[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 4th 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
163/14:26:51
553 -9
1 9
5 9
5
N/A 1
4 -0
0 192
1
000/00:33:43
105 -2
3 -0
3 190
3
163/18:35:11
639 3
7 8
5 8
5
N/A 5
2 -0
5 201
6
000/00:40:23
279 -5
6 0
4 193
2
166/15:04:46
905 8
7 9
8 9
8
N/A -4
0 0
3 205
2
000/00:29:33
809 2
1 0
5 196
2
166/19:08:06
618 -8
6 9
4 9
4
N/A -1
2 0
2 206
5
000/00:36:13
236 3
6 -0
3 205
3
Coasting Arc #1 (Orbit 3875)
---------------------------------------
Vector Time (GMT): 2011/154/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5357756
39 A = 6725638
69 meter
Y = -1804977
23 meter E =
0004419
Z = -3647630
89 I = 51
38089
XDOT = -820
937744 Wp = 105
67850
YDOT = -6308
199595 meter/sec RA = 229
64213 deg
ZDOT = 4330
514515 TA = 210
38312
MA = 210
40874
Ha = 189
224 n
mi
Hp = 183
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17577940
91 X = -5319455
02
Y = -5921841
32 feet Y = -1864676
14 meter
Z = -11967292
96 Z = -3673566
20
XDOT = -2693
365301 XDOT = -771
374120
YDOT = -20696
192897 feet/sec YDOT = -6317
103430 meter/sec
ZDOT = 14207
724787 ZDOT = 4326
645710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7740490
70 X = -2359301
57
Y = 16781359
60 feet Y = 5114958
41 meter
Z = -12072244
43 Z = -3679620
10
XDOT = -19649
583327 XDOT = -5989
192998
YDOT = 1138
819647 feet/sec YDOT = 347
112229 meter/sec
ZDOT = 14192
305222 ZDOT = 4325
814632
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
54415364
00016717 00000-0 10270-3 0 9001
2 25544 51
6445 230
5899 0001381 268
1603 91
9402 15
74228453 38762
Satellite: ISS
Catalog Number: 25544
Epoch time: 11154
54415364 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 230
5899 deg
Eccentricity:
0001381
Arg of perigee: 268
1603 deg
Mean anomaly: 91
9402 deg
Mean motion: 15
74228453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3876
Checksum: 307
Coasting Arc #2 (Orbit 3891)
---------------------------------------
Vector Time (GMT): 2011/155/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1095978
06 A = 6725041
97 meter
Y = 5401192
53 meter E =
0005220
Z = -3859538
29 I = 51
39930
XDOT = -6312
498576 Wp = 68
86966
YDOT = -1636
373424 meter/sec RA = 224
53907 deg
ZDOT = -4085
126665 TA = 158
35278
MA = 158
33070
Ha = 189
244 n
mi
Hp = 183
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3595728
54 X = 1054248
32
Y = 17720447
93 feet Y = 5413215
73 meter
Z = -12662527
21 Z = -3854314
52
XDOT = -20710
297164 XDOT = -6273
886414
YDOT = -5368
679213 feet/sec YDOT = -1706
747057 meter/sec
ZDOT = -13402
646538 ZDOT = -4115
699196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17975526
88 X = 5478940
59
Y = -2086644
91 feet Y = -636009
37 meter
Z = -12641577
44 Z = -3853152
80
XDOT = -7328
785829 XDOT = -2233
813921
YDOT = 18761
638040 feet/sec YDOT = 5718
547275 meter/sec
ZDOT = -13526
399961 ZDOT = -4122
846708
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
55984034
00016717 00000-0 10270-3 0 9019
2 25544 51
6442 225
3723 0001363 276
7751 83
3257 15
74239403 38924
Satellite: ISS
Catalog Number: 25544
Epoch time: 11155
55984034 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 225
3723 deg
Eccentricity:
0001363
Arg of perigee: 276
7751 deg
Mean anomaly: 83
3257 deg
Mean motion: 15
74239403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3892
Checksum: 307
Coasting Arc #3 (Orbit 3907)
---------------------------------------
Vector Time (GMT): 2011/156/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5653517
71 A = 6725874
59 meter
Y = 1041327
72 meter E =
0010865
Z = 3483124
25 I = 51
42584
XDOT = 1675
399684 Wp = 85
04741
YDOT = 6019
166083 meter/sec RA = 219
33371 deg
ZDOT = -4505
917714 TA = 53
43618
MA = 53
33623
Ha = 189
010 n
mi
Hp = 183
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18548286
45 X = 5624532
90
Y = 3416429
51 feet Y = 1104386
