[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 27th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3262)
---------------------------------------
Vector Time (GMT): 2011/115/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4126804
08 A = 6720097
67 meter
Y = -721005
37 meter E =
0016431
Z = -5268525
62 I = 51
94854
XDOT = 2133
274423 Wp = 101
06276
YDOT = 7357
353922 meter/sec RA = 69
94728 deg
ZDOT = 662
771742 TA = 175
22943
MA = 175
21375
Ha = 190
607 n
mi
Hp = 183
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13539383
48 X = 4160153
24
Y = -2365503
17 feet Y = -674670
52 meter
Z = -17285189
05 Z = -5248396
67
XDOT = 6998
931834 XDOT = 2047
624921
YDOT = 24138
300269 feet/sec YDOT = 7380
730604 meter/sec
ZDOT = 2174
447973 ZDOT = 672
927049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -151167
18 X = -46075
76
Y = -13845514
42 feet Y = -4220112
79 meter
Z = -17203695
81 Z = -5243686
48
XDOT = 23935
901387 XDOT = 7295
662743
YDOT = -3019
442827 feet/sec YDOT = -920
326174 meter/sec
ZDOT = 2215
289381 ZDOT = 675
220203
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 11115
64888285
00016717 00000-0 10270-3 0 9005
2 25544 51
6453 70
5718 0002290 143
6273 216
5046 15
74054821 32638
Satellite: ISS
Catalog Number: 25544
Epoch time: 11115
64888285 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 70
5718 deg
Eccentricity:
0002290
Arg of perigee: 143
6273 deg
Mean anomaly: 216
5046 deg
Mean motion: 15
74054821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3263
Checksum: 297
Coasting Arc #2 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2011/116/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2389562
55 A = 6731752
21 meter
Y = -6254653
67 meter E =
0013140
Z = -633851
60 I = 51
97671
XDOT = 4652
694055 Wp = 141
71214
YDOT = -1174
724355 meter/sec RA = 64
84571 deg
ZDOT = -6024
484519 TA = 45
15905
MA = 45
05236
Ha = 190
514 n
mi
Hp = 183
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7839772
14 X = -2316365
09
Y = -20520517
28 feet Y = -6280965
95 meter
Z = -2079565
61 Z = -645282
12
XDOT = 15264
744274 XDOT = 4694
750042
YDOT = -3854
082529 feet/sec YDOT = -1122
460101 meter/sec
ZDOT = -19765
369156 ZDOT = -6001
779599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21429594
16 X = -6531740
30
Y = 4809632
29 feet Y = 1465975
92 meter
Z = -2125601
36 Z = -647883
30
XDOT = -1262
880248 XDOT = -384
925899
YDOT = -14213
530289 feet/sec YDOT = -4332
284032 meter/sec
ZDOT = -19673
432651 ZDOT = -5996
462272
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 11116
66466312
00016717 00000-0 10270-3 0 9012
2 25544 51
6454 65
3549 0002388 151
5122 208
6172 15
74085031 32798
Satellite: ISS
Catalog Number: 25544
Epoch time: 11116
66466312 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 65
3549 deg
Eccentricity:
0002388
Arg of perigee: 151
5122 deg
Mean anomaly: 208
6172 deg
Mean motion: 15
74085031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 294
Coasting Arc #3 (Orbit 3294)
---------------------------------------
Vector Time (GMT): 2011/117/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3987371
16 A = 6719678
60 meter
Y = 1317071
99 meter E =
0003686
Z = 5242804
14 I = 51
92323
XDOT = -3318
722182 Wp = 96
77201
YDOT = -6908
439464 meter/sec RA = 59
71800 deg
ZDOT = -788
477417 TA =
69808
MA =
69757
Ha = 190
336 n
mi
Hp = 183
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13081926
38 X = -4027271
18
Y = 4321102
34 feet Y = 1272259
87 meter
Z = 17200800
97 Z = 5223336
51
XDOT = -10888
196134 XDOT = -3237
393749
YDOT = -22665
483805 feet/sec YDOT = -6945
096724 meter/sec
ZDOT = -2586
868165 ZDOT = -804
