[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 5th 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 2429)
---------------------------------------
Vector Time (GMT): 2011/062/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1040957
46 A = 6725580
37 meter
Y = -4066957
71 meter E =
0018261
Z = -5269244
38 I = 51
52115
XDOT = 7355
210175 Wp = 72
35182
YDOT = -2212
745108 meter/sec RA = 341
70895 deg
ZDOT = 260
991288 TA = 200
09847
MA = 200
17047
Ha = 194
721 n
mi
Hp = 185
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3415214
76 X = -969806
26
Y = -13343037
12 feet Y = -4078201
03 meter
Z = -17287547
18 Z = -5274127
99
XDOT = 24131
266978 XDOT = 7378
139042
YDOT = -7259
662429 feet/sec YDOT = -2130
366465 meter/sec
ZDOT = 856
270630 ZDOT = 296
777837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9741802
21 X = -2969301
31
Y = -9701545
88 feet Y = -2957031
18 meter
Z = -17307134
83 Z = -5275214
70
XDOT = 16174
706685 XDOT = 4930
050597
YDOT = -17991
092540 feet/sec YDOT = -5483
685006 meter/sec
ZDOT = 1000
798190 ZDOT = 305
043288
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 11062
65680937
00016717 00000-0 10270-3 0 9001
2 25544 51
6475 342
1580 0006507 22
2637 337
8806 15
72090873 24309
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
65680937 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 342
1580 deg
Eccentricity:
0006507
Arg of perigee: 22
2637 deg
Mean anomaly: 337
8806 deg
Mean motion: 15
72090873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2430
Checksum: 304
Coasting Arc #2 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2011/063/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6050172
50 A = 6737565
09 meter
Y = 2936681
90 meter E =
0012787
Z = 364985
80 I = 51
53290
XDOT = -2395
049308 Wp = 102
41667
YDOT = -4165
766503 meter/sec RA = 336
57988 deg
ZDOT = -6009
487260 TA = 73
61455
MA = 73
47401
Ha = 194
764 n
mi
Hp = 185
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19849647
31 X = -6084334
37
Y = 9634783
13 feet Y = 2868834
24 meter
Z = 1197459
96 Z = 335511
45
XDOT = -7857
773320 XDOT = -2319
096593
YDOT = -13667
212937 feet/sec YDOT = -4192
125390 meter/sec
ZDOT = -19716
165552 ZDOT = -6020
937185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11679495
87 X = -3559910
34
Y = 18726929
42 feet Y = 5707968
09 meter
Z = 1078399
43 Z = 328696
15
XDOT = -12462
609717 XDOT = -3798
603442
YDOT = -6598
055198 feet/sec YDOT = -2011
087224 meter/sec
ZDOT = -19762
257453 ZDOT = -6023
536072
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
67387521
00016717 00000-0 10270-3 0 9018
2 25544 51
6475 336
9509 0006348 26
8032 333
3457 15
72091012 24469
Satellite: ISS
Catalog Number: 25544
Epoch time: 11063
67387521 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 336
9509 deg
Eccentricity:
0006348
Arg of perigee: 26
8032 deg
Mean anomaly: 333
3457 deg
Mean motion: 15
72091012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2446
Checksum: 301
Coasting Arc #3 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2011/064/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3045487
98 A = 6725739
06 meter
Y = 3029869
28 meter E =
0007210
Z = 5169027
95 I = 51
46544
XDOT = -6233
951640 Wp = 60
34964
YDOT = 4389
598679 meter/sec RA = 331
46075 deg
ZDOT = 1102
283834 TA = 19
12395
MA = 19
09690
Ha = 194
677 n
mi
Hp = 185
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9991758
45 X = 2986271
34
Y = 9940516
01 feet Y = 3063595
28 meter
Z = 16958753
13 Z = 5183678
46
XDOT = -20452
597244 XDOT = -6287
928237
YDOT = 14401
570470 feet/sec YDOT = 4319
585185 meter/sec
ZDOT = 3616
