[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 19th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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 536)
---------------------------------------
Vector Time (GMT): 2011/196/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3495730
47 A = 6762193
60 meter
Y = -3031859
01 meter E =
0008193
Z = -4933807
61 I = 51
72513
XDOT = 6345
359613 Wp = 43
27080
YDOT = 3696
276600 meter/sec RA = 16
34223 deg
ZDOT = 2232
484459 TA = 248
43248
MA = 248
51981
Ha = 213
362 n
mi
Hp = 206
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11468931
99 X = 3553340
45
Y = -9947043
99 feet Y = -2992444
81 meter
Z = -16187032
83 Z = -4916686
26
XDOT = 20818
108966 XDOT = 6292
710793
YDOT = 12126
891732 feet/sec YDOT = 3766
939583 meter/sec
ZDOT = 7324
424078 ZDOT = 2263
182102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6470422
94 X = -1972184
91
Y = 13815464
33 feet Y = 4210953
53 meter
Z = -16117279
21 Z = -4912546
70
XDOT = -22912
153584 XDOT = -6983
624412
YDOT = -2071
703882 feet/sec YDOT = -631
455343 meter/sec
ZDOT = 7448
882294 ZDOT = 2270
419323
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 11196
76692958
00016717 00000-0 10270-3 0 9007
2 25544 51
6406 16
8268 0011210 327
1108 32
9350 15
59934097 5371
Satellite: ISS
Catalog Number: 25544
Epoch time: 11196
76692958 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 16
8268 deg
Eccentricity:
0011210
Arg of perigee: 327
1108 deg
Mean anomaly: 32
9350 deg
Mean motion: 15
59934097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 537
Checksum: 312
Coasting Arc #2 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2011/197/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6220415
52 A = 6769844
76 meter
Y = 807611
78 meter E =
0010152
Z = 2550086
60 I = 51
72108
XDOT = -2797
859908 Wp = 50
15350
YDOT = -4810
113224 meter/sec RA = 11
31535 deg
ZDOT = -5281
153533 TA = 101
17713
MA = 101
06298
Ha = 213
535 n
mi
Hp = 206
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20408187
40 X = -6241371
62
Y = 2649644
95 feet Y = 737933
83 meter
Z = 8366425
84 Z = 2519817
77
XDOT = -9179
330406 XDOT = -2718
210109
YDOT = -15781
211365 feet/sec YDOT = -4840
954625 meter/sec
ZDOT = -17326
619202 ZDOT = -5294
552299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17384423
66 X = 5298772
33
Y = -11105844
89 feet Y = -3385061
52 meter
Z = 8243411
66 Z = 2512591
87
XDOT = 14119
516231 XDOT = 4303
628547
YDOT = 9150
687021 feet/sec YDOT = 2789
129404 meter/sec
ZDOT = -17380
731877 ZDOT = -5297
647076
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 11197
79194436
00016717 00000-0 10270-3 0 9010
2 25544 51
6404 11
6719 0011276 331
1704 28
8827 15
59922906 5539
Satellite: ISS
Catalog Number: 25544
Epoch time: 11197
79194436 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 11
6719 deg
Eccentricity:
0011276
Arg of perigee: 331
1704 deg
Mean anomaly: 28
8827 deg
Mean motion: 15
59922906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 553
Checksum: 313
Coasting Arc #3 (Orbit 568)
---------------------------------------
Vector Time (GMT): 2011/198/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6515958
19 A = 6772117
16 meter
Y = 1503978
28 meter E =
0019083
Z = 984400
50 I = 51
69934
XDOT = -1935
283169 Wp = 19
39711
YDOT = 4495
224210 meter/sec RA = 6
32088 deg
ZDOT = 5926
990078 TA = 351
29770
MA = 351
33074
Ha = 213
710 n
mi
Hp = 205
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21377815
59 X = 6493874
21
Y = 4934311
94 feet Y = 1576720
12 meter
Z = 3229660
43 Z = 1016000
76
XDOT = -6349
354229 XDOT = -2014
197348
YDOT = 14748
110926 feet/sec YDOT = 4473
140891 meter/sec