402004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2625056
74 X = 800117
29
Y = 13624382
27 feet Y = 4152711
72 meter
Z = 17121961
40 Z = 5218773
83
XDOT = -22862
005658 XDOT = -6968
339324
YDOT = 7736
712225 feet/sec YDOT = 2358
149886 meter/sec
ZDOT = -2651
060888 ZDOT = -808
043359
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 11117
68039762
00016717 00000-0 10270-3 0 9021
2 25544 51
6455 60
1378 0002221 157
3559 202
7703 15
74219748 32953
Satellite: ISS
Catalog Number: 25544
Epoch time: 11117
68039762 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 60
1378 deg
Eccentricity:
0002221
Arg of perigee: 157
3559 deg
Mean anomaly: 202
7703 deg
Mean motion: 15
74219748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3295
Checksum: 308
Coasting Arc #4 (Orbit 3310)
---------------------------------------
Vector Time (GMT): 2011/118/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3364684
66 A = 6731208
09 meter
Y = 5773335
97 meter E =
0013026
Z = 766380
80 I = 51
94627
XDOT = -4478
753621 Wp = 62
40536
YDOT = 1804
361105 meter/sec RA = 54
61564 deg
ZDOT = 5999
378590 TA = 305
91458
MA = 306
03540
Ha = 190
128 n
mi
Hp = 183
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11038991
66 X = 3296153
08
Y = 18941390
99 feet Y = 5810578
77 meter
Z = 2514372
70 Z = 782559
84
XDOT = -14694
073561 XDOT = -4527
741494
YDOT = 5919
819897 feet/sec YDOT = 1754
003272 meter/sec
ZDOT = 19683
000623 ZDOT = 5977
501648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20030181
32 X = 6105199
27
Y = -8893539
80 feet Y = -2710750
93 meter
Z = 2579629
00 Z = 786270
92
XDOT = 3622
465183 XDOT = 1104
127388
YDOT = 13908
143595 feet/sec YDOT = 4239
202168 meter/sec
ZDOT = 19594
391785 ZDOT = 5972
370616
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 11118
69609166
00016717 00000-0 10270-3 0 9035
2 25544 51
6459 54
9201 0002210 160
7602 199
3645 15
74247206 33113
Satellite: ISS
Catalog Number: 25544
Epoch time: 11118
69609166 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 54
9201 deg
Eccentricity:
0002210
Arg of perigee: 160
7602 deg
Mean anomaly: 199
3645 deg
Mean motion: 15
74247206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3311
Checksum: 292
Coasting Arc #5 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2011/119/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3845411
67 A = 6719522
03 meter
Y = -1803280
00 meter E =
0015417
Z = -5220305
16 I = 51
88913
XDOT = 4321
827511 Wp = 105
43037
YDOT = 6279
659279 meter/sec RA = 49
48123 deg
ZDOT = 1012
807897 TA = 174
21442
MA = 174
19659
Ha = 189
920 n
mi
Hp = 183
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12616180
00 X = 3890650
01
Y = -5916272
98 feet Y = -1760025
50 meter
Z = -17126985
43 Z = -5201514
04
XDOT = 14179
224117 XDOT = 4246
365867
YDOT = 20602
556691 feet/sec YDOT = 6327
566681 meter/sec
ZDOT = 3322
860556 ZDOT = 1033
620021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4723404
19 X = -1439693
60
Y = -13208381
77 feet Y = -4025914
76 meter
Z = -17050865
60 Z = -5197103
83
XDOT = 20853
314524 XDOT = 6356
090267
YDOT = -11861
775111 feet/sec YDOT = -3615
469054 meter/sec
ZDOT = 3406
836485 ZDOT = 1038
403761
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 11119
64826351
00016717 00000-0 10270-3 0 9049
2 25544 51
6461 50
0284 0002212 167
3536 192
7683 15
74328847 33261
Satellite: ISS
Catalog Number: 25544
Epoch time: 11119
64826351 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 50
0284 deg
Eccentricity:
0002212
Arg of perigee: 167
3536 deg
Mean anomaly: 192
7683 deg
Mean motion: 15
74328847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3326
Checksum: 304
Coasting Arc #6 (Orbit 3341)