20 meter
Z = 11427572
99 Z = 3510518
64
XDOT = 5496
718124 XDOT = 1629
856504
YDOT = 19747
920219 feet/sec YDOT = 6037
647442 meter/sec
ZDOT = -14783
194600 ZDOT = -4497
888396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4729238
00 X = 1441471
74
Y = -18187848
48 feet Y = -5543656
22 meter
Z = 11538493
00 Z = 3516932
67
XDOT = 18769
680377 XDOT = 5720
998579
YDOT = -4504
263287 feet/sec YDOT = -1372
899450 meter/sec
ZDOT = -14750
895053 ZDOT = -4496
072812
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
57549630
00016717 00000-0 10270-3 0 9022
2 25544 51
6442 220
1548 0001498 288
5955 71
5046 15
74323129 39080
Satellite: ISS
Catalog Number: 25544
Epoch time: 11156
57549630 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 220
1548 deg
Eccentricity:
0001498
Arg of perigee: 288
5955 deg
Mean anomaly: 71
5046 deg
Mean motion: 15
74323129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3908
Checksum: 316
Coasting Arc #4 (Orbit 3923)
---------------------------------------
Vector Time (GMT): 2011/157/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1794114
13 A = 6724254
16 meter
Y = -5085940
71 meter E =
0009641
Z = 4009344
81 I = 51
44419
XDOT = 6607
144571 Wp = 100
54431
YDOT = 744
418021 meter/sec RA = 214
23275 deg
ZDOT = 3891
252108 TA = 309
17917
MA = 309
26476
Ha = 189
199 n
mi
Hp = 183
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5886201
20 X = -1756585
35
Y = -16686157
17 feet Y = -5105794
26 meter
Z = 13154018
40 Z = 4000719
56
XDOT = 21676
983501 XDOT = 6579
426417
YDOT = 2442
316341 feet/sec YDOT = 818
147643 meter/sec
ZDOT = 12766
575156 ZDOT = 3923
282172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16984899
66 X = -5176997
41
Y = 5049910
38 feet Y = 1539212
68 meter
Z = 13119260
44 Z = 3998750
58
XDOT = 3980
818509 XDOT = 1213
353482
YDOT = -20196
850897 feet/sec YDOT = -6156
000153 meter/sec
ZDOT = 12896
298121 ZDOT = 3930
791667
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
59112616
00016717 00000-0 10270-3 0 9036
2 25544 51
6435 214
9367 0001277 295
2752 64
8279 15
74337727 39247
Satellite: ISS
Catalog Number: 25544
Epoch time: 11157
59112616 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 214
9367 deg
Eccentricity:
0001277
Arg of perigee: 295
2752 deg
Mean anomaly: 64
8279 deg
Mean motion: 15
74337727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3924
Checksum: 327
Coasting Arc #5 (Orbit 3938)
---------------------------------------
Vector Time (GMT): 2011/158/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5860248
20 A = 6726196
80 meter
Y = -253574
43 meter E =
0003835
Z = -3293931
92 I = 51
47850
XDOT = -2395
035780 Wp = 77
01755
YDOT = -5606
539485 meter/sec RA = 209
03064 deg
ZDOT = 4698
053220 TA = 244
23915
MA = 244
27873
Ha = 189
079 n
mi
Hp = 183
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19226536
11 X = -5840975
91
Y = -831937
09 feet Y = -318999
17 meter
Z = -10806863
26 Z = -3322354
06
XDOT = -7857
728937 XDOT = -2354
986528
YDOT = -18394
158416 feet/sec YDOT = -5633
098810 meter/sec
ZDOT = 15413
560432 ZDOT = 4686
514876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1543402
68 X = -470429
14
Y = 19117215
21 feet Y = 5826927
20 meter
Z = -10922000
46 Z = -3329025
74
XDOT = -17281
900681 XDOT = -5267
523328
YDOT = 7374
139106 feet/sec YDOT = 2247
637599 meter/sec
ZDOT = 15367
009448 ZDOT = 4683
864480
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 11158
54325280
00016717 00000-0 10270-3 0 9046
2 25544 51
6442 210
0448 0001236 303
0491 57
0553 15
74406493 39397
Satellite: ISS
Catalog Number: 25544
Epoch time: 11158
54325280 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 210
0448 deg
Eccentricity:
0001236
Arg of perigee: 303
0491 deg
Mean anomaly: 57
0553 deg
Mean motion: 15
74406493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3939
Checksum: 287