ZDOT = 19445
505505 ZDOT = 5917
397455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21344264
13 X = -6505731
71
Y = 4993580
09 feet Y = 1522043
21 meter
Z = 3357928
97 Z = 1023496
75
XDOT = -339
333790 XDOT = -103
428939
YDOT = -14532
416339 feet/sec YDOT = -4429
480500 meter/sec
ZDOT = 19406
244392 ZDOT = 5915
023291
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 11198
81694999
00016717 00000-0 10270-3 0 9024
2 25544 51
6408 6
5167 0011419 335
2066 24
8539 15
59916907 5695
Satellite: ISS
Catalog Number: 25544
Epoch time: 11198
81694999 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 6
5167 deg
Eccentricity:
0011419
Arg of perigee: 335
2066 deg
Mean anomaly: 24
8539 deg
Mean motion: 15
59916907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 569
Checksum: 343
Coasting Arc #4 (Orbit 583)
---------------------------------------
Vector Time (GMT): 2011/199/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4262225
72 A = 6765326
46 meter
Y = -3325884
73 meter E =
0013362
Z = -4078933
63 I = 51
64592
XDOT = 5961
193214 Wp = 11
99445
YDOT = -2908
560587 meter/sec RA = 1
30959 deg
ZDOT = -3846
954793 TA = 218
18322
MA = 218
27795
Ha = 213
846 n
mi
Hp = 205
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13983680
20 X = -4204903
97
Y = -10911695
30 feet Y = -3373226
71 meter
Z = -13382328
20 Z = -4099500
10
XDOT = 19557
720517 XDOT = 6011
961653
YDOT = -9542
521611 feet/sec YDOT = -2841
614732 meter/sec
ZDOT = -12621
242759 ZDOT = -3817
872862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17351322
50 X = 5288683
10
Y = 3361972
78 feet Y = 1024729
30 meter
Z = -13465654
86 Z = -4104331
60
XDOT = -12866
272389 XDOT = -3921
639824
YDOT = 16188
295550 feet/sec YDOT = 4934
192484 meter/sec
ZDOT = -12502
921418 ZDOT = -3810
890448
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 11199
77788407
00016717 00000-0 10270-3 0 9039
2 25544 51
6400 1
6844 0011404 338
5253 21
5423 15
59934924 5845
Satellite: ISS
Catalog Number: 25544
Epoch time: 11199
77788407 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 1
6844 deg
Eccentricity:
0011404
Arg of perigee: 338
5253 deg
Mean anomaly: 21
5423 deg
Mean motion: 15
59934924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 584
Checksum: 308
Coasting Arc #5 (Orbit 599)
---------------------------------------
Vector Time (GMT): 2011/200/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 278576
19 A = 6760349
19 meter
Y = 4190439
93 meter E =
0011099
Z = 5298709
35 I = 51
60012
XDOT = -7660
735824 Wp = 353
45440
YDOT = 509
775570 meter/sec RA = 356
25451 deg
ZDOT = 10
411219 TA = 96
50965
MA = 96
38328
Ha = 213
975 n
mi
Hp = 205
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 913963
87 X = 205957
48
Y = 13748162
49 feet Y = 4193148
75 meter
Z = 17384217
03 Z = 5299886
54
XDOT = -25133
647718 XDOT = -7665
917445
YDOT = 1672
492028 feet/sec YDOT = 424
079583 meter/sec
ZDOT = 34
157542 ZDOT = -26
816494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7199797
77 X = -2194498
36
Y = -11741095
93 feet Y = -3578686
04 meter
Z = 17388728
60 Z = 5300084
48
XDOT = 20515
720238 XDOT = 6253
191528
YDOT = -12806
413756 feet/sec YDOT = -3903
394913 meter/sec
ZDOT = -117
090067 ZDOT = -35
689053
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 11200
80287054
00016717 00000-0 10270-3 0 9049
2 25544 51
6408 356
5291 0011526 342
0887 17
9861 15
59984756 6001
Satellite: ISS
Catalog Number: 25544
Epoch time: 11200
80287054 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 356
5291 deg
Eccentricity:
0011526
Arg of perigee: 342
0887 deg
Mean anomaly: 17
9861 deg
Mean motion: 15
59984756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 600