---------------------------------------
Vector Time (GMT): 2011/120/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4152677
58 A = 6730722
24 meter
Y = -5189151
04 meter E =
0011796
Z = -1025977
78 I = 51
90655
XDOT = 4323
753200 Wp = 148
00327
YDOT = -2292
248370 meter/sec RA = 44
38046 deg
ZDOT = -5947
595710 TA = 43
17445
MA = 43
08202
Ha = 189
827 n
mi
Hp = 183
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13624270
29 X = -4089358
79
Y = -17024773
76 feet Y = -5235234
79 meter
Z = -3366068
82 Z = -1045997
82
XDOT = 14185
541996 XDOT = 4377
956913
YDOT = -7520
499903 feet/sec YDOT = -2243
594596 meter/sec
ZDOT = -19513
109286 ZDOT = -5926
458945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17994025
18 X = -5484578
87
Y = 12293421
61 feet Y = 3747034
91 meter
Z = -3446871
71 Z = -1050606
50
XDOT = -5534
946199 XDOT = -1687
051601
YDOT = -13512
134030 feet/sec YDOT = -4118
498452 meter/sec
ZDOT = -19427
476463 ZDOT = -5921
494826
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 11120
66387254
00016717 00000-0 10270-3 0 9058
2 25544 51
6464 44
8109 0002412 174
8887 185
2301 15
74342091 33424
Satellite: ISS
Catalog Number: 25544
Epoch time: 11120
66387254 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 44
8109 deg
Eccentricity:
0002412
Arg of perigee: 174
8887 deg
Mean anomaly: 185
2301 deg
Mean motion: 15
74342091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3342
Checksum: 296
Coasting Arc #7 (Orbit 3357)
---------------------------------------
Vector Time (GMT): 2011/121/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3709363
61 A = 6719352
50 meter
Y = 2195815
98 meter E =
0003568
Z = 5151512
00 I = 51
84682
XDOT = -5155
309352 Wp = 84
77364
YDOT = -5567
241337 meter/sec RA = 39
23725 deg
ZDOT = -1337
971984 TA = 17
99087
MA = 17
97824
Ha = 189
648 n
mi
Hp = 183
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12169828
13 X = -3758667
46
Y = 7204120
66 feet Y = 2154059
98 meter
Z = 16901286
10 Z = 5133371
86
XDOT = -16913
744594 XDOT = -5086
172509
YDOT = -18265
227482 feet/sec YDOT = -5624
504579 meter/sec
ZDOT = -4389
671864 ZDOT = -1362
848889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6486429
49 X = 1977063
71
Y = 12665286
95 feet Y = 3860379
46 meter
Z = 16827783
04 Z = 5129108
27
XDOT = -18283
803379 XDOT = -5572
903270
YDOT = 15334
544993 feet/sec YDOT = 4673
969314 meter/sec
ZDOT = -4490
101221 ZDOT = -1368
582852
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 11121
67943530
00016717 00000-0 10270-3 0 9066
2 25544 51
6466 39
5927 0002246 180
8549 179
2611 15
74476086 33588
Satellite: ISS
Catalog Number: 25544
Epoch time: 11121
67943530 = yrday
fracday
Element set: 906
Inclination: 51
6466 deg
RA of node: 39
5927 deg
Eccentricity:
0002246
Arg of perigee: 180
8549 deg
Mean anomaly: 179
2611 deg
Mean motion: 15
74476086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3358
Checksum: 328
Coasting Arc #8 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2011/122/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4799822
02 A = 6729851
77 meter
Y = 4517760
62 meter E =
0012755
Z = 1331746
86 I = 51
85776
XDOT = -4194
201177 Wp = 68
01520
YDOT = 2716
727459 meter/sec RA = 34
13699 deg
ZDOT = 5860
632911 TA = 306
56897
MA = 306
68629
Ha = 189
358 n
mi
Hp = 182
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15747447
56 X = 4742477
32
Y = 14822049
27 feet Y = 4571114
49 meter
Z = 4369248
23 Z = 1354925
56
XDOT = -13760
502550 XDOT = -4252
738803
YDOT = 8913
147832 feet/sec YDOT = 2669
497985 meter/sec
ZDOT = 19227
798266 ZDOT = 5840
114973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15445146
84 X = 4707680
76
Y = -15109469