Coasting Arc #6 (Orbit 3954)
---------------------------------------
Vector Time (GMT): 2011/159/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2340247
19 A = 6723319
98 meter
Y = 4700356
61 meter E =
0007559
Z = -4207196
57 I = 51
49676
XDOT = -6787
220577 Wp = 61
68648
YDOT = 139
398941 meter/sec RA = 203
93179 deg
ZDOT = -3621
042631 TA = 171
35052
MA = 171
33749
Ha = 189
113 n
mi
Hp = 183
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7677976
35 X = 2307950
71
Y = 15421117
47 feet Y = 4726346
48 meter
Z = -13803138
35 Z = -4195905
69
XDOT = -22267
784045 XDOT = -6770
684601
YDOT = 457
345607 feet/sec YDOT = 63
592910 meter/sec
ZDOT = -11880
061124 ZDOT = -3653
974677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15572128
90 X = 4746384
89
Y = -7451671
89 feet Y = -2271269
59 meter
Z = -13757550
68 Z = -4193301
45
XDOT = -529
249327 XDOT = -161
315195
YDOT = 21065
250120 feet/sec YDOT = 6420
688237 meter/sec
ZDOT = -12013
494484 ZDOT = -3661
713119
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 11159
55882710
00016717 00000-0 10270-3 0 9055
2 25544 51
6448 204
8264 0001298 309
5926 50
5123 15
74427322 39555
Satellite: ISS
Catalog Number: 25544
Epoch time: 11159
55882710 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 204
8264 deg
Eccentricity:
0001298
Arg of perigee: 309
5926 deg
Mean anomaly: 50
5123 deg
Mean motion: 15
74427322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3955
Checksum: 314
Coasting Arc #7 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2011/160/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5981554
33 A = 6726727
35 meter
Y = -508129
50 meter E =
0012201
Z = 3024189
61 I = 51
53653
XDOT = 2938
891043 Wp = 91
56341
YDOT = 5134
996954 meter/sec RA = 198
73471 deg
ZDOT = -4933
298747 TA = 53
36572
MA = 53
25359
Ha = 189
007 n
mi
Hp = 183
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19624522
09 X = 5972100
78
Y = -1667091
54 feet Y = -441293
25 meter
Z = 9921881
93 Z = 3053225
04
XDOT = 9642
030982 XDOT = 2905
217198
YDOT = 16847
102867 feet/sec YDOT = 5167
673576 meter/sec
ZDOT = -16185
363343 ZDOT = -4919
102931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1613054
17 X = -491658
91
Y = -19569116
07 feet Y = -5964666
58 meter
Z = 10039549
56 Z = 3060054
71
XDOT = 15445
925317 XDOT = 4707
918037
YDOT = -9575
211824 feet/sec YDOT = -2918
524564 meter/sec
ZDOT = -16128
013830 ZDOT = -4915
818615
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 11160
57437292
00016717 00000-0 10270-3 0 9061
2 25544 51
6437 199
6080 0001366 318
7947 41
3114 15
74483509 39716
Satellite: ISS
Catalog Number: 25544
Epoch time: 11160
57437292 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 199
6080 deg
Eccentricity:
0001366
Arg of perigee: 318
7947 deg
Mean anomaly: 41
3114 deg
Mean motion: 15
74483509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 321
Coasting Arc #8 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2011/161/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2753688
13 A = 6722380
12 meter
Y = -4264258
38 meter E =
0008328
Z = 4401592
83 I = 51
55093
XDOT = 6884
169729 Wp = 105
49460
YDOT = -1028
488643 meter/sec RA = 193
63710 deg
ZDOT = 3303
062818 TA = 311
27948
MA = 311
35116
Ha = 189
168 n
mi
Hp = 183
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9034409
88 X = -2727181
98
Y = -13990349
01 feet Y = -4294904
02 meter
Z = 14440921
35 Z = 4388279
30
XDOT = 22585
858690 XDOT = 6879
113061
YDOT = -3374
306573 feet/sec YDOT = -951
534273 meter/sec
ZDOT = 10836
820268 ZDOT = 3336
493930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13856267
87 X = -4223390
45
Y = 9322308
36 feet Y = 2841439
59 meter
Z = 14387113
83 Z = 4385192
30
XDOT = -3019
381284 XDOT = -920
307415
YDOT = -21458
847557 feet/sec YDOT = -6540
656735 meter/sec
ZDOT = 10972
327790 ZDOT = 3344
365510