Checksum: 314
Coasting Arc #6 (Orbit 614)
---------------------------------------
Vector Time (GMT): 2011/201/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3740076
66 A = 6765216
67 meter
Y = -3867942
11 meter E =
0009897
Z = -4098486
09 I = 51
58561
XDOT = 6326
394636 Wp = 25
72112
YDOT = 2084
355139 meter/sec RA = 351
19819 deg
ZDOT = 3818
232781 TA = 283
62199
MA = 283
73220
Ha = 214
197 n
mi
Hp = 204
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12270592
71 X = 3802960
17
Y = -12690098
78 feet Y = -3825766
43 meter
Z = -13446476
66 Z = -4080164
57
XDOT = 20755
887913 XDOT = 6284
068779
YDOT = 6838
435496 feet/sec YDOT = 2154
863838 meter/sec
ZDOT = 12527
010436 ZDOT = 3848
863265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4610146
21 X = -1405172
56
Y = 17098391
30 feet Y = 5211589
67 meter
Z = -13371811
92 Z = -4075728
27
XDOT = -20146
587634 XDOT = -6140
679911
YDOT = 4430
498992 feet/sec YDOT = 1350
416093 meter/sec
ZDOT = 12651
288346 ZDOT = 3856
112688
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 11201
76378957
00016717 00000-0 10270-3 0 9059
2 25544 51
6400 351
6968 0011559 346
9710 13
1145 15
59997647 6156
Satellite: ISS
Catalog Number: 25544
Epoch time: 11201
76378957 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 351
6968 deg
Eccentricity:
0011559
Arg of perigee: 346
9710 deg
Mean anomaly: 13
1145 deg
Mean motion: 15
59997647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 615
Checksum: 329
Coasting Arc #7 (Orbit 630)
---------------------------------------
Vector Time (GMT): 2011/202/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6275060
38 A = 6771878
25 meter
Y = 2350693
26 meter E =
0010024
Z = 988052
14 I = 51
57905
XDOT = -2512
472514 Wp = 66
61647
YDOT = -4203
986331 meter/sec RA = 346
18004 deg
ZDOT = -5903
339235 TA = 102
65303
MA = 102
54093
Ha = 214
339 n
mi
Hp = 204
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20587468
45 X = -6305679
63
Y = 7712248
24 feet Y = 2280350
45 meter
Z = 3241640
88 Z = 957494
05
XDOT = -8243
020059 XDOT = -2436
598983
YDOT = -13792
606073 feet/sec YDOT = -4231
657696 meter/sec
ZDOT = -19367
910876 ZDOT = -5915
360671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13954227
05 X = 4253248
40
Y = -17011536
31 feet Y = -5185116
27 meter
Z = 3117377
95 Z = 950176
80
XDOT = 12710
315740 XDOT = 3874
104237
YDOT = 6835
776770 feet/sec YDOT = 2083
544759 meter/sec
ZDOT = -19416
466706 ZDOT = -5918
139052
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 11202
78875933
00016717 00000-0 10270-3 0 9069
2 25544 51
6406 346
5415 0011794 350
8395 9
2544 15
60016012 6313
Satellite: ISS
Catalog Number: 25544
Epoch time: 11202
78875933 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 346
5415 deg
Eccentricity:
0011794
Arg of perigee: 350
8395 deg
Mean anomaly: 9
2544 deg
Mean motion: 15
60016012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 631
Checksum: 296
Coasting Arc #8 (Orbit 646)
---------------------------------------
Vector Time (GMT): 2011/203/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6254430
98 A = 6769497
33 meter
Y = 12786
72 meter E =
0019318
Z = 2556169
60 I = 51
54110
XDOT = -2167
232890 Wp = 39
24061
YDOT = 5161
114887 meter/sec RA = 341
17498 deg
ZDOT = 5269
924025 TA = 349
64966
MA = 349
68938
Ha = 214
461 n
mi
Hp = 204
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20519786
68 X = 6241405
86
Y = 41951
17 feet Y = 82654
55 meter
Z = 8386383
20 Z = 2586521
70
XDOT = -7110
344127 XDOT = -2250
384494
YDOT = 16932
791624 feet/sec YDOT = 5136
414234 meter/sec
ZDOT = 17289
776986 ZDOT = 5259
194135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17547878