71 feet Y = -4605366
37 meter
Z = 4462840
30 Z = 1360273
72
XDOT = 7244
455994 XDOT = 2208
110187
YDOT = 13097
868322 feet/sec YDOT = 3992
230265 meter/sec
ZDOT = 19144
647748 ZDOT = 5835
288633
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 11122
69495597
00016717 00000-0 10270-3 0 9075
2 25544 51
6460 34
3739 0002302 187
1760 172
9371 15
74535757 33746
Satellite: ISS
Catalog Number: 25544
Epoch time: 11122
69495597 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 34
3739 deg
Eccentricity:
0002302
Arg of perigee: 187
1760 deg
Mean anomaly: 172
9371 deg
Mean motion: 15
74535757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 325
Coasting Arc #9 (Orbit 3388)
---------------------------------------
Vector Time (GMT): 2011/123/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3637261
77 A = 6719471
77 meter
Y = -2537776
03 meter E =
0013637
Z = -5060029
17 I = 51
79629
XDOT = 5770
784537 Wp = 112
76464
YDOT = 4773
428678 meter/sec RA = 28
98274 deg
ZDOT = 1752
696820 TA = 174
10036
MA = 174
08428
Ha = 189
201 n
mi
Hp = 183
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11933273
52 X = 3689950
47
Y = -8326036
84 feet Y = -2496807
20 meter
Z = -16601145
56 Z = -5042231
14
XDOT = 18933
020133 XDOT = 5708
463808
YDOT = 15660
855244 feet/sec YDOT = 4837
612582 meter/sec
ZDOT = 5750
317652 ZDOT = 1780
580558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8045386
29 X = -2452233
74
Y = -12222423
87 feet Y = -3725394
79 meter
Z = -16529006
46 Z = -5038041
17
XDOT = 15204
035811 XDOT = 4634
190115
YDOT = -17943
159251 feet/sec YDOT = -5469
074940 meter/sec
ZDOT = 5862
927527 ZDOT = 1787
020310
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 11123
64696758
00016717 00000-0 10270-3 0 9084
2 25544 51
6452 29
4807 0002302 192
1482 167
9627 15
74592187 33899
Satellite: ISS
Catalog Number: 25544
Epoch time: 11123
64696758 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 29
4807 deg
Eccentricity:
0002302
Arg of perigee: 192
1482 deg
Mean anomaly: 167
9627 deg
Mean motion: 15
74592187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3389
Checksum: 337
Coasting Arc #10 (Orbit 3404)
---------------------------------------
Vector Time (GMT): 2011/124/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5242756
33 A = 6729016
12 meter
Y = -3829549
01 meter E =
0009022
Z = -1752063
29 I = 51
80115
XDOT = 4150
136902 Wp = 154
56521
YDOT = -3077
256789 meter/sec RA = 23
88592 deg
ZDOT = -5711
294967 TA = 44
79661
MA = 44
72381
Ha = 189
029 n
mi
Hp = 183
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17200644
11 X = -5191032
57
Y = -12564137
16 feet Y = -3887887
39 meter
Z = -5748239
14 Z = -1777407
58
XDOT = 13615
934717 XDOT = 4211
983812
YDOT = -10095
986842 feet/sec YDOT = -3030
501334 meter/sec
ZDOT = -18737
844379 ZDOT = -5690
983208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12667137
37 X = -3860943
47
Y = 17090229
43 feet Y = 5209101
93 meter
Z = -5850610
47 Z = -1783266
07
XDOT = -8768
045790 XDOT = -2672
500357
YDOT = -12864
543437 feet/sec YDOT = -3921
112840 meter/sec
ZDOT = -18655
503680 ZDOT = -5686
197522
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 11124
66240438
00016717 00000-0 10270-3 0 9098
2 25544 51
6449 24
2626 0002439 198
5704 161
5371 15
74623581 34053
Satellite: ISS
Catalog Number: 25544
Epoch time: 11124
66240438 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 24
2626 deg
Eccentricity:
0002439
Arg of perigee: 198
5704 deg
Mean anomaly: 161
5371 deg
Mean motion: 15
74623581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3405
Checksum: 305
Coasting Arc #11 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2011/125/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3616057