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 11161
58989195
00016717 00000-0 10270-3 0 9078
2 25544 51
6433 194
3891 0001334 326
0961 34
0117 15
74498658 39877
Satellite: ISS
Catalog Number: 25544
Epoch time: 11161
58989195 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 194
3891 deg
Eccentricity:
0001334
Arg of perigee: 326
0961 deg
Mean anomaly: 34
0117 deg
Mean motion: 15
74498658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 339
Coasting Arc #9 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2011/162/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6013461
35 A = 6727228
65 meter
Y = 1289552
44 meter E =
0004955
Z = -2723797
94 I = 51
59933
XDOT = -3330
121545 Wp = 43
56961
YDOT = -4634
766792 meter/sec RA = 188
44700 deg
ZDOT = 5166
875496 TA = 285
31804
MA = 285
37280
Ha = 188
976 n
mi
Hp = 183
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19729203
90 X = -6014202
60
Y = 4230815
10 feet Y = 1222302
45 meter
Z = -8936344
95 Z = -2753013
25
XDOT = -10925
595620 XDOT = -3303
147159
YDOT = -15205
927796 feet/sec YDOT = -4671
856033 meter/sec
ZDOT = 16951
691260 ZDOT = 5150
762581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4851213
00 X = 1478649
72
Y = 19531412
28 feet Y = 5953174
46 meter
Z = -9054789
39 Z = -2759899
81
XDOT = -13424
099887 XDOT = -4091
665646
YDOT = 11149
269761 feet/sec YDOT = 3398
297423 meter/sec
ZDOT = 16886
548735 ZDOT = 5147
020055
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 11162
54191421
00016717 00000-0 10270-3 0 9083
2 25544 51
6441 189
4974 0001348 329
1819 30
9265 15
74572572 40020
Satellite: ISS
Catalog Number: 25544
Epoch time: 11162
54191421 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 189
4974 deg
Eccentricity:
0001348
Arg of perigee: 329
1819 deg
Mean anomaly: 30
9265 deg
Mean motion: 15
74572572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 307
Coasting Arc #10 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2011/163/12:52:20
377
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3014203
33 A = 6721276
92 meter
Y = 3846887
43 meter E =
0010411
Z = -4624465
99 I = 51
60841
XDOT = -6868
648876 Wp = 62
62749
YDOT = 1898
267292 meter/sec RA = 183
34959 deg
ZDOT = -2898
141882 TA = 178
64585
MA = 178
64303
Ha = 189
000 n
mi
Hp = 183
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9889118
55 X = 2993427
72
Y = 12621021
74 feet Y = 3880478
60 meter
Z = -15172132
51 Z = -4609872
74
XDOT = -22534
937256 XDOT = -6875
286379
YDOT = 6227
911064 feet/sec YDOT = 1821
421204 meter/sec
ZDOT = -9508
339509 ZDOT = -2931
525961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12117701
84 X = 3693475
52
Y = -10584583
18 feet Y = -3226180
95 meter
Z = -15113118
85 Z = -4606478
63
XDOT = 6546
191619 XDOT = 1995
279205
YDOT = 21262
783850 feet/sec YDOT = 6480
896518 meter/sec
ZDOT = -9643
716118 ZDOT = -2939
404673
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 11163
55737782
00016717 00000-0 10270-3 0 9092
2 25544 51
6428 184
2780 0001453 330
9573 29
1510 15
74591276 40189
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
55737782 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 184
2780 deg
Eccentricity:
0001453
Arg of perigee: 330
9573 deg
Mean anomaly: 29
1510 deg
Mean motion: 15
74591276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 315
Coasting Arc #11 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2011/163/14:43:43
105
Vector Time (MET): N/A
Weight (LBS) : 903960
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5279406
49 A = 6734170
30 meter
Y = 2428196
04 meter E =
0005837
Z = -3399989
33 I = 51
62331
XDOT = -4768
912433 Wp = 253
06334
YDOT = -3899
131376 meter/sec RA = 182
90401 deg
ZDOT = 4612
183173 TA = 66
83245
MA = 66
77096
Ha = 192
104 n
mi
Hp = 190
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17320887
44 X = -5289649
97
Y = 7966522
43 feet Y = 2369101