416778 ZDOT = 1071
868268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13716705
50 X = 4180851
84
Y = 2914613
64 feet Y = 888374
24 meter
Z = 17017797
18 Z = 5187024
58
XDOT = -9053
243694 XDOT = -2759
428678
YDOT = 22253
429202 feet/sec YDOT = 6782
845221 meter/sec
ZDOT = 3493
523771 ZDOT = 1064
826045
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
69090840
00016717 00000-0 10270-3 0 9027
2 25544 51
6468 331
7424 0006423 29
8800 330
2728 15
72150050 24623
Satellite: ISS
Catalog Number: 25544
Epoch time: 11064
69090840 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 331
7424 deg
Eccentricity:
0006423
Arg of perigee: 29
8800 deg
Mean anomaly: 330
2728 deg
Mean motion: 15
72150050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 284
Coasting Arc #4 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2011/065/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4675612
30 A = 6736308
58 meter
Y = -4589940
29 meter E =
0014644
Z = -1538247
23 I = 51
47384
XDOT = 4409
918103 Wp = 34
55000
YDOT = 2573
915886 meter/sec RA = 326
30304 deg
ZDOT = 5762
603224 TA = 308
46296
MA = 308
59426
Ha = 194
714 n
mi
Hp = 185
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15339935
35 X = 4734062
79
Y = -15058859
22 feet Y = -4537328
12 meter
Z = -5046742
87 Z = -1515390
94
XDOT = 14468
235246 XDOT = 4352
815064
YDOT = 8444
605924 feet/sec YDOT = 2622
911656 meter/sec
ZDOT = 18906
178556 ZDOT = 5783
887277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4270932
90 X = 1301780
35
Y = -21089473
47 feet Y = -6428071
51 meter
Z = -4954362
94 Z = -1510089
83
XDOT = 15083
006160 XDOT = 4597
300278
YDOT = -1376
792502 feet/sec YDOT = -419
646354 meter/sec
ZDOT = 18992
007111 ZDOT = 5788
763767
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
64434811
00016717 00000-0 10270-3 0 9034
2 25544 51
6456 326
8591 0006354 31
8026 328
3519 15
72200604 24779
Satellite: ISS
Catalog Number: 25544
Epoch time: 11065
64434811 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 326
8591 deg
Eccentricity:
0006354
Arg of perigee: 31
8026 deg
Mean anomaly: 328
3519 deg
Mean motion: 15
72200604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2477
Checksum: 297
Coasting Arc #5 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2011/066/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4473309
21 A = 6726854
63 meter
Y = -1368678
30 meter E =
0017645
Z = -4850316
10 I = 51
41652
XDOT = 4343
884124 Wp = 60
44552
YDOT = -5890
125171 meter/sec RA = 321
19974 deg
ZDOT = -2341
978854 TA = 186
59526
MA = 186
61851
Ha = 194
643 n
mi
Hp = 184
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14676211
33 X = -4434110
23
Y = -4490414
38 feet Y = -1418482
92 meter
Z = -15913110
57 Z = -4871951
83
XDOT = 14251
588333 XDOT = 4420
802558
YDOT = -19324
557646 feet/sec YDOT = -5841
119411 meter/sec
ZDOT = -7683
657658 ZDOT = -2320
689020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14509822
02 X = -4422593
75
Y = 4715367
59 feet Y = 1437244
04 meter
Z = -16000389
43 Z = -4876918
70
XDOT = 919
887416 XDOT = 280
381684
YDOT = -22973
781204 feet/sec YDOT = -7002
408511 meter/sec
ZDOT = -7597
569420 ZDOT = -2315
739159
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
66132122
00016717 00000-0 10270-3 0 9048
2 25544 51
6442 321
6500 0006273 36
2240 323
9346 15
72258143 24932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11066
66132122 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 321
6500 deg
Eccentricity:
0006273
Arg of perigee: 36
2240 deg
Mean anomaly: 323
9346 deg
Mean motion: 15
72258143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 274