69 A = 6719782
52 meter
Y = 2847997
35 meter E =
0004821
Z = 4892268
36 I = 51
74197
XDOT = -6197
165378 Wp = 73
76874
YDOT = -3981
399564 meter/sec RA = 18
71958 deg
ZDOT = -2259
662534 TA = 38
17997
MA = 38
14583
Ha = 188
922 n
mi
Hp = 182
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11863706
34 X = -3671401
87
Y = 9343823
33 feet Y = 2807250
62 meter
Z = 16050749
22 Z = 4874567
08
XDOT = -20331
907407 XDOT = -6141
206833
YDOT = -13062
334526 feet/sec YDOT = -4050
386989 meter/sec
ZDOT = -7413
590990 ZDOT = -2289
633124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9477937
69 X = 2888875
41
Y = 11854199
28 feet Y = 3613159
94 meter
Z = 15978978
99 Z = 4870392
80
XDOT = -11970
140254 XDOT = -3648
498750
YDOT = 19741
065960 feet/sec YDOT = 6017
076905 meter/sec
ZDOT = -7534
670617 ZDOT = -2296
567604
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 11125
67779652
00016717 00000-0 10270-3 0 9107
2 25544 51
6447 19
0425 0002443 204
6380 155
4667 15
74721353 34218
Satellite: ISS
Catalog Number: 25544
Epoch time: 11125
67779652 = yrday
fracday
Element set: 910
Inclination: 51
6447 deg
RA of node: 19
0425 deg
Eccentricity:
0002443
Arg of perigee: 204
6380 deg
Mean anomaly: 155
4667 deg
Mean motion: 15
74721353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 299
Coasting Arc #12 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2011/126/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5524463
97 A = 6727715
07 meter
Y = 3130822
48 meter E =
0012268
Z = 2208285
69 I = 51
73888
XDOT = -4158
355381 Wp = 79
66163
YDOT = 3448
025194 meter/sec RA = 13
62286 deg
ZDOT = 5490
942606 TA = 305
06737
MA = 305
18237
Ha = 188
608 n
mi
Hp = 182
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18124881
81 X = 5478316
36
Y = 10271727
31 feet Y = 3192342
19 meter
Z = 7245031
79 Z = 2235011
96
XDOT = -13642
898231 XDOT = -4223
277070
YDOT = 11312
418617 feet/sec YDOT = 3401
160516 meter/sec
ZDOT = 18014
903562 ZDOT = 5470
583685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9754368
32 X = 2973131
46
Y = -18365607
85 feet Y = -5597837
27 meter
Z = 7353023
53 Z = 2241201
57
XDOT = 10359
959530 XDOT = 3157
715665
YDOT = 12712
408305 feet/sec YDOT = 3874
742051 meter/sec
ZDOT = 17932
345066 ZDOT = 5465
778776
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 11126
69314568
00016717 00000-0 10270-3 0 9112
2 25544 51
6434 13
8218 0002584 208
9798 151
1222 15
74801444 34379
Satellite: ISS
Catalog Number: 25544
Epoch time: 11126
69314568 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 13
8218 deg
Eccentricity:
0002584
Arg of perigee: 208
9798 deg
Mean anomaly: 151
1222 deg
Mean motion: 15
74801444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 305
Coasting Arc #13 (Orbit 3451)
---------------------------------------
Vector Time (GMT): 2011/127/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3660579
87 A = 6720412
22 meter
Y = -3181337
41 meter E =
0010556
Z = -4662428
27 I = 51
68335
XDOT = 6393
979508 Wp = 122
88837
YDOT = 3209
360937 meter/sec RA = 8
44370 deg
ZDOT = 2829
193061 TA = 175
06727
MA = 175
05687
Ha = 188
524 n
mi
Hp = 183
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12009776
46 X = 3718531
49
Y = -10437458
70 feet Y = -3140078
20 meter
Z = -15296680
69 Z = -4644504
55
XDOT = 20977
623059 XDOT = 6343
872811
YDOT = 10529
399399 feet/sec YDOT = 3280
581911 meter/sec
ZDOT = 9282
129466 ZDOT = 2860
133745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10979007
48 X = -3346401
48
Y = -11612722
26 feet Y = -3539557
74 meter
Z = -15223987
37 Z = -4640271
35
XDOT = 8718
191588 XDOT = 2657