35 X = -5348593
32
Y = 10538149
24 feet Y = 3212027
89 meter
Z = 8509653
61 Z = 2593742
42
XDOT = -1802
620289 XDOT = -549
438664
YDOT = -16946
260802 feet/sec YDOT = -5165
220292 meter/sec
ZDOT = 17245
868205 ZDOT = 5256
540629
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 11203
81372161
00016717 00000-0 10270-3 0 9070
2 25544 51
6399 341
3862 0011810 355
4924 4
6123 15
59980435 6477
Satellite: ISS
Catalog Number: 25544
Epoch time: 11203
81372161 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 341
3862 deg
Eccentricity:
0011810
Arg of perigee: 355
4924 deg
Mean anomaly: 4
6123 deg
Mean motion: 15
59980435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 647
Checksum: 301
Coasting Arc #9 (Orbit 661)
---------------------------------------
Vector Time (GMT): 2011/204/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3848254
23 A = 6761842
04 meter
Y = -2591196
07 meter E =
0019173
Z = -4934460
54 I = 51
48818
XDOT = 5826
522647 Wp = 37
24745
YDOT = -4477
134762 meter/sec RA = 336
13223 deg
ZDOT = -2182
391138 TA = 211
35788
MA = 211
47235
Ha = 214
595 n
mi
Hp = 203
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12625506
02 X = -3795022
45
Y = -8501299
43 feet Y = -2633931
51 meter
Z = -16189175
02 Z = -4953026
14
XDOT = 19115
887949 XDOT = 5886
755367
YDOT = -14688
762341 feet/sec YDOT = -4411
642060 meter/sec
ZDOT = -7160
075912 ZDOT = -2153
940224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15130569
38 X = 4611797
55
Y = 547493
88 feet Y = 166876
14 meter
Z = -16264409
07 Z = -4957391
88
XDOT = -8387
705033 XDOT = -2556
572494
YDOT = 21519
599436 feet/sec YDOT = 6559
173908 meter/sec
ZDOT = -7044
242068 ZDOT = -2147
084982
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 11204
77461348
00016717 00000-0 10270-3 0 9083
2 25544 51
6407 336
5533 0011775 358
5029 1
6089 15
60004112 6624
Satellite: ISS
Catalog Number: 25544
Epoch time: 11204
77461348 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 336
5533 deg
Eccentricity:
0011775
Arg of perigee: 358
5029 deg
Mean anomaly: 1
6089 deg
Mean motion: 15
60004112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 662
Checksum: 291
Coasting Arc #10 (Orbit 677)
---------------------------------------
Vector Time (GMT): 2011/205/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 30997
60 A = 6761443
70 meter
Y = 4542032
42 meter E =
0016065
Z = 5008518
27 I = 51
45901
XDOT = -7106
706158 Wp = 18
96519
YDOT = 2182
949158 meter/sec RA = 331
05880 deg
ZDOT = -1918
998043 TA = 89
76192
MA = 89
57783
Ha = 214
729 n
mi
Hp = 203
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 101698
17 X = -44124
86
Y = 14901681
17 feet Y = 4541958
50 meter
Z = 16432146
56 Z = 5008486
86
XDOT = -23315
965085 XDOT = -7121
266064
YDOT = 7161
906687 feet/sec YDOT = 2103
396433 meter/sec
ZDOT = -6295
925339 ZDOT = -1953
557273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8135478
26 X = -2479693
78
Y = -12485919
32 feet Y = -3805708
21 meter
Z = 16431728
36 Z = 5008390
80
XDOT = 14686
469045 XDOT = 4476
435765
YDOT = -18111
651298 feet/sec YDOT = -5520
431316 meter/sec
ZDOT = -6436
418240 ZDOT = -1961
820280
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 11205
79955531
00016717 00000-0 10270-3 0 9099
2 25544 51
6398 331
3978 0011911 2
5006 357
6208 15
60051860 6788
Satellite: ISS
Catalog Number: 25544
Epoch time: 11205
79955531 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 331
3978 deg
Eccentricity:
0011911
Arg of perigee: 2
5006 deg
Mean anomaly: 357
6208 deg
Mean motion: 15
60051860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 678
Checksum: 311
Coasting Arc #11 (Orbit 692)
---------------------------------------