Coasting Arc #6 (Orbit 2508)
---------------------------------------
Vector Time (GMT): 2011/067/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2846307
36 A = 6734128
49 meter
Y = 5549210
36 meter E =
0017319
Z = 2528055
95 I = 51
41927
XDOT = -5591
183590 Wp = 84
52985
YDOT = -450
616145 meter/sec RA = 316
02109 deg
ZDOT = -5273
331985 TA = 66
74825
MA = 66
56600
Ha = 194
539 n
mi
Hp = 184
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9338278
75 X = -2920428
88
Y = 18206070
72 feet Y = 5516967
04 meter
Z = 8294146
83 Z = 2514048
12
XDOT = -18343
778181 XDOT = -5560
112478
YDOT = -1478
399427 feet/sec YDOT = -512
966941 meter/sec
ZDOT = -17300
957957 ZDOT = -5300
418212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3144790
81 X = 958532
24
Y = 20241340
39 feet Y = 6169560
55 meter
Z = 8237460
94 Z = 2510778
09
XDOT = -14131
869183 XDOT = -4307
393727
YDOT = 9324
721323 feet/sec YDOT = 2842
175059 meter/sec
ZDOT = -17410
255806 ZDOT = -5306
645970
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
67826143
00016717 00000-0 10270-3 0 9054
2 25544 51
6448 316
4409 0006279 37
9311 322
2293 15
72355806 25096
Satellite: ISS
Catalog Number: 25544
Epoch time: 11067
67826143 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 316
4409 deg
Eccentricity:
0006279
Arg of perigee: 37
9311 deg
Mean anomaly: 322
2293 deg
Mean motion: 15
72355806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2509
Checksum: 314
Coasting Arc #7 (Orbit 2524)
---------------------------------------
Vector Time (GMT): 2011/068/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5112177
68 A = 6728668
00 meter
Y = -631402
66 meter E =
0013273
Z = 4316994
54 I = 51
37832
XDOT = -2085
121045 Wp = 83
89612
YDOT = 6580
686002 meter/sec RA = 310
92645 deg
ZDOT = 3424
074284 TA = 331
40425
MA = 331
47698
Ha = 194
450 n
mi
Hp = 184
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16772236
49 X = 5097887
15
Y = -2071531
04 feet Y = -574314
73 meter
Z = 14163367
92 Z = 4341794
68
XDOT = -6840
948311 XDOT = -2175
185981
YDOT = 21590
177171 feet/sec YDOT = 6556
865623 meter/sec
ZDOT = 11233
839514 ZDOT = 3413
725514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12061578
01 X = 3676368
98
Y = -11716312
22 feet Y = -3571131
97 meter
Z = 14263467
75 Z = 4347504
97
XDOT = 6657
169256 XDOT = 2029
105189
YDOT = 20508
578741 feet/sec YDOT = 6251
014800 meter/sec
ZDOT = 11191
894237 ZDOT = 3411
289363
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
69517382
00016717 00000-0 10270-3 0 9060
2 25544 51
6434 311
2310 0006185 43
1415 317
0231 15
72344612 25250
Satellite: ISS
Catalog Number: 25544
Epoch time: 11068
69517382 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 311
2310 deg
Eccentricity:
0006185
Arg of perigee: 43
1415 deg
Mean anomaly: 317
0231 deg
Mean motion: 15
72344612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2525
Checksum: 274
Coasting Arc #8 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2011/069/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 785912
19 A = 6731700
50 meter
Y = -5754724
16 meter E =
0010293
Z = -3407167
03 I = 51
36922
XDOT = 5879
172101 Wp = 66
83229
YDOT = -1901
237086 meter/sec RA = 305
73362 deg
ZDOT = 4582
268549 TA = 252
79829
MA = 252
91098
Ha = 194
531 n
mi
Hp = 184
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2578452
05 X = 866755
49
Y = -18880328
62 feet Y = -5745483
83 meter
Z = -11178369
52 Z = -3403152
33
XDOT = 19288
622380 XDOT = 5877
735449
YDOT = -6237
654481 feet/sec YDOT = -1835
500340 meter/sec
ZDOT = 15033
689465 ZDOT = 4610
826022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9562492