74 meter
Z = -11154820
65 Z = -3425661
47
XDOT = -15646
038167 XDOT = -4747
362529
YDOT = -12792
425773 feet/sec YDOT = -3952
340450 meter/sec
ZDOT = 15131
834556 ZDOT = 4589
067322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15662216
12 X = 4773843
47
Y = 10762874
26 feet Y = 3280524
07 meter
Z = -11258959
50 Z = -3431730
86
XDOT = -2172
601219 XDOT = -662
208851
YDOT = 18920
813900 feet/sec YDOT = 5767
064077 meter/sec
ZDOT = 15038
278844 ZDOT = 4583
667392
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 11163
62086078
00016717 00000-0 10270-3 0 9107
2 25544 51
6411 183
9515 0010664 261
5800 98
4153 15
71508387 40190
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
62086078 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 183
9515 deg
Eccentricity:
0010664
Arg of perigee: 261
5800 deg
Mean anomaly: 98
4153 deg
Mean motion: 15
71508387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 301
Coasting Arc #12 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2011/163/18:55:23
279
Vector Time (MET): N/A
Weight (LBS) : 902208
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4286010
91 A = 6742792
24 meter
Y = 3324201
30 meter E =
0009012
Z = -4000335
80 I = 51
62451
XDOT = -5928
639909 Wp = 170
29950
YDOT = 2911
025014 meter/sec RA = 182
06190 deg
ZDOT = -3943
012169 TA = 58
91161
MA = 58
82320
Ha = 201
625 n
mi
Hp = 193
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14061715
57 X = 4267953
60
Y = 10906172
25 feet Y = 3372029
73 meter
Z = -13124461
28 Z = -3979557
50
XDOT = -19450
918338 XDOT = -5941
596291
YDOT = 9550
607000 feet/sec YDOT = 2844
655528 meter/sec
ZDOT = -12936
391631 ZDOT = -3971
844812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14833734
21 X = -4521322
19
Y = -9941694
82 feet Y = -3030228
58 meter
Z = -13040358
71 Z = -3974701
34
XDOT = 17970
462859 XDOT = 5477
397080
YDOT = -9734
660219 feet/sec YDOT = -2967
124435 meter/sec
ZDOT = -13053
360507 ZDOT = -3978
664282
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 11163
81172716
00016717 00000-0 10270-3 0 9114
2 25544 51
6431 182
9767 0012098 204
7688 155
2892 15
67890162 40222
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
81172716 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 182
9767 deg
Eccentricity:
0012098
Arg of perigee: 204
7688 deg
Mean anomaly: 155
2892 deg
Mean motion: 15
67890162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 320
Coasting Arc #13 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2011/164/18:55:23
279
Vector Time (MET): N/A
Weight (LBS) : 902208
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2877260
58 A = 6739931
62 meter
Y = -3877683
27 meter E =
0007045
Z = 4698382
65 I = 51
64513
XDOT = 6947
080469 Wp = 172
12020
YDOT = 1815
842600 meter/sec RA = 176
92716 deg
ZDOT = -2762
049479 TA = 305
09347
MA = 305
15951
Ha = 201
288 n
mi
Hp = 193
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9439831
29 X = 2897583
67
Y = -12722057
98 feet Y = -3845395
21 meter
Z = 15414641
26 Z = 4712409
17
XDOT = 22792
258758 XDOT = 6939
676676
YDOT = 5957
488845 feet/sec YDOT = 1893
488170 meter/sec
ZDOT = -9061
842124 ZDOT = -2728
317962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8250759
83 X = -2514831
60
Y = 13458289
92 feet Y = 4102086
77 meter
Z = 15471642
90 Z = 4715756
76
XDOT = -22282
926197 XDOT = -6791
835905
YDOT = -3424
325410 feet/sec YDOT = -1043
734385 meter/sec
ZDOT = -8925
166872 ZDOT = -2720
390863
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 11164
83151933
00016717 00000-0 10270-3 0 9126
2 25544 51
6423 177
7876 0012083 208
9182 151
1309 15
67916357 40385
Satellite: ISS
Catalog Number: 25544
Epoch time: 11164
83151933 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 177
7876 deg
Eccentricity:
0012083
Arg of perigee: 208
9182 deg
Mean anomaly: 151
1309 deg
Mean motion: 15