Vector Time (GMT): 2011/206/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3532644
49 A = 6768843
47 meter
Y = -5052344
45 meter E =
0015339
Z = -2779428
52 I = 51
45908
XDOT = 5618
070999 Wp = 20
49366
YDOT = 1126
570448 meter/sec RA = 326
00942 deg
ZDOT = 5115
338983 TA = 307
80605
MA = 307
94484
Ha = 214
845 n
mi
Hp = 203
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11590040
99 X = 3602380
06
Y = -16575933
22 feet Y = -5012450
02 meter
Z = -9118859
98 Z = -2762098
32
XDOT = 18431
991467 XDOT = 5580
206781
YDOT = 3696
097269 feet/sec YDOT = 1189
182823 meter/sec
ZDOT = 16782
608212 ZDOT = 5142
539463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -362643
26 X = -110533
67
Y = 20254470
97 feet Y = 6173562
75 meter
Z = -9048155
35 Z = -2757877
75
XDOT = -15779
394284 XDOT = -4809
559378
YDOT = 7230
564540 feet/sec YDOT = 2203
876072 meter/sec
ZDOT = 16893
004603 ZDOT = 5148
987803
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 11206
76043170
00016717 00000-0 10270-3 0 9106
2 25544 51
6408 326
5648 0011922 6
6931 353
4382 15
60074210 6932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11206
76043170 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 326
5648 deg
Eccentricity:
0011922
Arg of perigee: 6
6931 deg
Mean anomaly: 353
4382 deg
Mean motion: 15
60074210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 693
Checksum: 282
Coasting Arc #12 (Orbit 708)
---------------------------------------
Vector Time (GMT): 2011/207/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5600465
86 A = 6771850
03 meter
Y = 3731674
25 meter E =
0009488
Z = -784128
52 I = 51
44405
XDOT = -2098
096139 Wp = 65
38119
YDOT = -4384
038713 meter/sec RA = 320
99535 deg
ZDOT = -5931
160564 TA = 123
12959
MA = 123
03850
Ha = 214
983 n
mi
Hp = 203
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18374231
83 X = -5637968
82
Y = 12243025
76 feet Y = 3668836
84 meter
Z = -2572600
14 Z = -811425
85
XDOT = -6883
517516 XDOT = -2020
104907
YDOT = -14383
329110 feet/sec YDOT = -4407
064068 meter/sec
ZDOT = -19459
188203 ZDOT = -5941
164107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7999088
21 X = 2438122
08
Y = -20565375
95 feet Y = -6268326
59 meter
Z = -2683700
11 Z = -817991
79
XDOT = 12300
021533 XDOT = 3749
046563
YDOT = 7307
198441 feet/sec YDOT = 2227
234085 meter/sec
ZDOT = -19499
538648 ZDOT = -5943
459380
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 11207
78535664
00016717 00000-0 10270-3 0 9114
2 25544 51
6401 321
4088 0012022 10
3074 349
8326 15
60058627 7098
Satellite: ISS
Catalog Number: 25544
Epoch time: 11207
78535664 = yrday
fracday
Element set: 911
Inclination: 51
6401 deg
RA of node: 321
4088 deg
Eccentricity:
0012022
Arg of perigee: 10
3074 deg
Mean anomaly: 349
8326 deg
Mean motion: 15
60058627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 709
Checksum: 286
Coasting Arc #13 (Orbit 724)
---------------------------------------
Vector Time (GMT): 2011/208/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5413498
31 A = 6765349
90 meter
Y = -849379
21 meter E =
0016774
Z = 3948410
26 I = 51
39876
XDOT = -1923
220208 Wp = 54
32614
YDOT = 6286
531724 meter/sec RA = 315
96710 deg
ZDOT = 3986
934182 TA = 354
09467
MA = 354
11443
Ha = 215
013 n
mi
Hp = 203
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17760821
22 X = 5403413
56
Y = -2786677
19 feet Y = -788899
07 meter
Z = 12954101
90 Z = 3974683
98
XDOT = -6309
777586 XDOT = -2012
741957
YDOT = 20625
104083 feet/sec YDOT = 6264
524042 meter/sec
ZDOT = 13080
492722 ZDOT = 3977
374712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12660610
13 X = -3858953
97
Y = 12654795
62 feet Y = 3857181