304796
YDOT = -20579
357636 feet/sec YDOT = -6272
588208 meter/sec
ZDOT = 9407
170971 ZDOT = 2867
305712
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 11127
64499784
00016717 00000-0 10270-3 0 9123
2 25544 51
6424 8
9268 0002552 211
0953 149
0060 15
74846371 34522
Satellite: ISS
Catalog Number: 25544
Epoch time: 11127
64499784 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 8
9268 deg
Eccentricity:
0002552
Arg of perigee: 211
0953 deg
Mean anomaly: 149
0060 deg
Mean motion: 15
74846371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3452
Checksum: 309
Coasting Arc #14 (Orbit 3467)
---------------------------------------
Vector Time (GMT): 2011/128/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5602132
02 A = 6726189
80 meter
Y = -2505237
80 meter E =
0005071
Z = -2749616
79 I = 51
67310
XDOT = 4241
712777 Wp = 148
82432
YDOT = -3834
987006 meter/sec RA = 3
34982 deg
ZDOT = -5156
493993 TA = 62
58970
MA = 62
53813
Ha = 188
269 n
mi
Hp = 182
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18379698
22 X = -5560344
43
Y = -8219284
13 feet Y = -2567650
40 meter
Z = -9021052
44 Z = -2776730
69
XDOT = 13916
380501 XDOT = 4309
330457
YDOT = -12581
978367 feet/sec YDOT = -3787
175166 meter/sec
ZDOT = -16917
631210 ZDOT = -5135
723726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7053221
91 X = -2149822
04
Y = 18805124
54 feet Y = 5731801
96 meter
Z = -9130644
95 Z = -2783020
58
XDOT = -12066
492498 XDOT = -3677
866913
YDOT = -12685
716822 feet/sec YDOT = -3866
606487 meter/sec
ZDOT = -16833
384268 ZDOT = -5130
815525
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 11128
66026395
00016717 00000-0 10270-3 0 9131
2 25544 51
6423 3
7068 0002493 217
0144 143
0848 15
74918318 34680
Satellite: ISS
Catalog Number: 25544
Epoch time: 11128
66026395 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 3
7068 deg
Eccentricity:
0002493
Arg of perigee: 217
0144 deg
Mean anomaly: 143
0848 deg
Mean motion: 15
74918318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3468
Checksum: 305
Coasting Arc #15 (Orbit 3483)
---------------------------------------
Vector Time (GMT): 2011/129/15:13:08
094
Vector Time (MET): N/A
Weight (LBS) : 879265
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3741412
38 A = 6721405
92 meter
Y = 3538080
69 meter E =
0007573
Z = 4314090
98 I = 51
62624
XDOT = -6398
736107 Wp = 81
60983
YDOT = -2537
311655 meter/sec RA = 358
15949 deg
ZDOT = -3462
185728 TA = 43
39016
MA = 43
33057
Ha = 188
242 n
mi
Hp = 182
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12274975
00 X = -3801654
89
Y = 11607876
29 feet Y = 3495904
87 meter
Z = 14153841
81 Z = 4295769
06
XDOT = -20993
228698 XDOT = -6353
069153
YDOT = -8324
513304 feet/sec YDOT = -2608
610674 meter/sec
ZDOT = -11358
877061 ZDOT = -3493
160017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12559231
25 X = 3828053
68
Y = 11392186
16 feet Y = 3472338
34 meter
Z = 14079518
68 Z = 4291437
29
XDOT = -5795
202419 XDOT = -1766
377697
YDOT = 20607
408352 feet/sec YDOT = 6281
138066 meter/sec
ZDOT = -11484
089804 ZDOT = -3500
350572
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 11129
67548720
00016717 00000-0 10270-3 0 9145
2 25544 51
6423 358
4852 0002695 221
6473 138
4486 15
74964034 34841
Satellite: ISS
Catalog Number: 25544
Epoch time: 11129
67548720 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 358
4852 deg
Eccentricity:
0002695
Arg of perigee: 221
6473 deg
Mean anomaly: 138
4486 deg
Mean motion: 15
74964034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3484
Checksum: 330
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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