16 X = -2914647
61
Y = -16493617
86 feet Y = -5027254
72 meter
Z = -11162010
68 Z = -3402180
86
XDOT = 10062
752334 XDOT = 3067
126911
YDOT = -16052
860852 feet/sec YDOT = -4892
911988 meter/sec
ZDOT = 15148
986027 ZDOT = 4617
410941
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
64849865
00016717 00000-0 10270-3 0 9071
2 25544 51
6428 306
3463 0006117 48
3311 311
8374 15
72402571 25400
Satellite: ISS
Catalog Number: 25544
Epoch time: 11069
64849865 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 306
3463 deg
Eccentricity:
0006117
Arg of perigee: 48
3311 deg
Mean anomaly: 311
8374 deg
Mean motion: 15
72402571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2540
Checksum: 305
Coasting Arc #9 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2011/070/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4987009
89 A = 6730571
47 meter
Y = 2639244
27 meter E =
0011780
Z = -3683093
26 I = 51
34922
XDOT = -210
354122 Wp = 64
21266
YDOT = -6375
571568 meter/sec RA = 300
64194 deg
ZDOT = -4289
420418 TA = 160
20774
MA = 160
16199
Ha = 194
512 n
mi
Hp = 184
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16361580
99 X = -4998260
11
Y = 8658937
89 feet Y = 2583413
39 meter
Z = -12083639
29 Z = -3707347
43
XDOT = -690
138197 XDOT = -118
208570
YDOT = -20917
229554 feet/sec YDOT = -6377
408901 meter/sec
ZDOT = -14072
901634 ZDOT = -4290
218135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7190809
92 X = -2191758
86
Y = 16988054
54 feet Y = 5177959
02 meter
Z = -12181589
88 Z = -3712948
60
XDOT = -12414
086352 XDOT = -3783
813520
YDOT = -15335
019792 feet/sec YDOT = -4674
114033 meter/sec
ZDOT = -14075
949575 ZDOT = -4290
349430
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
66534826
00016717 00000-0 10270-3 0 9084
2 25544 51
6428 301
1369 0006237 51
9479 308
2245 15
72466637 25563
Satellite: ISS
Catalog Number: 25544
Epoch time: 11070
66534826 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 301
1369 deg
Eccentricity:
0006237
Arg of perigee: 51
9479 deg
Mean anomaly: 308
2245 deg
Mean motion: 15
72466637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2556
Checksum: 321
Coasting Arc #10 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2011/071/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1109490
85 A = 6729288
85 meter
Y = 5239805
88 meter E =
0016394
Z = 4064877
80 I = 51
33001
XDOT = -5310
807228 Wp = 68
88917
YDOT = 4085
724640 meter/sec RA = 295
44454 deg
ZDOT = -3798
975635 TA = 60
36829
MA = 60
20510
Ha = 194
433 n
mi
Hp = 184
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3640061
85 X = 1031069
66
Y = 17190964
18 feet Y = 5251774
60 meter
Z = 13336213
24 Z = 4070076
92
XDOT = -17423
908228 XDOT = -5337
645324
YDOT = 13404
608400 feet/sec YDOT = 4026
185739 meter/sec
ZDOT = -12463
830822 ZDOT = -3824
840639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13787362
96 X = 4202388
23
Y = 10868831
40 feet Y = 3312819
81 meter
Z = 13357058
44 Z = 4071231
41
XDOT = -3862
746802 XDOT = -1177
365225
YDOT = 20418
627544 feet/sec YDOT = 6223
597675 meter/sec
ZDOT = -12568
320723 ZDOT = -3830
824156
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
68216628
00016717 00000-0 10270-3 0 9095
2 25544 51
6424 295
9263 0006025 55
8201 304
3531 15
72485253 25721
Satellite: ISS
Catalog Number: 25544
Epoch time: 11071
68216628 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 295
9263 deg
Eccentricity:
0006025
Arg of perigee: 55
8201 deg
Mean anomaly: 304
3531 deg
Mean motion: 15
72485253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 300
Coasting Arc #11 (Orbit 2587)