71 meter
Z = 13060865
03 Z = 3980951
66
XDOT = -6044
194778 XDOT = -1842
270568
YDOT = -19514
327533 feet/sec YDOT = -5947
967032 meter/sec
ZDOT = 13041
274793 ZDOT = 3974
980557
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 11208
81027306
00016717 00000-0 10270-3 0 9129
2 25544 51
6394 316
2531 0012170 14
3010 345
8488 15
60059585 7259
Satellite: ISS
Catalog Number: 25544
Epoch time: 11208
81027306 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 316
2531 deg
Eccentricity:
0012170
Arg of perigee: 14
3010 deg
Mean anomaly: 345
8488 deg
Mean motion: 15
60059585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 725
Checksum: 282
Coasting Arc #14 (Orbit 739)
---------------------------------------
Vector Time (GMT): 2011/209/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3323498
19 A = 6760131
52 meter
Y = -2619603
37 meter E =
0021962
Z = -5287982
05 I = 51
36090
XDOT = 4915
477974 Wp = 56
92681
YDOT = -5878
220514 meter/sec RA = 310
89602 deg
ZDOT = -166
119930 TA = 211
41740
MA = 211
54877
Ha = 215
166 n
mi
Hp = 202
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10903865
45 X = -3268270
77
Y = -8594499
24 feet Y = -2656459
31 meter
Z = -17349022
49 Z = -5303993
43
XDOT = 16126
896239 XDOT = 4981
651010
YDOT = -19285
500375 feet/sec YDOT = -5822
882632 meter/sec
ZDOT = -545
012895 ZDOT = -142
081037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13797619
49 X = 4205514
42
Y = 360901
37 feet Y = 110002
74 meter
Z = -17413894
65 Z = -5307755
09
XDOT = -1241
095268 XDOT = -378
285838
YDOT = 24103
584671 feet/sec YDOT = 7346
772608 meter/sec
ZDOT = -447
016372 ZDOT = -136
250590
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 11209
77112294
00016717 00000-0 10270-3 0 9137
2 25544 51
6400 311
4205 0012136 17
0648 343
0913 15
60066547 7407
Satellite: ISS
Catalog Number: 25544
Epoch time: 11209
77112294 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 311
4205 deg
Eccentricity:
0012136
Arg of perigee: 17
0648 deg
Mean anomaly: 343
0913 deg
Mean motion: 15
60066547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 740
Checksum: 268
Coasting Arc #15 (Orbit 755)
---------------------------------------
Vector Time (GMT): 2011/210/18:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 189831
05 A = 6764727
49 meter
Y = 5361932
16 meter E =
0020149
Z = 4117335
12 I = 51
35666
XDOT = -5937
608762 Wp = 45
75713
YDOT = 3107
149435 meter/sec RA = 305
81974 deg
ZDOT = -3747
412039 TA = 83
03136
MA = 82
80221
Ha = 215
262 n
mi
Hp = 202
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 622805
28 X = 109858
01
Y = 17591640
96 feet Y = 5363607
39 meter
Z = 13508317
31 Z = 4118063
59
XDOT = -19480
343707 XDOT = -5953
708428
YDOT = 10194
059827 feet/sec YDOT = 3040
661844 meter/sec
ZDOT = -12294
658920 ZDOT = -3776
294998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11258621
16 X = -3431627
73
Y = -13528704
22 feet Y = -4123549
05 meter
Z = 13510957
26 Z = 4118139
77
XDOT = 8028
416742 XDOT = 2447
061423
YDOT = -19159
757363 feet/sec YDOT = -5839
894044 meter/sec
ZDOT = -12412
159910 ZDOT = -3783
226341
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 11210
79602071
00016717 00000-0 10270-3 0 9149
2 25544 51
6389 306
2642 0012281 20
7528 339
4124 15
60119604 7562
Satellite: ISS
Catalog Number: 25544
Epoch time: 11210
79602071 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 306
2642 deg
Eccentricity:
0012281
Arg of perigee: 20
7528 deg
Mean anomaly: 339
4124 deg
Mean motion: 15
60119604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 756
Checksum: 285
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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