67916357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 315
Coasting Arc #14 (Orbit 4053)
---------------------------------------
Vector Time (GMT): 2011/165/18:55:23
279
Vector Time (MET): N/A
Weight (LBS) : 902208
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6708378
39 A = 6749408
96 meter
Y = 549481
21 meter E =
0003897
Z = 513355
06 I = 51
70757
XDOT = 69
185526 Wp = 117
54561
YDOT = -4796
912986 meter/sec RA = 171
86509 deg
ZDOT = 6002
061437 TA = 248
01474
MA = 248
05616
Ha = 201
126 n
mi
Hp = 193
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22009115
44 X = -6716518
00
Y = 1802759
87 feet Y = 474418
44 meter
Z = 1684235
75 Z = 480745
98
XDOT = 226
986633 XDOT = 93
663375
YDOT = -15737
903496 feet/sec YDOT = -4796
003618 meter/sec
ZDOT = 19691
802616 ZDOT = 6002
456064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21725194
63 X = 6621839
32
Y = -4011852
03 feet Y = -1222812
50 meter
Z = 1552004
28 Z = 473050
90
XDOT = 1184
571818 XDOT = 361
057490
YDOT = 14083
613474 feet/sec YDOT = 4292
685387 meter/sec
ZDOT = 19693
581030 ZDOT = 6002
603498
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 11165
85129265
00016717 00000-0 10270-3 0 9133
2 25544 51
6425 172
5969 0012061 212
9197 147
1212 15
67928549 40542
Satellite: ISS
Catalog Number: 25544
Epoch time: 11165
85129265 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 172
5969 deg
Eccentricity:
0012061
Arg of perigee: 212
9197 deg
Mean anomaly: 147
1212 deg
Mean motion: 15
67928549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4054
Checksum: 319
Coasting Arc #15 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2011/166/15:19:33
809
Vector Time (MET): N/A
Weight (LBS) : 900925
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3274875
16 A = 6749441
51 meter
Y = -4127162
94 meter E =
0012136
Z = 4206245
69 I = 51
70471
XDOT = 6598
474213 Wp = 107
83141
YDOT = 1499
478133 meter/sec RA = 167
51137 deg
ZDOT = -3661
123017 TA = 19
51632
MA = 19
46990
Ha = 205
204 n
mi
Hp = 196
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10744341
06 X = 3300349
34
Y = -13540560
82 feet Y = -4090399
70 meter
Z = 13800018
66 Z = 4222216
06
XDOT = 21648
537443 XDOT = 6599
001386
YDOT = 4919
547679 feet/sec YDOT = 1573
269959 meter/sec
ZDOT = -12011
558454 ZDOT = -3629
066090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17181575
20 X = -5236944
12
Y = 1336130
78 feet Y = 407252
66 meter
Z = 13864934
02 Z = 4226031
89
XDOT = -11005
079528 XDOT = -3354
348240
YDOT = -18052
536254 feet/sec YDOT = -5502
413050 meter/sec
ZDOT = -11881
625067 ZDOT = -3621
519320
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 11166
67995036
00016717 00000-0 10270-3 0 9142
2 25544 51
6395 168
3793 0006757 163
4989 196
6391 15
65267790 40673
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
67995036 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 168
3793 deg
Eccentricity:
0006757
Arg of perigee: 163
4989 deg
Mean anomaly: 196
6391 deg
Mean motion: 15
65267790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 369
Coasting Arc #16 (Orbit 4069)
---------------------------------------
Vector Time (GMT): 2011/166/19:26:13
236
Vector Time (MET): N/A
Weight (LBS) : 899354
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6627587
18 A = 6766052
11 meter
Y = 600598
46 meter E =
0007766
Z = 1194757
19 I = 51
73579
XDOT = 616
581282 Wp = 33
95366
YDOT = -4908
472588 meter/sec RA = 166
68116 deg
ZDOT = 5875
720893 TA = 339
05278
MA = 339
08457
Ha = 206
460 n
mi
Hp = 205
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21744052
44 X = -6639614
51
Y = 1970467
40 feet Y = 526417
27 meter
Z = 3919807
04 Z = 1162531
35
XDOT = 2022
904469 XDOT = 642
879828
YDOT = -16103
912690 feet/sec YDOT = -4901
431738 meter/sec
ZDOT = 19277
299517 ZDOT = 5878
779132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20580869