---------------------------------------
Vector Time (GMT): 2011/072/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4137969
04 A = 6732500
22 meter
Y = -4414986
94 meter E =
0019023
Z = 2929644
50 I = 51
32948
XDOT = 2244
272876 Wp = 75
61167
YDOT = 5427
859702 meter/sec RA = 290
34751 deg
ZDOT = 4987
552018 TA = 318
31564
MA = 318
46045
Ha = 194
316 n
mi
Hp = 184
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13576013
90 X = 4172799
23
Y = -14484865
30 feet Y = -4368518
79 meter
Z = 9611694
54 Z = 2949831
26
XDOT = 7363
099987 XDOT = 2159
182437
YDOT = 17807
938656 feet/sec YDOT = 5452
480974 meter/sec
ZDOT = 16363
359638 ZDOT = 4998
247618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 687262
62 X = 209477
65
Y = -19800813
59 feet Y = -6035287
98 meter
Z = 9693275
98 Z = 2954510
52
XDOT = 15728
095858 XDOT = 4793
923617
YDOT = 8613
051314 feet/sec YDOT = 2625
258041 meter/sec
ZDOT = 16406
389433 ZDOT = 5000
667499
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
69895234
00016717 00000-0 10270-3 0 9105
2 25544 51
6424 290
7159 0006027 60
4754 299
7009 15
72556172 25888
Satellite: ISS
Catalog Number: 25544
Epoch time: 11072
69895234 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 290
7159 deg
Eccentricity:
0006027
Arg of perigee: 60
4754 deg
Mean anomaly: 299
7009 deg
Mean motion: 15
72556172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2588
Checksum: 327
Coasting Arc #12 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2011/073/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2697507
09 A = 6726974
01 meter
Y = -4121414
44 meter E =
0015424
Z = -4595149
95 I = 51
30241
XDOT = 4012
260946 Wp = 93
36439
YDOT = -5871
492398 meter/sec RA = 285
15382 deg
ZDOT = 2918
390233 TA = 205
70479
MA = 205
78153
Ha = 194
370 n
mi
Hp = 183
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8850088
88 X = -2628898
16
Y = -13521700
91 feet Y = -4151196
21 meter
Z = -15075951
26 Z = -4608087
35
XDOT = 13163
585782 XDOT = 4063
442130
YDOT = -19263
426504 feet/sec YDOT = -5826
338553 meter/sec
ZDOT = 9574
771107 ZDOT = 2938
006052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15559548
21 X = -4742550
29
Y = -4181715
26 feet Y = -1274586
81 meter
Z = -15128069
68 Z = -4611035
64
XDOT = -3463
421711 XDOT = -1055
650938
YDOT = -21949
108673 feet/sec YDOT = -6690
088324 meter/sec
ZDOT = 9654
079991 ZDOT = 2942
563581
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
65216079
00016717 00000-0 10270-3 0 9117
2 25544 51
6432 285
8316 0006098 64
3403 295
8389 15
72593710 26034
Satellite: ISS
Catalog Number: 25544
Epoch time: 11073
65216079 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 285
8316 deg
Eccentricity:
0006098
Arg of perigee: 64
3403 deg
Mean anomaly: 295
8389 deg
Mean motion: 15
72593710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2603
Checksum: 315
Coasting Arc #13 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2011/074/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2793088
97 A = 6733854
22 meter
Y = 5725151
36 meter E =
0009982
Z = -2187699
00 I = 51
31916
XDOT = -3749
210801 Wp = 101
80941
YDOT = -3907
692827 meter/sec RA = 280
04694 deg
ZDOT = -5462
679896 TA = 102
77801
MA = 102
66644
Ha = 194
287 n
mi
Hp = 183
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9163677
71 X = -2846273
88
Y = 18783304
99 feet Y = 5693619
84 meter
Z = -7177490
16 Z = -2201397
10
XDOT = -12300
560371 XDOT = -3678
699424
YDOT = -12820
514523 feet/sec YDOT = -3949
224872 meter/sec
ZDOT = -17922
178137 ZDOT = -5480
721664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6142137
74 X = 1872123
58
Y = 19956481
