
1396 0012744 71
2926 288
9612 15
60495348 9866
Satellite: ISS
Catalog Number: 25544
Epoch time: 11225
52550946 = yrday
fracday
Element set: 912
Inclination: 51
6368 deg
RA of node: 232
1396 deg
Eccentricity:
0012744
Arg of perigee: 71
2926 deg
Mean anomaly: 288
9612 deg
Mean motion: 15
60495348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 986
Checksum: 327
Coasting Arc #14 (Orbit 1001)
---------------------------------------
Vector Time (GMT): 2011/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2075750
02 A = 6759264
55 meter
Y = -3808318
02 meter E =
0015666
Z = 5170473
08 I = 51
36602
XDOT = 5891
249810 Wp = 86
18479
YDOT = 4803
775927 meter/sec RA = 226
26705 deg
ZDOT = 1171
079717 TA = 352
56352
MA = 352
58673
Ha = 215
533 n
mi
Hp = 200
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6810203
47 X = 2093064
50
Y = -12494481
70 feet Y = -3785008
88 meter
Z = 16963494
35 Z = 5180598
90
XDOT = 19328
247409 XDOT = 5831
406450
YDOT = 15760
419709 feet/sec YDOT = 4869
320882 meter/sec
ZDOT = 3842
125057 ZDOT = 1199
553313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13000345
55 X = -3962505
32
Y = 5663835
03 feet Y = 1726336
92 meter
Z = 17004795
59 Z = 5183061
70
XDOT = -4999
747108 XDOT = -1523
922918
YDOT = -23378
376719 feet/sec YDOT = -7125
729224 meter/sec
ZDOT = 3957
690470 ZDOT = 1206
304055
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 11226
55012701
00016717 00000-0 10270-3 0 9134
2 25544 51
6361 226
9813 0012755 74
7366 285
5199 15
60522215 10029
Satellite: ISS
Catalog Number: 25544
Epoch time: 11226
55012701 = yrday
fracday
Element set: 913
Inclination: 51
6361 deg
RA of node: 226
9813 deg
Eccentricity:
0012755
Arg of perigee: 74
7366 deg
Mean anomaly: 285
5199 deg
Mean motion: 15
60522215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1002
Checksum: 287
Coasting Arc #15 (Orbit 1016)
---------------------------------------
Vector Time (GMT): 2011/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4977774
91 A = 6761800
57 meter
Y = 492154
30 meter E =
0022058
Z = -4569450
08 I = 51
39667
XDOT = -3381
177507 Wp = 92
47031
YDOT = -6172
933492 meter/sec RA = 221
18437 deg
ZDOT = 3030
198089 TA = 207
86894
MA = 207
98727
Ha = 215
584 n
mi
Hp = 199
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16331282
50 X = -4960711
23
Y = 1614679
48 feet Y = 436585
10 meter
Z = -14991634
12 Z = -4593590
15
XDOT = -11093
102056 XDOT = -3326
619101
YDOT = -20252
406470 feet/sec YDOT = -6210
438768 meter/sec
ZDOT = 9941
594779 ZDOT = 3013
905332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13905817
98 X = 4238493
32
Y = 8543634
72 feet Y = 2604099
86 meter
Z = -15089784
74 Z = -4599366
39
XDOT = -2754
357501 XDOT = -839
528166
YDOT = 21857
754876 feet/sec YDOT = 6662
243686 meter/sec
ZDOT = 9875
581069 ZDOT = 3010
077110
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 11227
51069263
00016717 00000-0 10270-3 0 9147
2 25544 51
6364 222
1464 0012721 77
8649 282
3931 15
60521444 10171
Satellite: ISS
Catalog Number: 25544
Epoch time: 11227
51069263 = yrday
fracday
Element set: 914
Inclination: 51
6364 deg
RA of node: 222
1464 deg
Eccentricity:
0012721
Arg of perigee: 77
8649 deg
Mean anomaly: 282
3931 deg
Mean motion: 15
60521444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1017
Checksum: 292
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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