33 X = 6273048
97
Y = -7356761
53 feet Y = -2242340
92 meter
Z = 3789105
81 Z = 1154919
45
XDOT = 1648
071214 XDOT = 502
332106
YDOT = 14566
904322 feet/sec YDOT = 4439
992437 meter/sec
ZDOT = 19289
886714 ZDOT = 5879
557470
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 11166
87162043
00016717 00000-0 10270-3 0 9159
2 25544 51
6418 167
4105 0007376 263
2624 96
7694 15
61973285 40708
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
87162043 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 167
4105 deg
Eccentricity:
0007376
Arg of perigee: 263
2624 deg
Mean anomaly: 96
7694 deg
Mean motion: 15
61973285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4070
Checksum: 321
Coasting Arc #17 (Orbit 4084)
---------------------------------------
Vector Time (GMT): 2011/167/19:26:13
236
Vector Time (MET): N/A
Weight (LBS) : 899354
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4354358
95 A = 6757578
77 meter
Y = 2373187
98 meter E =
0003696
Z = -4593756
67 I = 51
73718
XDOT = -5558
478031 Wp = 33
36542
YDOT = 4351
633234 meter/sec RA = 161
65447 deg
ZDOT = -3018
832235 TA = 206
57396
MA = 206
59291
Ha = 206
140 n
mi
Hp = 205
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14285954
57 X = 4349813
35
Y = 7786049
79 feet Y = 2421856
55 meter
Z = -15071380
16 Z = -4572613
93
XDOT = -18236
476481 XDOT = -5592
060885
YDOT = 14277
011922 feet/sec YDOT = 4289
287777 meter/sec
ZDOT = -9904
305234 ZDOT = -3045
915841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15932729
26 X = -4856295
88
Y = -3665221
51 feet Y = -1117159
52 meter
Z = -14985721
84 Z = -4567648
02
XDOT = 13438
852478 XDOT = 4096
162235
YDOT = -17448
729868 feet/sec YDOT = -5318
372864 meter/sec
ZDOT = -10014
314963 ZDOT = -3052
363201
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 11167
83129154
00016717 00000-0 10270-3 0 9163
2 25544 51
6421 162
5696 0007489 267
1420 92
8879 15
62011465 40857
Satellite: ISS
Catalog Number: 25544
Epoch time: 11167
83129154 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 162
5696 deg
Eccentricity:
0007489
Arg of perigee: 267
1420 deg
Mean anomaly: 92
8879 deg
Mean motion: 15
62011465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4085
Checksum: 324
Coasting Arc #18 (Orbit 4100)
---------------------------------------
Vector Time (GMT): 2011/168/19:26:13
236
Vector Time (MET): N/A
Weight (LBS) : 899354
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 215466
31 A = 6755326
92 meter
Y = -4454268
12 meter E =
0004509
Z = 5077820
04 I = 51
75910
XDOT = 7290
660290 Wp = 313
69416
YDOT = -1650
440058 meter/sec RA = 156
58166 deg
ZDOT = -1755
055245 TA = 153
23642
MA = 153
21315
Ha = 205
835 n
mi
Hp = 205
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 706910
47 X = 240591
93
Y = -14613740
55 feet Y = -4451719
09 meter
Z = 16659514
58 Z = 5078926
98
XDOT = 23919
489142 XDOT = 7317
099612
YDOT = -5414
829585 feet/sec YDOT = -1568
763315 meter/sec
ZDOT = -5758
055265 ZDOT = -1719
573696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3560470
20 X = 1085231
32
Y = 14185516
18 feet Y = 4323745
33 meter
Z = 16664175
47 Z = 5079240
68
XDOT = -20401
532203 XDOT = -6218
387016
YDOT = 11723
669663 feet/sec YDOT = 3573
374513 meter/sec
ZDOT = -5614
067874 ZDOT = -1711
167888
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 11168
85492717
00016717 00000-0 10270-3 0 9175
2 25544 51
6425 157
4056 0007543 270
9194 89
1098 15
62058717 41017
Satellite: ISS
Catalog Number: 25544
Epoch time: 11168
85492717 = yrday
fracday
Element set: 917
Inclination: 51
6425 deg
RA of node: 157
4056 deg
Eccentricity:
0007543
Arg of perigee: 270
9194 deg
Mean anomaly: 89
1098 deg
Mean motion: 15
62058717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4101
Checksum: 326
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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