31 feet Y = 6082735
50 meter
Z = -7232903
86 Z = -2204589
10
XDOT = -16206
451655 XDOT = -4939
726464
YDOT = -1506
789830 feet/sec YDOT = -459
269540 meter/sec
ZDOT = -17994
912921 ZDOT = -5484
849458
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
66888380
00016717 00000-0 10270-3 0 9120
2 25544 51
6429 280
6209 0006133 66
5292 293
6514 15
72668233 26190
Satellite: ISS
Catalog Number: 25544
Epoch time: 11074
66888380 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 280
6209 deg
Eccentricity:
0006133
Arg of perigee: 66
5292 deg
Mean anomaly: 293
6514 deg
Mean motion: 15
72668233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2619
Checksum: 324
Coasting Arc #14 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2011/075/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3739753
09 A = 6725338
98 meter
Y = 2626471
90 meter E =
0012097
Z = 4926476
45 I = 51
28574
XDOT = -2253
341482 Wp = 63
90996
YDOT = 7076
423736 meter/sec RA = 274
86099 deg
ZDOT = -2052
986484 TA = 46
10687
MA = 46
00703
Ha = 194
235 n
mi
Hp = 183
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12269531
14 X = 3686174
02
Y = 8617033
78 feet Y = 2667992
93 meter
Z = 16162980
49 Z = 4944513
41
XDOT = -7392
852630 XDOT = -2322
331102
YDOT = 23216
613306 feet/sec YDOT = 7050
839585 meter/sec
ZDOT = -6735
519962 ZDOT = -2064
101166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14742888
64 X = 4493632
46
Y = -2254962
92 feet Y = -687312
70 meter
Z = 16235731
60 Z = 4948650
99
XDOT = 10671
378493 XDOT = 3252
636165
YDOT = 20734
156414 feet/sec YDOT = 6319
770875 meter/sec
ZDOT = -6780
523714 ZDOT = -2066
703628
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
68557636
00016717 00000-0 10270-3 0 9131
2 25544 51
6424 275
4101 0006117 71
7035 288
4792 15
72657288 26359
Satellite: ISS
Catalog Number: 25544
Epoch time: 11075
68557636 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 275
4101 deg
Eccentricity:
0006117
Arg of perigee: 71
7035 deg
Mean anomaly: 288
4792 deg
Mean motion: 15
72657288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2635
Checksum: 324
Coasting Arc #15 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2011/076/15:23:37
942
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1088857
52 A = 6734833
16 meter
Y = -6488825
17 meter E =
0019864
Z = 1396561
83 I = 51
31834
XDOT = 4648
283736 Wp = 64
93792
YDOT = 2039
127195 meter/sec RA = 269
74149 deg
ZDOT = 5794
262925 TA = 310
48728
MA = 310
66024
Ha = 194
120 n
mi
Hp = 183
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3572367
18 X = 1154551
76
Y = -21288796
48 feet Y = -6476281
43 meter
Z = 4581895
77 Z = 1402011
69
XDOT = 15250
274726 XDOT = 4596
989441
YDOT = 6690
049851 feet/sec YDOT = 2090
820973 meter/sec
ZDOT = 19010
048965 ZDOT = 5816
719006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12540105
28 X = -3822224
09
Y = -17564659
94 feet Y = -5353708
35 meter
Z = 4604010
48 Z = 1403302
39
XDOT = 14155
500698 XDOT = 4314
596613
YDOT = -5051
642862 feet/sec YDOT = -1539
740744 meter/sec
ZDOT = 19100
654682 ZDOT = 5821
879547
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
70223173
00016717 00000-0 10270-3 0 9142
2 25544 51
6434 270
1995 0005987 75
3312 284
8514 15
72769720 26510
Satellite: ISS
Catalog Number: 25544
Epoch time: 11076
70223173 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 270
1995 deg
Eccentricity:
0005987
Arg of perigee: 75
3312 deg
Mean anomaly: 284
8514 deg
Mean motion: 15
72769720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 316
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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